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7/23/2019 A 320321 Mel Cdl
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SAUDI ARABIAN AIRLINES
MEL
/
CDL
A‐320
A‐321
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NUMBER DATE CHANGED INITI AL NUMBER DATE CHANGED INITI AL NUMBER DATE CHANGED INITI AL
1 36 71
2 37 72
3 38 73
4 39 74
5 40 75
6 41 76
7 42 77
8 43 78
9 44 79
10 45 80
11 46 81
12 47 82
13 48 83
14 49 84
15 50 85
16 51 86
17 52 87
18 53 88
19 54 89
20 55 90
21 56 91
22 57 92
23 58 93
24 59 94
25 60 95
26 61 96
27 62 97
28 63 98
29 64 99
30 65 100
31 66 101
32 67 102
33 68 103
34 69 104
35 70 105
30 JUN 12
MEL/CDL MANUAL
A320/321
MEL/CDL 00.00.01
LOG OF REVISIONS
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00.00.02
LOG OF REVISIONS
A320/321
MEL/CDLMEL/CDL MANUAL
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INTRODUCTION
A. Approval
The A 320 / 321 MEL/CDL Manual has been developed using thefollowing documents:
1) FAA 320/321 Master Minimum Equipment List (MMEL), Revision 22.
2) Airbus 320/321 Master Minimum Equipment List (MMEL), Date 31 JAN 12.
3) A 320/321 Airplane Flight Manual, Appendix CDL, Date 21 FEB 12.
General Authority of Civil Aviation Approval
Approved By:
Director Flight Operations Signature & Date
Safety & Economic Regulation
30 JUN 12MEL /CDL MANUAL
A320/321MEL/CDL 00.01
CONTEN
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B. MEL/CDL MANUAL CONTENTS AND ORGANIZATION
This Manual is divided into four Sections as detailed below:
Section 00 – Table of Contents, Introduction, Log of Revisions, and Control Page.
Section 01 – EICAS CROSS-REFERENCE LIST and MEL and (O) PROCEDURES.
This Section consists of MEL Table of Contents, Preamble, Definitions, EICAS Cross-Reference List
introduction, EICAS Cross-References, MEL and Operating (O) procedures.
Section 02 – CDL.
This Section consists of CDL Table of Contents, CDL Item General Locations, Notes, and CDL.
Section 03 – MEL (M) Procedures.
This section has been removed as per the Airbus MMEL new format and replaced with AircraftMaintenance Manual (AMM), this reference is only for maintenance personnel to follow.
Page Numbering:
The MEL, CDL, and Maintenance Procedures pages are numbered as follows:
01.21.01
Assigned Page Number
02.21.01
ATA System Number
03.21.01
Section Number
* * *
00.01.02CONTENTS
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ATA NUMBER SYSTEM PAGE
TABLE OF CONTENTS
- - LOG OF REVISIONS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.00.01 THRU 00.00.0- - INTTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.01.01 THRU 00.01.0
- - MEL/CDL MANUAL TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . 00.02.01 THRU 00.02.0
- - LIST OF EFFECTIVE PAGES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.03.01 THRU 00.03.2
MINIMUM EQUIPMENT LIST - SECTION 01
- - MEL TABLE OF CONTENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.00.01 THRU 01.00.2
- - FAA MMEL PREAMBLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.01 THRU 01.01.0
- - DEFINITIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.02 THRU 01.01.0
- - ECAM WARNING GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.02.01 THRU 01.02.0
- - ECAM WARNING LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.03.01 THRU 01.03.2
21 AIR CONDITIONING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.01 THRU 01.21.5
22 AUTO FLIGHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01 THRU 01.22.2
23 COMMUNICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.01 THRU 01.23.2
24 ELECTRICAL POWER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.01 THRU 01.24.2
25 EQUIPMENT/FURNISHINGS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.01 THRU 01.25.2
26 FIRE PROTECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01 THRU 01.26.2
27 FLIGHT CONTROLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.01 THRU 01.27.5
28 FUEL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01 THRU 01.28.6
29 HYDRAULIC POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.01 THRU 01.29.2
30 ICE AND RAIN PROTECTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.01 THRU 01.30.2
31 INDICATING / RECORDING SYSTEMS . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 THRU 01.31.2
32 LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.01 THRU 01.32.5
33 LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.01 THRU 01.33.1
34 NAVIGATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01 THRU 01.34.3
35 OXYGEN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.01 THRU 01.35.0
36 PNEUMATIC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 THRU 01.36.1
38 WATER & WASTE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.38.01 THRU 01.38.0
46 INFORMATION SYSTEM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.01 THRU 01.46.0
47 INERT GAS SYSTEM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.47.01 THRU 01.47.0
49 AIRBORNE AUXILIARY POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 THRU 01.49.0
52 DOORS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.01 THRU 01.52.3
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MINIMUM EQUIPMENT LIST - SECTION 01 (Cont’d)
56 WINDOWS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.01 THRU 01.56.04
70 ENGINE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.01 THRU 01.70.02
73 ENGINE FUEL AND CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.01 THRU 01.73.04
74 IGNITION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.01 THRU 01.74.04
76 ENGINE CONTROLS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.76.01 THRU 01.76.02
77 ENGINE INDICATING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.01 THRU 01.77.06
78 EXHAUST. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.01 THRU 01.78.06
79 OIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.01 THRU 01.79.04
80 STARTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.01 THRU 01.80.02
CONFIGURATION DEVIATION LIST - SECTION 02
- - CDL TABLE OF CONTENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.00.01 THRU 02.00.04
- - CDL INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.01.01 THRU 02.01.02
21 AIR CONDITIONING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.21.01 THRU 02.21.02
23 COMMUNICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.23.01 THRU 02.23.02
27 FLIGHT CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.01 THRU 02.27.20
28 FUEL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.01 THRU 02.28.0230 ICE AND RAIN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.30.01 THRU 02.30.02
32 LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.01 THRU 02.32.02
33 LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.01 THRU 02.33.10
49 AIRBORNE AUXILIARY POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.49.01 THRU 02.49.02
51 STRUCTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.01 THRU 02.51.04
52 DOORS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.01 THRU 02.52.36
53 FUSELAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.01 THRU 02.53.04
54 NACELLE/PAYLON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.01 THRU 02.54.08
57 WINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.01 THRU 02.57.04
71 STRUCTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.01 THRU 02.71.02
78 EXHAUST. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.78.01 THRU 02.78.02
* * *
00.02.02
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SYSTEM PAGE REV NO. DATE
LOG OF REVISION 00.00.01 Rev 07 12 FEB 12
LOG OF REVISION 00.00.02 Rev 07 12 FEB 12
CONTENTS 00.01.01 Rev 10 30 JUN 12
CONTENTS 00.01.02 Rev 07 12 FEB 12
TABLE OF CONTENTS 00.02.01 Rev 10 30 JUN 12
TABLE OF CONTENTS 00.02.02 Rev 07 12 FEB 12
LIST OF EFFECTIVE PAGES 00.03.01 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.02 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.03 Rev 09 01 MAY 12
LIST OF EFFECTIVE PAGES 00.03.04 Rev 07 12 FEB 12
LIST OF EFFECTIVE PAGES 00.03.05 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.06 Rev 09 01 MAY 12
LIST OF EFFECTIVE PAGES 00.03.07 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.08 Rev 09 01 MAY 12
LIST OF EFFECTIVE PAGES 00.03.09 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.10 Rev 07 12 FEB 12
LIST OF EFFECTIVE PAGES 00.03.11 Rev 07 12 FEB 12
LIST OF EFFECTIVE PAGES 00.03.12 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.13 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.14 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.15 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.16 Rev 10 30 JUN 12LIST OF EFFECTIVE PAGES 00.03.17 Rev 09 01 MAY 12
LIST OF EFFECTIVE PAGES 00.03.18 Rev 10 30 JUN 12
LIST OF EFFECTIVE PAGES 00.03.19 Rev 07 12 FEB 12
LIST OF EFFECTIVE PAGES 00.03.20 Rev 07 12 FEB 12
LIST OF EFFECTIVE PAGES 00.03.21 Rev 07 12 FEB 12
LIST OF EFFECTIVE PAGES 00.03.22 Rev 07 12 FEB 12
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MINIMUM EQUIPMENT LIST - SECTION 01
TABLE OF CONTENTS 01.00.01 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.02 Rev 09 01 MAY 12
TABLE OF CONTENTS 01.00.03 Rev 09 01 MAY 12
TABLE OF CONTENTS 01.00.04 Rev 07 12 FEB 12
TABLE OF CONTENTS 01.00.05 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.06 Rev 07 12 FEB 12
TABLE OF CONTENTS 01.00.07 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.08 Rev 09 01 MAY 12
TABLE OF CONTENTS 01.00.09 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.10 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.11 Rev 07 12 FEB 12
TABLE OF CONTENTS 01.00.12 Rev 07 12 FEB 12
TABLE OF CONTENTS 01.00.13 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.14 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.15 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.16 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.17 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.18 Rev 07 12 FEB 12
TABLE OF CONTENTS 01.00.19 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.20 Rev 09 01 MAY 12
TABLE OF CONTENTS 01.00.21 Rev 09 01 MAY 12
TABLE OF CONTENTS 01.00.22 Rev 07 12 FEB 12TABLE OF CONTENTS 01.00.23 Rev 10 30 JUN 12
TABLE OF CONTENTS 01.00.24 Rev 07 12 FEB 12
TABLE OF CONTENTS 01.00.25 Rev 07 12 FEB 12
TABLE OF CONTENTS 01.00.26 Rev 07 12 FEB 12
MEL INTRODUCTION 01.01.01 Rev 07 12 FEB 12
MEL INTRODUCTION 01.01.02 Rev 07 12 FEB 12
MEL INTRODUCTION 01.01.03 Rev 07 12 FEB 12
MEL INTRODUCTION 01.01.04 Rev 07 12 FEB 12
MEL INTRODUCTION 01.01.05 Rev 07 12 FEB 12
MEL INTRODUCTION 01.01.06 Rev 07 12 FEB 12
GENERAL 01.02.01 Rev 07 12 FEB 12
GENERAL 01.02.02 Rev 07 12 FEB 12
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ECAM MESSAGES 01.03.01 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.02 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.03 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.04 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.05 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.06 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.07 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.08 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.09 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.10 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.11 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.12 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.13 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.14 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.15 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.16 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.17 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.18 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.19 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.20 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.21 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.22 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.23 Rev 07 12 FEB 12ECAM MESSAGES 01.03.24 Rev 09 01 MAY 12
ECAM MESSAGES 01.03.25 Rev 07 12 FEB 12
ECAM MESSAGES 01.03.26 Rev 07 12 FEB 12
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21 AIR CONDITIONING 01.21.01 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.02 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.03 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.04 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.05 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.06 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.07 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.08 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.09 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.10 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.11 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.12 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.13 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.14 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.15 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.16 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.17 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.18 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.19 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.20 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.21 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.22 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.23 Rev 07 12 FEB 1221 AIR CONDITIONING 01.21.24 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.25 Rev 07 12 FEB 12
21 AIR CONDITIONING 01.21.26 Rev 07 12 FEB 12
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21 AIR CONDITIONING 01.21.27 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.28 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.29 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.30 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.31 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.32 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.33 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.34 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.35 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.36 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.37 Rev 10 30 JUN 1
21 AIR CONDITIONING 01.21.38 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.39 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.40 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.41 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.42 Rev 07 12 FEB 1
21 AIR CONDITIONING 01.21.43 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.44 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.45 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.46 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.47 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.48 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.49 Rev 09 01 MAY 121 AIR CONDITIONING 01.21.50 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.51 Rev 09 01 MAY 1
21 AIR CONDITIONING 01.21.52 Rev 09 01 MAY 1
22 AUTO FLIGHT 01.22.01 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.02 Rev 09 01 MAY 1
22 AUTO FLIGHT 01.22.03 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.04 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.05 Rev 09 01 MAY 1
22 AUTO FLIGHT 01.22.06 Rev 09 01 MAY 1
22 AUTO FLIGHT 01.22.07 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.08 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.09 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.10 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.11 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.12 Rev 09 01 MAY 1
22 AUTO FLIGHT 01.22.13 Rev 07 12 FEB 1
22 AUTO FLIGHT 01.22.14 Rev 07 12 FEB 1
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22 AUTO FLIGHT 01.22.15 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.16 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.17 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.18 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.19 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.20 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.21 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.22 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.23 Rev 07 12 FEB 12
22 AUTO FLIGHT 01.22.24 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.01 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.02 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.03 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.04 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.05 Rev 09 01 MAY 12
23 COMMUNICATIONS 01.23.06 Rev 09 01 MAY 12
23 COMMUNICATIONS 01.23.07 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.08 Rev 09 01 MAY 12
23 COMMUNICATIONS 01.23.09 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.10 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.11 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.12 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.13 Rev 07 12 FEB 1223 COMMUNICATIONS 01.23.14 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.15 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.16 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.17 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.18 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.19 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.20 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.21 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.22 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.23 Rev 07 12 FEB 12
23 COMMUNICATIONS 01.23.24 Rev 07 12 FEB 12
24 ELECTRICAL POWER 01.24.01 Rev 07 12 FEB 12
24 ELECTRICAL POWER 01.24.02 Rev 07 12 FEB 12
24 ELECTRICAL POWER 01.24.03 Rev 07 12 FEB 12
24 ELECTRICAL POWER 01.24.04 Rev 07 12 FEB 12
24 ELECTRICAL POWER 01.24.05 Rev 07 12 FEB 12
24 ELECTRICAL POWER 01.24.06 Rev 07 12 FEB 12
00.03.06
LIST OF EFFECTIVE PAGES
A320/321MEL/CDL 01 MAY 12
MEL/CDL MANUAL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 14/763
SYSTEM PAGE REV NO. DATE
24 ELECTRICAL POWER 01.24.07 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.08 Rev 10 30 JUN 1
24 ELECTRICAL POWER 01.24.09 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.10 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.11 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.12 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.13 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.14 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.15 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.16 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.17 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.18 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.19 Rev 07 12 FEB 1
24 ELECTRICAL POWER 01.24.20 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.01 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.02 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.03 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.04 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.05 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.06 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.07 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.08 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.09 Rev 07 12 FEB 125 EQUIPMENT & FURNISHNGS 01.25.10 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.11 Rev 09 01 MAY 1
25 EQUIPMENT & FURNISHNGS 01.25.12 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.13 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.14 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.15 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.16 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.17 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.18 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.19 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.20 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.21 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.22 Rev 10 30 JUN 1
25 EQUIPMENT & FURNISHNGS 01.25.23 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.24 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.25 Rev 07 12 FEB 1
25 EQUIPMENT & FURNISHNGS 01.25.26 Rev 07 12 FEB 1
30 JUN 12
MEL/CDL MANUAL
A320/321MEL/CDL 00.03
LIST OF EFFECTIVE PAG
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 15/763
SYSTEM PAGE REV NO. DATE
26 FIRE PROTECTION 01.26.01 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.02 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.03 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.04 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.05 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.06 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.07 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.08 Rev 09 01 MAY 12
26 FIRE PROTECTION 01.26.09 Rev 09 01 MAY 12
26 FIRE PROTECTION 01.26.10 Rev 09 01 MAY 12
26 FIRE PROTECTION 01.26.11 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.12 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.13 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.14 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.15 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.16 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.17 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.18 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.19 Rev 07 12 FEB 12
26 FIRE PROTECTION 01.26.20 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.01 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.02 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.03 Rev 07 12 FEB 1227 FLIGHT CONTROL 01.27.04 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.05 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.06 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.07 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.08 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.09 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.10 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.11 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.12 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.13 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.14 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.15 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.16 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.17 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.18 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.19 Rev 07 12 FEB 12
27 FLIGHT CONTROL 01.27.20 Rev 07 12 FEB 12
00.03.08
LIST OF EFFECTIVE PAGES
A320/321MEL/CDL 01 MAY 12
MEL/CDL MANUAL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 16/763
SYSTEM PAGE REV NO. DATE
27 FLIGHT CONTROL 01.27.21 Rev 07 12 FEB 1
27 FLIGHT CONTROL 01.27.22 Rev 07 12 FEB 1
27 FLIGHT CONTROL 01.27.23 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.24 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.25 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.26 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.27 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.28 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.29 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.30 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.31 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.32 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.33 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.34 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.35 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.36 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.37 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.38 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.39 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.40 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.41 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.42 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.43 Rev 10 30 JUN 127 FLIGHT CONTROL 01.27.44 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.45 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.46 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.47 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.48 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.49 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.50 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.51 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.52 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.53 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.54 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.55 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.56 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.57 Rev 10 30 JUN 1
27 FLIGHT CONTROL 01.27.58 Rev 10 30 JUN 1
30 JUN 12
MEL/CDL MANUAL
A320/321MEL/CDL 00.03
LIST OF EFFECTIVE PAG
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 17/763
SYSTEM PAGE REV NO. DATE
28 FUEL 01.28.01 Rev 07 12 FEB 12
28 FUEL 01.28.02 Rev 07 12 FEB 12
28 FUEL 01.28.03 Rev 07 12 FEB 12
28 FUEL 01.28.04 Rev 07 12 FEB 12
28 FUEL 01.28.05 Rev 07 12 FEB 12
28 FUEL 01.28.06 Rev 07 12 FEB 12
28 FUEL 01.28.07 Rev 07 12 FEB 12
28 FUEL 01.28.08 Rev 07 12 FEB 12
28 FUEL 01.28.09 Rev 07 12 FEB 12
28 FUEL 01.28.10 Rev 07 12 FEB 12
28 FUEL 01.28.11 Rev 07 12 FEB 12
28 FUEL 01.28.12 Rev 07 12 FEB 12
28 FUEL 01.28.13 Rev 07 12 FEB 12
28 FUEL 01.28.14 Rev 07 12 FEB 12
28 FUEL 01.28.15 Rev 07 12 FEB 12
28 FUEL 01.28.16 Rev 07 12 FEB 12
28 FUEL 01.28.17 Rev 07 12 FEB 1228 FUEL 01.28.18 Rev 07 12 FEB 12
28 FUEL 01.28.19 Rev 07 12 FEB 12
28 FUEL 01.28.20 Rev 07 12 FEB 12
28 FUEL 01.28.21 Rev 07l 12 FEB 12
28 FUEL 01.28.22 Rev 07l 12 FEB 12
28 FUEL 01.28.23 Rev 07l 12 FEB 12
28 FUEL 01.28.24 Rev 07 12 FEB 12
28 FUEL 01.28.25 Rev 07 12 FEB 12
28 FUEL 01.28.26 Rev 07 12 FEB 12
28 FUEL 01.28.27 Rev 07 12 FEB 12
28 FUEL 01.28.28 Rev 07 12 FEB 12
28 FUEL 01.28.29 Rev 07 12 FEB 12
28 FUEL 01.28.30 Rev 07 12 FEB 12
00.03.10
LIST OF EFFECTIVE PAGES
A320/321MEL/CDL 30 JUN 12
MEL/CDL MANUAL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 18/763
SYSTEM PAGE REV NO. DATE
28 FUEL 01.28.31 Rev 07 12 FEB 1
28 FUEL 01.28.32 Rev 07 12 FEB 1
28 FUEL 01.28.33 Rev 07 12 FEB 1
28 FUEL 01.28.34 Rev 07 12 FEB 1
28 FUEL 01.28.35 Rev 07 12 FEB 1
28 FUEL 01.28.36 Rev 07 12 FEB 1
28 FUEL 01.28.37 Rev 07 12 FEB 1
28 FUEL 01.28.38 Rev 07 12 FEB 1
28 FUEL 01.28.39 Rev 07 12 FEB 1
28 FUEL 01.28.40 Rev 07 12 FEB 1
28 FUEL 01.28.41 Rev 07 12 FEB 1
28 FUEL 01.28.42 Rev 07 12 FEB 1
28 FUEL 01.28.43 Rev 07 12 FEB 1
28 FUEL 01.28.44 Rev 07 12 FEB 1
28 FUEL 01.28.45 Rev 07 12 FEB 1
28 FUEL 01.28.46 Rev 07 12 FEB 1
28 FUEL 01.28.47 Rev 07 12 FEB 1
28 FUEL 01.28.48 Rev 07 12 FEB 1
28 FUEL 01.28.49 Rev 07 12 FEB 1
28 FUEL 01.28.50 Rev 07 12 FEB 1
28 FUEL 01.28.51 Rev 07 12 FEB 1
28 FUEL 01.28.52 Rev 07 12 FEB 1
28 FUEL 01.28.53 Rev 07 12 FEB 128 FUEL 01.28.54 Rev 07 12 FEB 1
28 FUEL 01.28.55 Rev 07 12 FEB 1
28 FUEL 01.28.56 Rev 07 12 FEB 1
28 FUEL 01.28.57 Rev 07 12 FEB 1
28 FUEL 01.28.58 Rev 07 12 FEB 1
28 FUEL 01.28.59 Rev 07 12 FEB 1
28 FUEL 01.28.60 Rev 07 12 FEB 1
28 FUEL 01.28.61 Rev 07 12 FEB 1
28 FUEL 01.28.62 Rev 07 12 FEB 1
12 FEB 12
MEL/CDL MANUAL
A320/321MEL/CDL 00.03
LIST OF EFFECTIVE PAG
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 19/763
SYSTEM PAGE REV NO. DATE
29 HYDRAULIC 01.29.01 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.02 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.03 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.04 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.05 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.06 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.07 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.08 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.09 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.10 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.11 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.12 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.13 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.14 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.15 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.16 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.17 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.18 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.19 Rev 07 12 FEB 12
29 HYDRAULIC 01.29.20 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.01 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.02 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.03 Rev 07 12 FEB 1230 ICE AND RAIN PROTECTION 01.30.04 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.05 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.06 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.07 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.08 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.09 Rev 10 30 JUN 12
30 ICE AND RAIN PROTECTION 01.30.10 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.11 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.12 Rev 10 30 JUN 12
30 ICE AND RAIN PROTECTION 01.30.13 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 01.30.14 Rev 07 12 FEB 12
00.03.12
LIST OF EFFECTIVE PAGES
A320/321MEL/CDL 30 JUN 12
MEL/CDL MANUAL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 20/763
SYSTEM PAGE REV NO. DATE
30 ICE AND RAIN PROTECTION 01.30.15 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.16 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.17 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.18 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.19 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.20 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.21 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.22 Rev 10 30 JUN 1
30 ICE AND RAIN PROTECTION 01.30.23 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.24 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.25 Rev 07 12 FEB 1
30 ICE AND RAIN PROTECTION 01.30.26 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.01 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.02 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.03 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.04 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.05 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.06 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.07 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.08 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.09 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.10 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.11 Rev 07 12 FEB 131 INDICATING/RECORDING SYSTEM 01.31.12 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.13 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.14 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.15 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.16 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.17 Rev 07 12 FEB 1
31 INDICATING/RECORDING SYSTEM 01.31.18 Rev 07 12 FEB 1
30 JUN 12
MEL/CDL MANUAL
A320/321MEL/CDL 00.03
LIST OF EFFECTIVE PAG
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 21/763
SYSTEM PAGE REV NO. DATE
31 INDICATING/RECORDING SYSTEM 01.31.19 Rev 07 12 FEB 12
31 INDICATING/RECORDING SYSTEM 01.31.20 Rev 07 12 FEB 12
31 INDICATING/RECORDING SYSTEM 01.31.21 Rev 07 12 FEB 12
31 INDICATING/RECORDING SYSTEM 01.31.22 Rev 07 12 FEB 12
31 INDICATING/RECORDING SYSTEM 01.31.23 Rev 07 12 FEB 12
31 INDICATING/RECORDING SYSTEM 01.31.24 Rev 07 12 FEB 12
31 INDICATING/RECORDING SYSTEM 01.31.25 Rev 07 12 FEB 12
31 INDICATING/RECORDING SYSTEM 01.31.26 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.01 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.02 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.03 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.04 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.05 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.06 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.07 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.08 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.09 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.10 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.11 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.12 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.13 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.14 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.15 Rev 07 12 FEB 1232 LANDING GEAR 01.32.16 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.17 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.18 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.19 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.20 Rev 10 30 JUN 12
32 LANDING GEAR 01.32.21 Rev 09 01 MAY 12
32 LANDING GEAR 01.32.22 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.23 Rev 10 30 JUN 12
32 LANDING GEAR 01.32.24 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.25 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.26 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.27 Rev 10 30 JUN 12
32 LANDING GEAR 01.32.28 Rev 07 12 FEB 12
32 LANDING GEAR 01.32.29 Rev 10 30 JUN 12
32 LANDING GEAR 01.32.30 Rev 07 12 FEB 12
00.03.14
LIST OF EFFECTIVE PAGES
A320/321MEL/CDL 30 JUN 12
MEL/CDL MANUAL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 22/763
SYSTEM PAGE REV NO. DATE
32 LANDING GEAR 01.32.31 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.32 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.33 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.34 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.35 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.36 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.37 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.38 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.39 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.40 Rev10 30 JUN 1
32 LANDING GEAR 01.32.41 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.42 Rev10 30 JUN 1
32 LANDING GEAR 01.32.43 Rev10 30 JUN 1
32 LANDING GEAR 01.32.44 Rev 07 12 FEB 1
32 LANDING GEAR 01.32.45 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.46 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.47 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.48 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.49 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.50 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.51 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.52 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.53 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.54 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.55 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.56 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.57 Rev 10 30 JUN 1
32 LANDING GEAR 01.32.58 Rev 10 30 JUN 1
33 LIGHTS 01.33.01 Rev07 12 FEB 1233 LIGHTS 01.33.02 Rev07 12 FEB 12
30 JUN 12
MEL/CDL MANUAL
A320/321MEL/CDL 00.03
LIST OF EFFECTIVE PAG
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 23/763
SYSTEM PAGE REV NO. DATE
33 LIGHTS 01.33.03 Rev 10 30 JUN 12
33 LIGHTS 01.33.04 Rev 07 12 FEB 12
33 LIGHTS 01.33.05 Rev 07 12 FEB 12
33 LIGHTS 01.33.06 Rev 07 12 FEB 12
33 LIGHTS 01.33.07 Rev 10 30 JUN 12
33 LIGHTS 01.33.08 Rev 07 12 FEB 12
33 LIGHTS 01.33.09 Rev 07 12 FEB 12
33 LIGHTS 01.33.10 Rev 07 12 FEB 12
33 LIGHTS 01.33.11 Rev 07 12 FEB 12
33 LIGHTS 01.33.12 Rev 07 12 FEB 12
34 NAVIGATION 01.34.01 Rev 07 12 FEB 12
34 NAVIGATION 01.34.02 Rev 07 12 FEB 12
34 NAVIGATION 01.34.03 Rev 07 12 FEB 12
34 NAVIGATION 01.34.04 Rev 07 12 FEB 12
34 NAVIGATION 01.34.05 Rev 07 12 FEB 12
34 NAVIGATION 01.34.06 Rev 07 12 FEB 12
34 NAVIGATION 01.34.07 Rev 07 12 FEB 12
34 NAVIGATION 01.34.08 Rev 07 12 FEB 12
34 NAVIGATION 01.34.09 Rev 07 12 FEB 12
34 NAVIGATION 01.34.10 Rev 07 12 FEB 12
34 NAVIGATION 01.34.11 Rev 07 12 FEB 12
34 NAVIGATION 01.34.12 Rev 07 12 FEB 12
34 NAVIGATION 01.34.13 Rev 09 01 MAY 1234 NAVIGATION 01.34.14 Rev 07 12 FEB 12
34 NAVIGATION 01.34.15 Rev 07 12 FEB 12
34 NAVIGATION 01.34.16 Rev 07 12 FEB 12
34 NAVIGATION 01.34.17 Rev 07 12 FEB 12
34 NAVIGATION 01.34.18 Rev 07 12 FEB 12
34 NAVIGATION 01.34.19 Rev 07 12 FEB 12
34 NAVIGATION 01.34.20 Rev 07 12 FEB 12
34 NAVIGATION 01.34.21 Rev 07 12 FEB 12
34 NAVIGATION 01.34.22 Rev 07 12 FEB 12
34 NAVIGATION 01.34.23 Rev 07 12 FEB 12
34 NAVIGATION 01.34.24 Rev 07 12 FEB 12
34 NAVIGATION 01.34.25 Rev 07 12 FEB 12
34 NAVIGATION 01.34.26 Rev 10 30 JUN 12
34 NAVIGATION 01.34.27 Rev 10 30 JUN 12
34 NAVIGATION 01.34.28 Rev 10 30 JUN 12
34 NAVIGATION 01.34.29 Rev 10 30 JUN 12
34 NAVIGATION 01.34.30 Rev 10 30 JUN 12
34 NAVIGATION 01.34.31 Rev 10 30 JUN 12
00.03.16
LIST OF EFFECTIVE PAGES
A320/321MEL/CDL 30 JUN 12
MEL/CDL MANUAL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 24/763
SYSTEM PAGE REV NO. DATE
35 OXYGEN 01.35.01 Rev 07 12 FEB 1
35 OXYGEN 01.35.02 Rev 07 12 FEB 1
35 OXYGEN 01.35.03 Rev 07 12 FEB 1
35 OXYGEN 01.35.04 Rev 07 12 FEB 1
35 OXYGEN 01.35.05 Rev 07 12 FEB 1
35 OXYGEN 01.35.06 Rev 07 12 FEB 1
35 OXYGEN 01.35.07 Rev 07 12 FEB 1
35 OXYGEN 01.35.08 Rev 07 12 FEB 1
36 PNEUMATIC 01.36.01 Rev 07 12 FEB 1
36 PNEUMATIC 01.36.02 Rev 07 12 FEB 12
36 PNEUMATIC 01.36.03 Rev 09 01 MAY 12
36 PNEUMATIC 01.36.04 Rev 09 01 MAY 12
36 PNEUMATIC 01.36.05 Rev 09 01 MAY 12
36 PNEUMATIC 01.36.06 Rev 07 12 FEB 12
36 PNEUMATIC 01.36.07 Rev 07 12 FEB 1
36 PNEUMATIC 01.36.08 Rev 07 12 FEB 1
36 PNEUMATIC 01.36.09 Rev 07 12 FEB 1
36 PNEUMATIC 01.36.10 Rev 07 12 FEB 1
36 PNEUMATIC 01.36.11 Rev 07 12 FEB 1
36 PNEUMATIC 01.36.12 Rev 07 12 FEB 1
38 WATER/WASTE 01.38.01 Rev 07 12 FEB 12
38 WATER/WASTE 01.38.02 Rev 09 01 MAY 12
46 INFORMATION SYSTEM 01.46.01 Rev 07 12 FEB 1246 INFORMATION SYSTEM 01.46.02 Rev 07 12 FEB 1
47 INERT GAS SYSTEM 01.47.01 Rev 07 12 FEB 1
47 INERT GAS SYSTEM 01.47.02 Rev 07 12 FEB 1
49 AIRBORNE AUXILIARYPOWER 01.49.01 Rev 07 12 FEB 1
49 AIRBORNE AUXILIARYPOWER 01.49.02 Rev 07 12 FEB 1
52 DOORS 01.52.01 Rev 07 12 FEB 1
52 DOORS 01.52.02 Rev 07 12 FEB 1
52 DOORS 01.52.03 Rev 07 12 FEB 1
52 DOORS 01.52.04 Rev 07 12 FEB 1
52 DOORS 01.52.05 Rev 07 12 FEB 1
52 DOORS 01.52.06 Rev 07 12 FEB 1
52 DOORS 01.52.07 Rev 07 12 FEB 1
52 DOORS 01.52.08 Rev 07 12 FEB 1
52 DOORS 01.52.09 Rev 07 12 FEB 1
52 DOORS 01.52.10 Rev 07 12 FEB 1
01 MAY 12
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52 DOORS 01.52.11 Rev 07 12 FEB 12
52 DOORS 01.52.12 Rev 07 12 FEB 12
52 DOORS 01.52.13 Rev 07 12 FEB 12
52 DOORS 01.52.14 Rev 07 12 FEB 12
52 DOORS 01.52.15 Rev 07 12 FEB 12
52 DOORS 01.52.16 Rev 07 12 FEB 12
52 DOORS 01.52.17 Rev 07 12 FEB 12
52 DOORS 01.52.18 Rev 07 12 FEB 12
52 DOORS 01.52.19 Rev 07 12 FEB 12
52 DOORS 01.52.20 Rev 07 12 FEB 12
52 DOORS 01.52.21 Rev 07 12 FEB 12
52 DOORS 01.52.22 Rev 07 12 FEB 12
52 DOORS 01.52.23 Rev 07 12 FEB 12
52 DOORS 01.52.24 Rev 07 12 FEB 12
52 DOORS 01.52.25 Rev 07 12 FEB 12
52 DOORS 01.52.26 Rev 07 12 FEB 12
52 DOORS 01.52.27 Rev 07 12 FEB 12
52 DOORS 01.52.28 Rev 07 12 FEB 12
52 DOORS 01.52.29 Rev 07 12 FEB 12
52 DOORS 01.52.30 Rev 07 12 FEB 12
52 DOORS 01.52.31 Rev 07 12 FEB 12
52 DOORS 01.52.32 Rev 07 12 FEB 12
52 DOORS 01.52.33 Rev 07 12 FEB 1252 DOORS 01.52.34 Rev 07 12 FEB 12
52 DOORS 01.52.35 Rev 07 12 FEB 12
52 DOORS 01.52.36 Rev 07 12 FEB 12
52 DOORS 01.52.37 Rev 09 01 MAY 12
52 DOORS 01.52.38 Rev 07 12 FEB 12
56 WINDOWS 01.56.01 Rev 07 12 FEB 12
56 WINDOWS 01.56.02 Rev 07 12 FEB 12
56 WINDOWS 01.56.03 Rev 07 12 FEB 12
56 WINDOWS 01.56.04 Rev 07 12 FEB 12
70 ENGINES 01.70.01 Rev 07 12 FEB 12
70 ENGINES 01.70.02 Rev 07 12 FEB 12
73 ENGINE FUEL AND CONTROL 01.73.01 Rev 07 12 FEB 12
73 ENGINE FUEL AND CONTROL 01.73.02 Rev 07 12 FEB 12
73 ENGINE FUEL AND CONTROL 01.73.03 Rev 10 30 JUN 12
73 ENGINE FUEL AND CONTROL 01.73.04 Rev 10 30 JUN 12
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74 IGNITION 01.74.01 Rev 07 12 FEB 1
74 IGNITION 01.74.02 Rev 07 12 FEB 1
74 IGNITION 01.74.03 Rev 07 12 FEB 1
74 IGNITION 01.74.04 Rev 07 12 FEB 1
76 ENGINE CONTROLS 01.76.01 Rev 07 12 FEB 1
76 ENGINE CONTROLS 01.76.02 Rev 07 12 FEB 1
77 ENGINE INDICATING 01.77.01 Rev 07 12 FEB 1
77 ENGINE INDICATING 01.77.02 Rev 07 12 FEB 1
77 ENGINE INDICATING 01.77.03 Rev 07 12 FEB 1
77 ENGINE INDICATING 01.77.04 Rev 07 12 FEB 1
77 ENGINE INDICATING 01.77.05 Rev 07 12 FEB 1
77 ENGINE INDICATING 01.77.06 Rev 07 12 FEB 1
78 EXHAUST 01.78.01 Rev 07 12 FEB 1
78 EXHAUST 01.78.02 Rev 07 12 FEB 1
78 EXHAUST 01.78.03 Rev 07 12 FEB 1
78 EXHAUST 01.78.04 Rev 07 12 FEB 1
78 EXHAUST 01.78.05 Rev 07 12 FEB 1
78 EXHAUST 01.78.06 Rev 07 12 FEB 1
79 OIL 01.79.01 Rev 07 12 FEB 1
79 OIL 01.79.02 Rev 07 12 FEB 1
79 OIL 01.79.03 Rev 07 12 FEB 1
79 OIL 01.79.04 Rev 07 12 FEB 1
80 STARTING 01.80.01 Rev 07 12 FEB 180 STARTING 01.80.02 Rev 07 12 FEB 1
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CONFIGURATION DEVIATION LIST - SECTION 02
TABLE OF CONTENTS 02.00.01 Rev 07 12 FEB 12
TABLE OF CONTENTS 02.00.02 Rev 07 12 FEB 12
TABLE OF CONTENTS 02.00.03 Rev 07 12 FEB 12
TABLE OF CONTENTS 02.00.04 Rev 07 12 FEB 12
CDL INTRODUCTION 02.01.01 Rev 07 12 FEB 12
CDL INTRODUCTION 02.01.02 Rev 07 12 FEB 12
21 AIR CONDITIONING 02.21.01 Rev 07 12 FEB 12
21 AIR CONDITIONING 02.21.02 Rev 07 12 FEB 12
23 COMMUNICATIONS 02.23.01 Rev 07 12 FEB 12
23 COMMUNICATIONS 02.23.02 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.01 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.02 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.03 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.04 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.05 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.06 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.07 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.08 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.09 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.10 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.11 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.12 Rev 07 12 FEB 1227 FLIGHT CONTROLS 02.27.13 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.14 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.15 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.16 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.17 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.18 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.19 Rev 07 12 FEB 12
27 FLIGHT CONTROLS 02.27.20 Rev 07 12 FEB 12
28 FUEL 02.28.01 Rev 07 12 FEB 12
28 FUEL 02.28.02 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 02.30.01 Rev 07 12 FEB 12
30 ICE AND RAIN PROTECTION 02.30.02 Rev 07 12 FEB 12
32 LANDING GEAR 02.32.01 Rev 07 12 FEB 12
32 LANDING GEAR 02.32.02 Rev 07 12 FEB 12
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33 LIGHTS 02.33.01 Rev 07 12 FEB 1
33 LIGHTS 02.33.02 Rev 07 12 FEB 1
33 LIGHTS 02.33.03 Rev 07 12 FEB 1
33 LIGHTS 02.33.04 Rev 07 12 FEB 1
33 LIGHTS 02.33.05 Rev 07 12 FEB 1
33 LIGHTS 02.33.06 Rev 07 12 FEB 1
33 LIGHTS 02.33.07 Rev 07 12 FEB 1
33 LIGHTS 02.33.08 Rev 07 12 FEB 1
33 LIGHTS 02.33.09 Rev 07 12 FEB 1
33 LIGHTS 02.33.10 Rev 07 12 FEB 1
49 APU 02.49.01 Rev 07 12 FEB 1
49 APU 02.49.02 Rev 07 12 FEB 1
51 STRUCTURE 02.51.01 Rev 07 12 FEB 1
51 STRUCTURE 02.51.02 Rev 07 12 FEB 1
51 STRUCTURE 02.51.03 Rev 07 12 FEB 1
51 STRUCTURE 02.51.04 Rev 07 12 FEB 1
52 DOORS 02.52.01 Rev 07 12 FEB 1
52 DOORS 02.52.02 Rev 07 12 FEB 1
52 DOORS 02.52.03 Rev 07 12 FEB 1
52 DOORS 02.52.04 Rev 07 12 FEB 1
52 DOORS 02.52.05 Rev 07 12 FEB 1
52 DOORS 02.52.06 Rev 07 12 FEB 1
52 DOORS 02.52.07 Rev 07 12 FEB 152 DOORS 02.52.08 Rev 07 12 FEB 1
52 DOORS 02.52.09 Rev 07 12 FEB 1
52 DOORS 02.52.10 Rev 07 12 FEB 1
52 DOORS 02.52.11 Rev 07 12 FEB 1
52 DOORS 02.52.12 Rev 07 12 FEB 1
52 DOORS 02.52.13 Rev 07 12 FEB 1
52 DOORS 02.52.14 Rev 07 12 FEB 1
52 DOORS 02.52.15 Rev 07 12 FEB 1
52 DOORS 02.52.16 Rev 07 12 FEB 1
52 DOORS 02.52.17 Rev 07 12 FEB 1
52 DOORS 02.52.18 Rev 07 12 FEB 1
52 DOORS 02.52.19 Rev 07 12 FEB 1
52 DOORS 02.52.20 Rev 07 12 FEB 1
52 DOORS 02.52.21 Rev 07 12 FEB 1
52 DOORS 02.52.22 Rev 07 12 FEB 1
52 DOORS 02.52.23 Rev 07 12 FEB 1
52 DOORS 02.52.24 Rev 07 12 FEB 1
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52 DOORS 02.52.25 Rev 07 12 FEB 12
52 DOORS 02.52.26 Rev 07 12 FEB 12
52 DOORS 02.52.27 Rev 07 12 FEB 12
52 DOORS 02.52.28 Rev 07 12 FEB 12
52 DOORS 02.52.29 Rev 07 12 FEB 12
52 DOORS 02.52.30 Rev 07 12 FEB 12
52 DOORS 02.52.31 Rev 07 12 FEB 12
52 DOORS 02.52.32 Rev 07 12 FEB 12
52 DOORS 02.52.33 Rev 07 12 FEB 12
52 DOORS 02.52.34 Rev 07 12 FEB 12
52 DOORS 02.52.35 Rev 07 12 FEB 12
52 DOORS 02.52.36 Rev 07 12 FEB 12
52 DOORS 02.52.37 Rev 07 12 FEB 12
52 DOORS 02.52.38 Rev 07 12 FEB 12
53 FUSELAG 02.53.01 Rev 07 12 FEB 12
53 FUSELAG 02.53.02 Rev 07 12 FEB 12
53 FUSELAG 02.53.03 Rev 07 12 FEB 12
53 FUSELAG 02.53.04 Rev 07 12 FEB 12
54 NACELLES / PYL 02.54.01 Rev 07 12 FEB 12
54 NACELLES / PYL 02.54.02 Rev 07 12 FEB 12
54 NACELLES / PYL 02.54.03 Rev 07 12 FEB 12
54 NACELLES / PYL 02.54.04 Rev 07 12 FEB 12
54 NACELLES / PYL 02.54.05 Rev 07 12 FEB 1254 NACELLES / PYL 02.54.06 Rev 07 12 FEB 12
54 NACELLES / PYL 02.54.07 Rev 07 12 FEB 12
54 NACELLES / PYL 02.54.08 Rev 07 12 FEB 12
57 NACELLES / PYL 02.57.01 Rev 07 12 FEB 12
57 NACELLES / PYL 02.57.02 Rev 07 12 FEB 12
57 NACELLES / PYL 02.57.03 Rev 07 12 FEB 12
57 NACELLES / PYL 02.57.04 Rev 07 12 FEB 12
71 POWER PLANT 02.71.01 Rev 07 12 FEB 12
71 POWER PLANT 02.71.02 Rev 07 12 FEB 12
78 EXHAUST 02.78.01 Rev 07 12 FEB 12
78 EXHAUST 02.78.02 Rev 07 12 FEB 12
* * *
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ITEM PAG
MEL TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.00.0
FAA MMEL Preamble . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.0
Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.0ECAM General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.02.0
ECAM Messages Cross Reference List. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.03.0
ATA 21 - AIR CONDITIONING
21-00-03 AFT CRG HEAT MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-00-04 TEMP CTL 1(2) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-01-01 AIR COND Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-01-02 CABIN PRESS Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-01-03 CARGO VENT Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-01-04 VENTILATION Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-07-01 Indications on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-07-02 Indications on the CAB PRESS SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-07-03 Indications on the COND SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-07-04 Indications on the CRUISE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-09-01 VENT BLOWER FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-09-02 VENT EXTRACT FAULT Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-09-03 CAB PR SAFETY VALVE OPEN Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-21-01 Cabin Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-23-01 Lavatory and Galley Extraction Fan. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0
21-26-01 Avionics Blower Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.1
21-26-02 Avionics Extract Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.1
21-26-03 Avionics Skin Exchanger Inlet Bypass Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2
21-26-04 Avionics Skin Air Outlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2
21-26-05 Avionics Skin Air Inlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2
21-26-06 Avionics Skin Exchanger Isolation Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2
21-26-07 Avionics Skin Exchanger Outlet Bypass Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2
21-26-08 Avionics Air Conditioning Inlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2
21-26-09 Avionics Ventilation Filte . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3
21-26-10 Avionics Equipment Ventilation Computer (AEVC) . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3
21-28-03 AFT Cargo Extraction Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3
21-28-04 AFT Cargo Isolation Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3
21-31-01 Automatic Cabin Pressure Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .(CPC, Outflow Valve AUTO Channel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.37
21-31-02 Manual Cabin Pressure Control System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(MAN V/S CTL selector, Outflow Valve MAN Channel). . . . . . . . . . . . . . . . . . . . . 01.21.3
21-31-03 Pressure Safety Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.4
21-31-04 Landing Elevation Selection AUTO Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.4
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ITEM PAGE
ATA 21 - AIR CONDITIONING (Cont’d)
21-31-05 Landing Elevation Selection MAN Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.41
21-43-02 AFT Cargo Compartment Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.41
21-51-02 Pack Flow Selection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.43
21-51-03 Pack Flow Sensor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.43
21-52-01 Air Conditioning Pack. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.46
21-52-02 Air Conditioning Pack Ram Air Inlet Flap. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.47
21-55-01 Emergency Ram Air Inlet. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.48
21-61-01 Pack Turbine Bypass Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.49
21-63-02 Cockpit and Cabin Trim Air Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.49
21-63-03 Hot Air Pressure Regulating Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.50
21-63-04 Air Conditioning System Controller Channel (COND CTL 1(2)-A(B)) . . . . . . . . . . 01.21.52
ATA 22 - AUTO FLIGHT
22-01-01 FAC pb-sw FAULT light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01
22-01-02 FAC pb-sw OFF light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01
22-05-01 AP Related Indications on the FMA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01
22-05-02 A/THR Related Indications on the FMA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01
22-05-03 Approach and Landing Capabilities on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02
22-05-04 Special Messages on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02
22-10-01 Autopilot (AP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02
22-10-02 Flight Director (FD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.0322-10-03 Take-over pb Priority Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.03
22-10-04 Take-over pb AP Disconnection Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.04
22-10-05 AUTO LAND lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.05
22-10-06 AP Disengagement Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.05
22-10-07 Sticks and Rudder Pedals Locking Solenoid in AP Mode . . . . . . . . . . . . . . . . . . . 01.22.05
22-30-01 Autothrust (A/THR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.06
22-30-02 Autothrust Instinctive Disconnect pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.06
22-30-03 Autothrust Disengagement Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.09
22-60-01 FAC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.10
22-60-02 FAC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.11
22-60-03 Windshear Detection System Predictive . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.12
22-60-04 Yaw Damper System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.13
22-70-01 Flight Management System (FMS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.13
22-70-02 Navigation Database . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.14
22-70-03 Performance Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.15
22-70-04 Fuel/Time Prediction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.15
01.00.02TABLE OF CONTENTS
A320/321MEL/CDL
01 MAY 12MEL
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ITEM PAG
ATA 22 - AUTO FLIGHT( cont’d)
22-81-01 Auto Flight Control Panel (FCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.1
22-81-02 EFIS Control Panel (FCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.1
22-81-03 FCU Channel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2
22-82-01 MCDU 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2
22-82-02 MCDU 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2
22-82-04 MCDU Annunciator light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2
22-83-01 Flight Management and Guidance Computer (FMGC) . . . . . . . . . . . . . . . . . . . . . 01.22.2
ATA 23 - COMMUNICATIONS
23-00-01 CIDS 1(2) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.023-01-01 RCDR Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-01-02 CALLS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-09-01 COM HF 1(2) EMITTING Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-09-02 COM VHF 1(2)(3) EMITTING Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-10-01 HF System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-10-02 VHF System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-10-03 SATCOM Voice Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-13-01 Radio Management Panel (RMP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-13-02 RMP Selection Key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-20-01 Aircraft Communications Addressing Reporting System (ACARS) . . . . . . . . . . . 01.23.0
23-20-02 SATCOM Data Mode. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.023-31-01 Passenger Address System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-40-01 Mechanical Call Horn. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-40-02 Flight Crew Interphone System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-40-03 Flight Crew to Ground Communication System. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-40-04 Service Interphone Jack . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-51-01 SELCAL Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-51-02 Boomset. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-51-03 Hand Microphone. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-51-04 Cockpit Loudspeaker. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-51-05 Cockpit Loudspeaker Volume Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0
23-51-06 Sidestick Radio selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.1
23-52-01 CAPT and F/O ACP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.1
23-52-02 ACP 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.1
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ITEM PAGE
ATA 23 - COMMUNICATIONS ( cont’d)
23-52-03 Fourth Occupant ACP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11
23-52-04 ACP in the Avionics Compartment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11
23-52-05 ACP Transmission Key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11
23-52-06 ACP Reception knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11
23-52-07 ACP Reception knob light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11
23-53-01 AUDIO SWITCHING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12
23-71-01 Cockpit Voice Recorder (CVR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12
23-72-01 Cockpit Door Surveillance System (CDSS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12
23-73-01 Cabin Intercommunication Data System (CIDS) . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.14
23-73-02 DEU A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.15
23-73-03 DEU B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.16
23-73-04 Cabin Individual Call . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.18
23-73-05 Cabin Loudspeaker . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.18
23-73-06 Handset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.19
23-73-07 Prerecorded Announcement and Music Reproducer (PRAM) . . . . . . . . . . . . . . . 01.23.20
23-73-08 Cabin Assignment Module (CAM) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.21
23-73-10 Smoke Detection Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.21
23-74-01 FAP Display Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23
23-74-02 EMER pb on Hardkey FAP Sub-panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23
23-74-03 Other Controls on Hardkey FAP Sub-panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23
23-74-06 Door Bottle Pressure Monitoring on the FAP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23
23-74-08 Slide Pressure Monitoring on the FAP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24
23-74-09 Area Call Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24
23-74-10 Attendant Information Panel (AIP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24
23-74-11 Additional Attendant Panel (AAP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24
01.00.04TABLE OF CONTENTS
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ITEM PAG
ATA 24 - ELECTRICAL POWER
24-00-01 DC BUS TIE MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-00-03 AC GEN MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-01-01 ELEC Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-01-02 EMER ELEC PWR Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-07-01 AC Generation Indications on the ELEC SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-07-02 DC Generation Indications on the ELEC SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-07-03 AC ESS BUS SHED Indication on the ELEC SD page . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-09-01 ELEC AC ESS BUS SHED Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-09-02 C/B TRIPPED Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-22-01 AC Main Generation (IDG, GCU, Line Contactor) . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0
24-22-02 AC Bus Tie Control Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-23-01 AC Auxiliary Generation (APU Generator, GCU, Line Contactor) . . . . . . . . . . . . . 01.24.1
24-24-01 Emergency Generator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-24-02 RAT Extension Automatic Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-24-03 RAT Extension Manual Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-25-01 Manual Transfer to the AC BUS 2 (ALTN Function) . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-25-02 Automatic Transfer to the AC BUS 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-26-01 GALY & CAB Automatic Load Shed System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-26-02 GALY & CAB Manual Load Shed System (GALY & CAB pb-sw) . . . . . . . . . . . . . 01.24.1
24-26-03 Commercial Supply System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-28-01 Static Inverter AC Generation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-32-01 DC Main Generation (TR 1, TR 2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-34-01 DC Emergency Generation (ESS TR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-35-01 DC TIE Contactor 1PC1 (DC BUS 1-DC BAT BUS), . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4PC (DC ESS BUSDC BAT BUS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-35-02 DC TIE Contactor 1PC2 (DC BUS 2-DC BAT BUS) . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-38-01 BAT 1(2) Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-38-02 Battery Charger Limiter (BCL) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-38-03 Battery Voltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1
24-41-01 Ground Power Control Unit (GPCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.2
24-41-02 External Power Receptacle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.2
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ITEM PAGE
ATA 25 - EQUIPMENT / FURNISHINGS
25-07-01 Passenger Door Slide Permanently Indicated Armed (A320) . . . . . . . . . . . . . . . . 01.25.01
25-07-01 Cabin Passenger Door / Emergency Exit Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Permanently Indicated Armed (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.01
25-07-02 Passenger Door Slide Permanently Indicated Not Armed (A320) . . . . . . . . . . . . . 01.25.02
25-07-02 Cabin Passenger Door / Emergency Exit Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Permanently Indicated Not Armed (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.02
25-07-03 Emergency Exit Slide Permanently Indicated Armed . . . . . . . . . . . . . . . . . . . . . . 01.25.03
25-07-04 Emergency Exit Slide Permanently Indicated Not Armed . . . . . . . . . . . . . . . . . . . 01.25.03
25-11-01 Pilot Seat Manual Horizontal Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04
25-11-02 Pilot Seat Manual Vertical Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04
25-11-03 Pilot Seat Recline Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04
25-11-04 Pilot Seat Other Manual Adjustments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04
25-11-05 Pilot Seat Electrical Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.05
25-11-06 Pilot Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.05
25-11-07 Pilot Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06
25-11-08 Pilot Sidestick Armrest Height Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06
25-11-09 Pilot Sidestick Armrest Pitch Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06
25-11-10 Pilot Sidestick Armrest Memory Position Display . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06
25-11-11 Pilot Inboard Armrest Vertical Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07
25-11-12 Pilot Seat Headrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07
25-12-01 Third Occupant Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07
25-12-02 Third Occupant Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07
25-12-03 Third Occupant Seat Abdominal Belt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08
25-12-04 Third Occupant Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08
25-12-05 Fourth Occupant Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08
25-12-06 Fourth Occupant Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08
25-12-07 Fourth Occupant Seat Abdominal Belt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08
25-12-08 Fourth Occupant Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09
25-13-01 Pilot Sliding Table . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09
25-13-02 Pilot Retractable Footrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09
25-20-01 Passenger Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09
25-20-03 Cabin Attendant Seat. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.10
25-28-01 Overhead Storage Bin(s)/Cabin and Galley storage Compartment/ Closest. . . . . 01.25.12
25-35-01 Galley Waste Compartment Flapper Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.12
25-40-01 Toilet Waste Compartment Flapper Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.13
01.00.06TABLE OF CONTENTS
A320/321MEL/CDL
12 FEB 12MEL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 36/763
ITEM PAG
ATA 25 - EQUIPMENT / FURNISHINGS ( cont’d)
25-40-02 Exterior Lavatory Ashtray. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-40-03 Interior Lavatory Ashtray . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-50-01 Cargo Loading System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-50-02 Decompression Panels in the Cargo Compartments. . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-50-03 Sidewall Linings and Ceiling Panels in the Cargo Compartments. . . . . . . . . . . . . 01.25.1
25-50-04 Cargo Compartment Restraint Components (Nets, Attach Points, Stanchions) . . 01.25.1
25-62-01 Cabin Passenger Door Slide or Slide Raft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-62-02 Overwing Emergency Exit Slide or Slide Raft (A320) . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-62-03 Emergency Exit Slide or Slide Raft (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-62-04 SLIDE ARMED light (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-62-04 SLIDE ARMED light (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-62-05 Survival Kit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-62-06 Passenger Door CHECK SLIDE PRESSURE Message on . . . . . . . . . . . . . . . . . . . . . . .
Flight Attendant Panel (FAP) (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.17
25-62-06 Passenger Door CHECK SLIDE PRESSURE Message on . . . . . . . . . . . . . . . . . . . . . . .
Flight Attendant Panel (FAP) (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.18
25-62-07 Overwing Emergency Exit CHECK SLIDE PRESSURE . . . . . . . . . . . . . . . . . . . . . . . . . .
Message on Flight Attendant Panel (FAP) (A320). . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-62-08 Overwing Escape Life Line . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1
25-63-01 Emergency Evacuation Signaling System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(COMMAND pbsw, HORN SHUT OFF pb, CAPT&PURS and CAPT sw). . . . . . . 01.25.1
25-64-01 First Aid Kit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-64-02 Emergency Medical Kit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.225-64-03 Automated External Defibrillator (AED) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-65-01 Cockpit Flashlight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-65-02 Cabin Flashlight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-65-03 Crash Axe/Crowbar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-65-04 Emergency Locator Transmitter (ELT). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-65-05 Fireproof Gloves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-65-06 Megaphone . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-66-01 Life Vest. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-66-02 Supplementary Life Raft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-70-01 Non-Essential Equipment & furnishings (NEF) . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
25-70-04 Movie/stereo Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.225-70-05 Overhead Reading Lamp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2
30 JUN 12MEL
A320/321MEL/CDL
01.00TABLE OF CONTEN
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 37/763
ITEM PAGE
ATA 26 - FIRE PROTECTION
26-00-01 SMOKE MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01
26-01-01 FIRE Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01
26-01-02 CARGO SMOKE Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05
26-12-01 Engine Fire Detection Loop A on the Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05
26-12-02 Engine Fire Detection Loop A on the Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05
26-12-03 Engine Fire Detection Loop B on the Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06
26-12-04 Engine Fire Detection Loop B on the Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06
26-12-05 FIRE light on the ENG MASTER Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06
26-13-01 APU Fire Detection Loop A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06
26-13-02 APU Fire Detection Loop B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.07
26-15-01 Avionics Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.07
26-16-01 Smoke Detector in the FWD Cargo Compartment (A320). . . . . . . . . . . . . . . . . . . 01.26.08
26-16-01 Smoke Detector in the FWD Cargo Compartment (A321). . . . . . . . . . . . . . . . . . . 01.26.09
26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments (A321). . . . . . . 01.26.10
26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments (A320). . . . . . . 01.26.11
26-17-01 Lavatory Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.12
26-22-01 APU Automatic Fire Extinguishing Control on Ground . . . . . . . . . . . . . . . . . . . . . 01.26.13
26-22-02 APU Fire Extinguisher Overpressure Indication (Red Disc) . . . . . . . . . . . . . . . . . 01.26.14
26-22-03 Squib of the APU Fire Extinguisher Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.15
26-22-04 APU Fire Extinguisher Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.15
26-22-05 APU AUTO EXTING TEST pb-sw on the Maintenance Panel. . . . . . . . . . . . . . . . 01.26.16
26-22-06 APU FIRE light on the External Power Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.16
26-22-07 APU SHUT OFF pb on the External Power Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.17
26-23-01 Cargo Agent Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.17
26-23-02 Squib of the Cargo Bottle 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.19
26-24-01 Portable Fire Extinguisher . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.19
26-25-01 Lavatory Waste Bin Fire Extinguishing System . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.20
01.00.08TABLE OF CONTENTS
A320/321MEL/CDL
01 MAY 12MEL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 38/763
ITEM PAG
ATA 27 - FLIGHT CONTROLS
27-00-01 F/CTL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-00-02 SFCS MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-01-01 FLT CTL Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-01 Aileron Actuator Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-02 Aileron Position Indication on the F/CTL SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-03 Elevator Actuator Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-04 Elevator Position Indication on the F/CTL SD page. . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-05 Pitch Trim Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-06 Rudder Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-07 Rudder Trim Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-08 Rudder Travel Limiter Position Indication on the F/CTL SD page . . . . . . . . . . . . . 01.27.0
27-07-09 ELAC Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-10 SEC Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0
27-07-11 Spoilers/ Speed brakes Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . 01.27.1
27-07-12 Spoilers/ Speed brakes Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . 01.27.1
27-08-01 Flap Position Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-08-02 Slat Position Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-14-01 Left Aileron Blue Servo-Control (Controlled by ELAC 1) . . . . . . . . . . . . . . . . . . . . 01.27.1
27-14-02 Left Aileron Green Servo- Control (Controlled by ELAC 2) . . . . . . . . . . . . . . . . . . 01.27.1
27-14-03 Right Aileron Green Servo- Control (Controlled by ELAC 1) . . . . . . . . . . . . . . . . . 01.27.1
27-14-04 Right Aileron Blue Servo- Control (Controlled by ELAC 2) . . . . . . . . . . . . . . . . . . 01.27.1
27-21-01 Rudder Pedal Adjustment System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-22-01 Rudder Trim System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-22-02 Manual Rudder Trim Reset Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-22-03 Rudder Trim Position Indication on the Center Pedestal. . . . . . . . . . . . . . . . . . . . 01.27.1
27-23-01 Rudder Travel Limiter System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-34-01 Elevator Servo Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-34-02 Elevator Servo Control Position Transducer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-40-01 Stabilizer Mechanical Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-40-02 Stabilizer Actuator Electrical Motor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1
27-51-01 SFCC Flap Channel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2
27-51-02 SFCC Slat Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2
27-51-03 Flap Wing Tip Brakes Solenoid . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.227-54-01 Flap Hydraulic Motor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2
27-54-02 Flap PCU Valve Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2
27-54-03 Flap Pressure Off Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2
27-64-01 Spoiler 5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2
27-64-02 Spoiler 1 or 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2
30 JUN 12MEL
A320/321MEL/CDL
01.00TABLE OF CONTEN
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 39/763
ITEM PAGE
ATA 27 - FLIGHT CONTROLS (Cont’d)
27-64-03 Spoiler 2 or 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.25
27-64-04 Spoilers 1 and 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.26
27-64-05 Spoilers 3 and 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.29
27-81-01 Slat Wing Tip Brakes Solenoids. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30
27-84-01 Slats Hydraulic Motor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30
27-84-02 Slat PCU Valve Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30
27-84-03 Slat Pressure- Off Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30
27-92-01 Speed brake Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.31
27-92-02 Ground Spoiler Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.34
27-92-03 SIDESTICK PRIORITY light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35
27-92-04 Sidestick Dual Input Visual Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35
27-92-05 Sidestick Dual Input Aural Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35
27-93-01 ELAC 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35
27-93-02 ELAC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.44
27-93-03 Pitch Normal Law. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.45
27-94-01 SEC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.45
27-94-02 SEC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.51
27-94-03 SEC 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.55
27-95-01 FCDC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.57
27-95-02 FCDC 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.57
ATA 28 - FUEL
28-00-01 FUEL MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01
28-01-01 FUEL Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01
28-07-01 Fuel Quantity Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.05
28-07-02 Fuel Temperature Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . 01.28.22
28-07-03 Tank Pump Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.23
28-07-04 Valve Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.23
28-09-01 FUEL L(R) INNER(OUTER) TK HI TEMP Alert (A320) . . . . . . . . . . . . . . . . . . . . . 01.28.27
28-09-01 FUEL L(R) WING TK HI TEMP Alert (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.28
28-09-02 FUEL L(R) INNER(OUTER) TK LO TEMP Alert (A320) . . . . . . . . . . . . . . . . . . . . 01.28.30
28-09-02 FUEL L(R) WING TK LO TEMP Alert (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.31
28-09-03 FUEL ACT XFR FAULT Alert (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.33
28-12-01 Overpressure Protector between Inner and Outer Tank (A320) . . . . . . . . . . . . . . 01.28.33
28-12-02 Overpressure Protector in Vent Surge Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36
28-12-03 Overpressure Protector in The Inner Tank (A320). . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36
28-12-03 Overpressure Protector in The Wing Tank (A321). . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36
01.00.10TABLE OF CONTENTS
A320/321MEL/CDL
30 JUN 12MEL
7/23/2019 A 320321 Mel Cdl
http://slidepdf.com/reader/full/a-320321-mel-cdl 40/763
ITEM PAG
ATA 28 - FUEL (Cont’d )
28-12-04 Overpressure Protector between Center and Inner Tank (A320) . . . . . . . . . . . . . 01.28.3
28-12-04 Overpressure Protector between Center and Wing Tank (A321) . . . . . . . . . . . . . 01.28.3
28-12-05 Overpressure Protector in the ACT (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . 01.28.3
28-15-01 LH Wing Transfer Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.3
28-15-02 RH Wing Transfer Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.3
28-20-01 Automatic Fuel Feed System (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-21-01 Wing Tank Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-21-02 Center Tank Pump (A320)(ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-21-02 Center Tank Pump (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-21-03 Wing Tank Pump Sequence Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-22-01 APU Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-23-01 Crossfeed Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-24-01 Engine LP Fuel Valve Electrical Motor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-25-01 Fuel Quantity Preselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-25-02 Fuel Quantity on the Refuel/Defuel Control Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-25-03 Refuel Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-25-04 Transfer Defuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-25-05 Exterior Refuel/Defuel Control Panel (A320 & A321) . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-26-01 Center Tank Transfer Valve (A321). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-28-01 ACT Auto Transfer System (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4
28-28-02 ACT Transfer Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-28-03 ACT Transfer Pump. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-28-04 ACT Air Shutoff Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-28-05 ACT Inward Pressure Relief Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-28-06 ACT Vent Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-28-07 ACT Refuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-28-08 ACT Integrated Impact Wall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-28-09 ACT 1 Inlet Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-29-01 APU LP Fuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-43-01 Manual Magnetic Indicators (A320 & A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5
28-46-01 High Level Detection System in the Inner Tank (A320). . . . . . . . . . . . . . . . . . . . . 01.28.6
28-46-01 High Level Detection System in the Wing Tank (A321). . . . . . . . . . . . . . . . . . . . . 01.28.6
28-46-02 High Level Detection System in the Center Tank (A320) . . . . . . . . . . . . . . . . . . . 01.28.628-46-02 High Level Detection System in the Center Tank (A320) (ACTs) . . . . . . . . . . . . . 01.28.6
28-46-03 High Level Detection System in the ACT (A320) (ACTs). . . . . . . . . . . . . . . . . . . . 01.28.6
28-46-04 Low Level Detection System in the Inner Tank (A320) . . . . . . . . . . . . . . . . . . . . . 01.28.6
28-46-04 Low Level Detection System in the Wing Tank (A321) . . . . . . . . . . . . . . . . . . . . . 01.28.6
28-46-05 Low Level Detection System in the ACT (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . 01.28.6
28-50-01 Fuel Quantity Indicating Computer (FQIC) Channel . . . . . . . . . . . . . . . . . . . . . . . 01.28.6
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ITEM PAGE
ATA 29 - HYDRAULIC POWER
29-01-01 HYD Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.01
29-01-02 Maintenance HYD Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.03
29-07-01 Yellow ELEC Pump Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . 01.29.03
29-07-02 Engine Driven Pump Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . 01.29.03
29-07-03 Fire Valve Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.03
29-07-04 PTU Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04
29-07-05 Reservoir Quantity Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . 01.29.04
29-07-06 RAT Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04
29-07-07 System Label Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04
29-07-08 System Pressure Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.29.06
29-09-01 HYD B(Y) ELEC PUMP LO PR Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08
29-09-02 HYD B(Y) ELEC PUMP OVHT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08
29-09-03 HYD G(Y) ENG 1(2) PUMP LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08
29-09-04 HYD G(B)(Y) RSVR LO AIR PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.10
29-09-05 HYD G(B)(Y) RSVR LO LVL Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.10
29-09-06 HYD G(B)(Y) RSVR OVHT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.11
29-09-07 HYD PTU FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.11
29-09-08 HYD RAT FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.12
29-09-09 HYD G(B)(Y)(B+G)(G+Y) (B+Y) SYS LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . 01.29.12
29-10-01 Engine Driven Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14
29-10-02 Engine Driven Pump Depressurization Function . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14
29-10-03 Blue System Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14
29-10-04 Hydraulic System Accumulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15
29-10-05 Yellow Brake Accumulator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15
29-10-07 Engine Pump Fire Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15
29-10-08 Hydraulic System Filter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15
29-10-09 Hydraulic Case Drain Filter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16
29-22-01 Ram Air Turbine. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16
29-23-01 Power Transfer Unit (PTU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16
29-24-01 Yellow System Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.18
01.00.12TABLE OF CONTENTS
A320/321MEL/CDL
12 FEB 12MEL
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ITEM PAG
ATA 30 - ICE AND RAIN PROTECTION
30-00-01 ICE DETECT MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0
30-01-01 ANTI ICE Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0
30-01-02 Wiper Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0
30-07-01 ANTI ICE Indication on the BLEED SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0
30-07-02 Arrow Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0
30-11-01 Wing Anti-Ice Control Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0
30-21-01 Engine Anti-Ice Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0
30-31-01 Probe Heat Computer (PHC). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1
30-31-02 Pitot Heater . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1
30-31-03 Static Ports Heater. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1
30-31-04 Angle of Attack (AOA) Probes Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1
30-31-05 TAT Probes Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-42-01 Window Heat Computer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-42-02 Fixed Lateral Window and Sliding Window Heating . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-42-03 Windshield Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-42-04 PROBES/ WINDOW HEAT pb-sw AUTO Control . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-42-05 PROBES/WINDOW HEAT pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-45-01 Windshield Wiper. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-45-02 Windshield Wiper PARK Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-45-03 Rain Repellent System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-71-01 Waste Water Drain Mast Heating System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-71-02 Waste Water Drain Line Ice Protection System. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-81-01 Ice Detection System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-81-02 External Visual Icing Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
30-81-03 Lighting of External Visual Icing Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2
ATA 31 - INDICATING / RECORDING SYSTEMS
31-00-01 QAR MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-00-02 ACMS MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-00-03 DAR MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-00-04 CFDIU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-00-05 DMC 1/3 MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-00-06 DMC 2/3 MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-05-01 AP Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-05-02 A/THR Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-05-03 Approach and Landing Capabilities on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-05-04 Special Messages on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
31-05-05 Actual Airspeed Reference Line and Scale Indications on the PFD . . . . . . . . . . . 01.31.0
31-05-06 Mach Number Indication on the PFD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0
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ITEM PAGE
ATA 31 - INDICATING / RECORDING SYSTEMS (Cont’d )
31-05-07 VMO/MMO Characteristic Speed Indication on the PFD. . . . . . . . . . . . . . . . . . . . 01.31.03
31-05-08 Altitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.03
31-05-09 Vertical Speed Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.03
31-05-10 Other Air Data Related Indications on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04
31-05-11 Attitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04
31-05-12 Heading Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04
31-06-01 Ground Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04
31-06-02 True Air Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04
31-06-04 Heading Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05
31-06-05 Position (Aircraft Symbol) Indication on the ND. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05
31-06-06 Navigation Station Information on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05
31-06-07 Chrono Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05
31-07-01 Indications on the System Display pages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05
31-07-02 Permanent Data Indications on the SD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.06
31-08-01 Engine Parameter Indications on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.06
31-08-02 Fuel On Board (FOB) Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07
31-08-03 MEMO Messages on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07
31-08-04 Slats/Flaps Position Indications on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07
31-20-01 Electrical Clock Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07
31-30-01 Centralized Fault Display System (CFDS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.08
31-30-02 Digital AIDS Recorder (DAR). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.08
31-30-03 Digital Flight Data Recorder (DFDR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09
31-30-04 Data Management Unit (DMU) part of Flight Data Interface . . . . . . . . . . . . . . . . . . . . . . . .
and Management Unit (FDIMU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09
31-30-05 Flight Data Interface Unit (FDIU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09
31-30-06 Quick Access Recorder (QAR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10
31-30-07 Printer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10
31-38-01 DATA LOADING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10
31-38-02 Data Loading Routing Box (DLRB) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10
31-38-03 Multipurpose Disk Drive Unit (MDDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11
31-53-01 Flight Warning Computer (FWC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11
31-53-02 MASTER CAUT Cancel Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11
31-53-03 MASTER WARN Cancel Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11
31-53-04 MASTER CAUT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11
31-53-05 MASTER WARN light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.12
31-53-06 Altitude Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.12
31-55-01 System Data Acquisition Concentrator (SDAC). . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13
31-56-01 System Page Manual Call pb onthe ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13
31-56-02 ALL pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13
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ITEM PAG
ATA 31 - INDICATING / RECORDING SYSTEMS (Cont’d )
31-56-03 CLR pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-56-04 EMER CANC pb on the ECP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-56-05 RCL pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-56-06 STS pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-56-07 T.O CONFIG pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-62-01 DMC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-62-02 DMC 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-62-03 DMC 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1
31-63-01 PFDU 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2
31-63-02 PFDU 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2
31-63-03 NDU 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2
31-63-04 NDU 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2
31-63-05 SDU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2
31-63-06 EWDU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2
31-68-01 AIR DATA SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . . . . . . 01.31.2
31-68-02 ATT HDG SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . . . . . . 01.31.2
31-68-03 ECAM/ND XFR SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . 01.31.2
31-68-04 EIS DMC SWITCHING selector on the Center Pedestal. . . . . . . . . . . . . . . . . . . . 01.31.2
31-68-05 PFD/ND XFR pb on the Lateral Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2
ATA 32 - LANDING GEAR
32-07-01 Brakes Temperature Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . 01.32.0
32-07-02 L/G Position Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-03 L/G Doors Position Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-04 L/G CTL Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-05 UP LOCK Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-06 [Y] N/W STEERING Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-07 Tire Pressure Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-08 ANTI SKID, [1], [2] Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-09 AUTO BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-10 [G] NORM BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-11 Release Brake Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
32-07-12 ACCU PRESS/ACCU ONLY Indication on the WHEEL SD page . . . . . . . . . . . . . 01.32.1
32-07-13 [Y] ALTN BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1
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ITEM PAGE
ATA 32 - LANDING GEAR (Cont’d)
32-09-01 BRAKES-N/WS MINOR FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.19
32-09-02 WHEEL TYRE LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.21
32-11-01 Main Gear Torque Link Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.22
32-12-01 Ground Opening Cable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.22
32-31-01 Landing Gear Control and Interface Unit (LGCIU). . . . . . . . . . . . . . . . . . . . . . . . . 01.32.23
32-31-02 Landing Gear Retracting System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.26
32-32-01 LGCIU 1 Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.26
32-32-02 LGCIU 2 RH L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.27
32-32-03 LGCIU 2 LH L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.29
32-32-04 LGCIU 2 Nose L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . 01.32.32
32-32-05 LGCIU 2 RH L/G Down Lock Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.33
32-32-06 LGCIU 2 LH L/G Down Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.34
32-32-07 LGCIU 2 Nose L/G Down Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . 01.32.35
32-32-08 LGCIU 2 RH L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.36
32-32-09 LGCIU 2 LH L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.37
32-32-10 LGCIU 2 Nose L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.38
32-32-11 LGCIU 2 RH L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.39
32-32-12 LGCIU 2 LH L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.39
32-32-13 LGCIU 2 Nose L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . 01.32.40
32-32-14 LGCIU 2 RH L/G Doors Closed Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . 01.32.41
32-32-15 LGCIU 2 LH L/G Doors Closed Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . 01.32.42
32-32-16 LGCIU 2 Nose L/G Doors Closed Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.43
32-33-01 Landing Gear Gravity Extension System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.43
32-41-01 Nose Wheel Tie Bolt . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.43
32-41-02 Main Wheel Tie Bolt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.44
32-42-01 Main Wheel Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.45
32-42-02 Green System Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.48
32-42-03 Braking/Steering Control Unit (BSCU) System 1. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.49
32-42-04 Braking/Steering Control Unit (BSCU) System 2. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.49
32-42-05 AUTO/BRK Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50
32-42-06 Tachometer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50
32-42-08 AUTO/BRK (LO,MED, MAX) pb-sw DECEL light . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50
32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5132-44-01 Yellow System Brake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.51
32-44-02 ACCU PRESS Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.52
32-44-03 BRAKES Pressure Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.53
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MEL
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ITEM PAG
ATA 32 - LANDING GEAR (Cont’d)
32-44-04 Alternate Braking Control Unit (ABCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-45-01 Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-47-01 Brake Temperature Monitoring Unit (BTMU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-48-01 Brake Fan System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-48-02 BRK FAN pb-sw HOT light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-48-03 BRK FAN pb-sw ON light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-51-01 Nose Wheel Steering Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-51-02 Rudder PEDALS DISC pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-51-03 NWS Electrical Deactivation Box. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-51-04 PARKING BRAKE light on the NWS Electrical Deactivation Box . . . . . . . . . . . . . 01.32.5
32-61-01 LDG GEAR Indicator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
32-61-02 DOWN Red Arrow light on the Landing Gear lever . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5
ATA 33 - LIGHTS
33-01-01 ANN LT Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-01-02 SIGNS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-10-01 Cockpit General Illumination (Center & Main Instrument Lighting, . . . . . . . . . . . . . . . . . .
Console and Floor Lighting, Dome lights and Lighting Strips, Instrument . . . . . . . . . . . .
and Panel Integral Lighting, Map Holder Lighting, Center Pedestal Lighting) . . . . 01.33.0
33-20-01 Cabin General Illumination. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.033-20-02 Cabin Signs (No Smoking/Fasten Seat Belt/Return to Seat). . . . . . . . . . . . . . . . . 01.33.0
33-20-03 Lavatory Sign (Return to seat). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-30-01 Cargo and Service Compartment Lighting System . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-01 Navigation light System 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-02 Navigation light System 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-03 Landing light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-04 Landing light Extension/Retraction System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-05 Runway Turnoff lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-06 Taxi and Takeoff light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-07 Logo lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-08 Beacon light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.033-40-09 Wing Scan lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-40-10 Strobe light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-51-01 Exit Marking Sign (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-51-01 Exit Marking Sign (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-51-02 Exit Location Sign in the Main Aisle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0
33-51-03 Overhead Emergency Lighting System in the Main Aisle . . . . . . . . . . . . . . . . . . . 01.33.0
30 JUN 12MEL
A320/321MEL/CDL
01.00TABLE OF CONTEN
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ITEM PAGE
ATA 33 - LIGHTS (Cont’d)
33-51-04 Overhead Emergency Lighting System in the Door Vicinity (A320). . . . . . . . . . . . 01.33.10
33-51-04 Overhead Emergency Lighting System in the Door Vicinity (A321). . . . . . . . . . . . 01.33.10
33-51-05 Floor Proximity Emergency Escape Path Marking System in the Main Aisle . . . . 01.33.10
33-51-07 Floor Proximity Emergency Escape Path Marking System Exit Marker . . . . . . . . 01.33.11
33-51-08 Overwing Emergency light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11
33-51-09 Overwing Exit Handle light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11
33-51-10 Escape Slide Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11
33-51-11 Lavatory Auxiliary light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11
ATA 34 - NAVIGATION
34-00-01 ADR (1)(2)(3) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01
34-00-02 IR MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01
34-01-01 ADIRS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01
34-01-02 GPWS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.04
34-05-01 Actual Airspeed Reference Line and Scale Indication on the PFD . . . . . . . . . . . . 01.34.04
34-05-02 Mach Number Indication on the PFD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.04
34-05-03 VMO/MMO Characteristic Speed Indication on the PFD. . . . . . . . . . . . . . . . . . . . 01.34.05
34-05-04 Altitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.05
34-05-05 Baro Reference Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.05
34-05-06 Vertical Speed in Inertial Mode Indication on the PFD . . . . . . . . . . . . . . . . . . . . . 01.34.05
34-05-07 Other Air Data Related Indications on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.0634-05-08 Attitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.06
34-05-09 Heading Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.06
34-06-01 Ground Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07
34-06-02 True Air Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07
34-06-03 Wind Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07
34-06-04 Heading Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07
34-06-05 Position (Aircraft Symbol) Indication on the ND. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07
34-06-06 Radio Navaids Indications on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07
34-06-07 Chrono Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08
34-10-01 ADR 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08
34-10-02 ADR 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08
34-10-03 ADR 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.10
34-10-04 IR 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.11
01.00.18TABLE OF CONTENTS
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12 FEB 12MEL
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ITEM PAG
ATA 34 - NAVIGATION (Cont’d)
34-10-05 IR 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1
34-10-07 IR 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1
34-11-01 Angle of Attack (AOA) Sensor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1
34-11-02 CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR1 . . . . . . 01.34.1
34-11-03 CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR3 . . . . . . 01.34.1
34-11-04 F/O Total Air Temperature (TAT) Sensor Element Connected to ADR2 . . . . . . . . 01.34.1
34-21-05 Standby ALT Metric Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1
34-22-01 Standby Compass Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1
34-22-02 Standby Compass Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1
34-23-01 ISIS Baro-Altitude Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-23-02 ISIS Airspeed Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-23-03 ISIS Bugs Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-23-04 ISIS Horizon Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-23-05 ISIS ILS Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-23-06 ISIS Mach Number Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-30-04 Instrument Landing System (ILS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness . . . . . . . . . . . . . . . . . . .
and Warning System (TAWS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-40-02 Radio Altimeter Automatic Callout. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-40-03 Radio Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-40-04 Traffic Collision Avoidance System (TCAS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-40-05 Weather Radar System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-40-06 Predictive Windshear Detection Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-40-07 PULL UP-GPWS pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-50-01 ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2
34-50-03 ADF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3
34-50-04 DME. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3
34-50-05 VOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3
34-50-06 MARKER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3
34-50-09 Global Positioning System (GPS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3
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ITEM PAGE
ATA 35 - OXYGEN
35-01-01 OXYGEN Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.01
35-07-01 Crew OXY High Pressure Indication on the DOOR/OXY SD page . . . . . . . . . . . . 01.35.02
35-07-02 Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page . . . . . . . . . 01.35.03
35-10-01 Crew Oxygen Mask . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.03
35-10-02 Crew Oxygen Mask Microphone . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.03
35-10-03 Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc). . . . . . . . . . . . . 01.35.03
35-20-01 Passenger Oxygen Unit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.04
35-20-02 Cabin Attendant Oxygen Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.05
35-20-04 Galley Oxygen Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.05
35-20-05 Manual Release Tool. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.06
35-30-01 Flight Crew Portable Device . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.06
35-30-02 Cabin Attendant Portable Device. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.07
ATA 36 - PNEUMATIC
36-00-01 AIR BLEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01
36-01-01 ENG BLEED pbsw FAULT light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01
36-01-02 ENG BLEED pbsw OFF light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01
36-01-03 APU BLEED pb-sw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01
36-01-04 APU BLEED pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01
36-07-01 APU Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . 01.36.02
36-07-02 Engine Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . 01.36.0236-07-03 Engine Bleed HP Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . 01.36.02
36-07-04 Engine Bleed Precooler Inlet Pressure Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.02
36-07-05 Engine Bleed Precooler Outlet Temperature Indication . . . . . . . . . . . . . . . . . . . . . . . . . . .
on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.02
36-07-06 X Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.36.03
36-11-01 Engine Bleed Air Supply System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.03
36-11-02 Engine Bleed Valve (PRV). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.05
36-11-03 Engine Bleed Overpressure Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.05
36-11-04 Engine Bleed Fan Air Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.06
36-11-05 Engine Bleed Air Precooler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.06
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ITEM PAG
ATA 36 - PNEUMATIC (Cont’d)
36-11-06 Engine Bleed IP Check Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0
36-11-07 Engine Bleed HP Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0
36-11-08 Bleed Monitoring Computer (BMC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0
36-12-01 APU Bleed Air Supply System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0
36-12-02 APU Bleed Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0
36-12-03 APU Bleed Check Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1
36-12-04 Automatic Control of the X Bleed Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1
36-22-01 Pylon Leak Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1
36-22-02 Wing Leak Detection System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1
36-22-03 APU Leak Detection Loop . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1
ATA 38 - WATER/WASTE
38-10-01 Potable Water Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.38.0
38-30-01 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories). . . . . . . . 01.38.0
ATA 46 - INFORMATION SYSTEMS
46-11-01 Electronic Flight Bag (EFB) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0
46-21-01 Air Traffic Service Unit (ATSU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0
46-21-02 Datalink Control and Display Unit (DCDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0
46-21-03 ATC MSG pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0
ATA 47 - INERT GAS SYSTEMS
47-00-01 FUEL INERT MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.47.0
ATA 49 - AIRBORNE AUXILIARY POWER
49-00-01 APU MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0
49-01-01 APU MASTER SW pb-sw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.049-01-02 APU MASTER SW pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0
49-01-03 APU START pb-sw AVAIL light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0
49-01-04 APU START pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0
49-07-01 Indications on the APU SD Page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0
49-10-01 Power Plant (APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0
49-10-02 APU Air Intake Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0
01 MAY 12MEL
A320/321MEL/CDL
01.00TABLE OF CONTEN
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ITEM PAGE
ATA 52 - DOORS
52-01-01 CKPT DOOR CONT Normal Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.01
52-01-02 CKPT DOOR CONT BK UP Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.02
52-01-03 CKPT DOOR BK UP Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.05
52-07-01 Passenger Door Permanently Indicated Open on the DOOR/OXY . . . . . . . . . . . . . . . . . .
SD page (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.10
52-07-01 Passenger Door/Emergency Exit Permanently . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Indicated Open on the DOOR/OXY SD page(A321) . . . . . . . . . . . . . . . . . . . . . . . 01.52.14
52-07-02 Passenger Door Permanently Indicated . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Closed on the DOOR/OXY SD page (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.18
52-07-02 Passenger Door/Emergency Exit Permanently Indicated Closed . . . . . . . . . . . . . . . . . . . .
on the DOOR/OXY SD page (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.19
52-07-03 Overwing Emergency Exit Permanently Indicated Open on the . . . . . . . . . . . . . . . . . . . . .DOOR/OXY SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.20
52-07-04 Overwing Emergency Exit Permanently Indicated Closed on the . . . . . . . . . . . . . . . . . . . .
DOOR/OXY SD page (A320). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.23
52-07-05 Cargo Door Indication on the DOOR/OXY SD page . . . . . . . . . . . . . . . . . . . . . . . 01.52.24
52-07-06 Avionics Compartment Access Door Indication on the . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DOOR/OXY SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.25
52-10-01 Cabin Passenger Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27
52-10-02 Overwing Emergency Exit (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27
52-10-03 Passenger Exit Stop Fitting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27
52-10-04 Door Damper Function (A320 & A321)). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27
52-10-05 Door Emergency Opening Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28
52-10-06 CHECK DOOR PRESSURE Message on the . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Flight Attendant Panel (FAP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28
52-10-07 Passenger Door Stay Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28
52-10-08 CABIN PRESSURE light (on Doors) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29
52-30-01 Cargo Door (FWD, AFT and BULK) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29
52-30-02 Cargo Door Actuator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29
52-30-03 Cargo Door Electrical Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.30
52-30-04 Cargo Door Locking Hooks and Spools (Rollers) . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.30
52-30-05 Cargo Door Hand Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31
52-30-06 Cargo Door Drift Pin. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31
52-30-07 Cargo Doors Open/Locked Indicator light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31
52-33-01 Cargo Door Balance Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.32
52-51-01 CDLS Normal System (Normal Control Unit, Switch and Lights on the . . . . . . . . . . . . . . .
CKPT DOOR Panel,Buzzer, Keypad) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.32
52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on . . . . . . . . . . . . . . . . .
the CKPT DOOR BK UP Panel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.34
01.00.22TABLE OF CONTENTS
A320/321MEL/CDL
12 FEB 12MEL
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TEM PAG
ATA 52 - DOORS (Cont’d)
52-51-03 CDLS Buzzer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3
52-51-04 CDLS Keypad . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3
52-51-05 CDLS Keypad Green and Red LEDs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3
52-51-06 CDLS Door Release Strike (Catch, Spring, Solenoid, Bolt). . . . . . . . . . . . . . . . . . 01.52.3
52-53-01 COCKPIT DOOR FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3
52-53-02 COCKPIT DOOR OPEN light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3
52-53-03 LOCK Function of the COCKPIT DOOR sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3
52-53-04 UNLOCK Function of the COCKPIT DOOR sw. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3
ATA 56 - WINDOWS
56-10-01 Front Windshield Note: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0
56-10-02 Lateral Fixed/Sliding Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0
56-10-03 Sliding Window Opening/Closing Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0
56-20-01 Cabin Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0
ATA 70- ENGINE
70-00-01 ENG FADEC MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.0
70-00-02 ENG EIU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.0
70-00-03 ENG EVMU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.0
ATA 73- ENGINE FUEL AND CONTROL
73-07-01 F. USED Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
73-07-02 Fuel Filter Clog Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
73-08-01 F. F. (Fuel Flow) Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
73-09-01 ENG 1(2) FUEL FILTER CLOG Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
73-10-01 Fuel Return Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
73-10-03 Fuel Metering Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
73-20-01 Flex Takeoff Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
73-20-05 Minimum Idle on Ground . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0
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ITEM PAGE
ATA 74 - IGNITION
74-07-01 Selected Igniter Indication on the ENGINE SD page. . . . . . . . . . . . . . . . . . . . . . . 01.74.01
74-09-01 ENG 1(2) IGN A(B)(A+B) FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.03
74-31-01 Ignition System A. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.03
74-31-02 Ignition System B. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.04
ATA 76 - ENGINE CONTROL
76-11-01 Thrust lever Position Sensor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.76.01
ATA 77 - ENGINE INDICATING
77-07-01 Indications on the CRUISE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.01
77-07-02 Indications on the ENGINE SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.02
77-08-01 EGT Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05
77-08-03 F.F. (Fuel Flow) Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05
77-08-04 N1 Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05
77-08-05 N2 Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05
ATA 78 - ENGINE EXHAUST
78-08-01 REV Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.0178-30-01 Thrust Reverser. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.01
78-30-02 Thrust Reverser Inhibition Relay sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.05
78-30-03 Thrust Reverser Shutoff Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.05
ATA 79 - ENGINE OIL
79-07-01 CLOG Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.01
79-07-02 Oil Pressure Indication and Advisory on the ENGINE SD page . . . . . . . . . . . . . . 01.79.01
79-07-03 Oil Quantity Indication on the ENGINE SD page. . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.02
79-07-04 Oil Temperature Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . 01.79.0279-09-01 ENG 1(2) OIL LO PR Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.02
79-09-02 ENG 1(2) OIL FILTER CLOG Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.03
79-20-02 EMCD Visual Pop- Out Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.04
79-40-01 Fuel Return Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.04
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ATA 80 - STARTING
80-01-31 ENG MAN START pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.0
80-07-01 Start Valve Position Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . 01.80.0
80-11-01 Start Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.0
80-12-01 FAULT light on the ENG MASTER Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.0
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FAA MMEL Preamble
The following is applicable for authorized certificateholders operating under Federal Aviation Regulations
(FAR) Parts 121, 125, 129, 135: The FAR require that allequipment installed on an aircraft in compliance with the
Airwor thiness Standards and the Operating Rules mustbe operative. However, the Rules also permit thepublication of a Minimum Equipment List (MEL) wherecompliance with certain equipment requirements is notnecessary in the interests of safety under all operatingconditions. Experience has shown that with the variouslevels of redundancy designed into aircraft, operation of every system or installed component may not benecessary when the remaining operative equipment canpr ovi de an acceptable l evel of safet y. A Mast er Minimum Equipment List (MMEL) is developed by the
FAA, with participation by the aviation industry, toimprove aircraft utilization and thereby provide moreconvenient and economic air transportation for thepublic. The FAA approved MMEL includes those itemsof equipment related to airworthiness and operatingregulations and other items of equipment which the
Administrator f inds may be inoperative and yet maintainan acceptable level of safety by appropriate conditionsand limitations; it does not contain obviously requireditems such as wings, flaps, and rudders. The MMEL isthe basis for development of individual operator MELswhich take into consideration the operator’s particular aircraft equipment configuration and operational
conditions. Operator MELs, for administrative control,may include items not contained in the MMEL; however,relief for administrative control items must be approvedby the Administrator. An operator’s MEL may differ informat from the MMEL, but cannot be less restrictivethan the MMEL. The individual operator’s MEL, whenapproved and authorized, permits operation of theaircraft with inoperative equipment.
E quipment not r equi r ed by t he oper at i on bei ngc o n d u c t e d a n d e q u i p m e n t i n e x c e s s o f F A Rrequirements are included in the MEL with appropriateconditions and limitations. The MEL must not deviate
from the Aircraft Flight Manual Limitations, EmergencyProcedures or with Airworthiness Directives. It isimportant to remember that all equipment related to theairworthiness and the operating regulations of theaircraft not listed on the MMEL must be operative.
Suitable conditions and limitations in the formplacards, maintenance procedures, crew operatprocedures and other restrictions as necessary a
specified in the MEL to ensure that an acceptable leof safety is maintained.
T h e M E L i s i n t e n d e d t o p e r m i t o p e r a t i o n winoperative items of equipment for a period of time urepairs can be accomplished. It is important that repabe accomplished at the earliest opportunity. In ordemaintain an acceptable level of safety and reliability MMEL establishes limitations on the duration of aconditions for operation with inoperative equipmeThe MEL provides forreleaseof theaircraft forflight winoperative equipment. When an item of equipmendiscovered to be inoperative, it is reported by making
entry in the Aircraft Maintenance Record/Logbookprescribed by FAR. The item is then either repairedmay be deferred per the MEL or other approved meaaccept abl e t o t he A dmini str at or pr i or t o f ur thoperation. MEL conditions and limitations, do not reliethe operator from determining that the aircraft iscondition for safe operation with items of equipminoperative.
When these requirements are met, an AirworthineRelease, Aircraft Maintenance Record/Logbook eno r o t h e r a p p r o v e d d o c u m e n t a t i o n i s i s s u e d prescribed by FAR. Such documentation is requi
p r i o r t o o p e r a t i o n w i t h a n y i t e m o f e q u i p m einoperative.
Operators are responsible for exercising the necessoperational control to ensure that an acceptable levesafety is maintained. When operating with multiinoperative items, the interrelationships between thoitems and the effect on aircraft operation and crworkload will be considered.
Operators are to establish a controlled and sound repprogram including the parts, personnel, facilitiprocedures, and schedules to ensure timely repair.
WHEN USING THE MEL, COMPLIANCE WITH TSTATED INTENT OF THE PREAMBLE, DEFINITION
A N D T H E C O N D I T I O N S A N D L I M I T A T I OSPECIFIED IN THE MEL IS REQUIRED.
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Definitions
1. System Definitions.
System numbers are based on the Air Transport Association (ATA) Specification Number 100 anditems are numbered sequentially.
a. “SYSTEM & SEQUENCE NUMBERS - ITEM”(Column 1) means the equipment, system,component, or function listed in the “Item” column.The letters “SV” added at the end of a sequencenumber indicates that it is a Saudia added itemand will not be found in the FAA Master MEL.Where applicable, EICAS/EIS status message(s)are also listed in this column..
b. “NUMBER INSTALLED” (Column 2) is thenumber (quantity) of items normally installedin theaircraft. This number represents the aircraftconfiguration considered in developing the MEL.Should the number be a variable (e.g., passenger cabin items) a number is not required, are a dash(-) symbol is shown.
c. “ N U MB E R R E Q U IR E D F O R D I S P A TC H ”(Column 3) is the minimum number (quantity) of i tems required for operation provided theconditions specified in Column 4 are met.
NOTE:
Where the MMEL shows a variable number required for dispatch, the MEL must reflectthe actual number required fordispatch or analternate means of configuration controlapproved by the Presidency of Civil Aviation(PCA).
d “REMARKS OR EXCEPTIONS” (Column 4) thiscolumn includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions andlimitations) for such operation, and appropriatenotes.
e. A vertical bar (change bar) in the margin indicatesa change, addition or deletion in the adjacent textfor the current revision of that page only. Thechange bar is dropped at the next revision of thatpage.
2. “Airplane Flight Manual” (AFM) is the documentrequired for type certification and approved by the
responsible FAA Aircraft Certification Office. The FAAapproved AFM for the specific aircraft is listed on theapplicable Type Certificate Data Sheet. (The AFM willnot be carried aboard the aircraft).
3. “Placarding” Each inoperative item must be placardedt o i nfor m and r emi nd t he cr ewmember s andmaintenance personnel of the equipment condition.placard should be located adjacent to the control or indicator for the item affected, unless otherwisespecified, placard wording and location will bedetermined by the placarding procedures located onsection 3 of this manual.
4. “-” symbol in Column 2 and/or Column 3 indicates avariable number (quantity) of the item installed.
5. “ER” refers to extended range operations of a two-engine airplane which has a type design approval for ER operations and complies with the provisions of
Advisory Circular 120-42A.
6. “Extended over-water operation” means operationover water at a horizontal distance of more than 50nautical miles from the nearest shoreline.
7. “Federal Aviation Regulations” (FAR) means theapplicable portions of the Federal Aviation Act andFederal Aviation Regulations.
8. “Flight” for MEL purposes means one operationalcycle of the aircraft including only one takeoff and onelanding. Where a proviso includes a limitation on thenumber of flights permitted with an inoperative item,the count will start with the next flight after discoverythat the item has become inoperative.
9. “Flight Hours” for MEL purposes means the time fromthe moment the aircraft leaves the surface of the earthuntil it touches down at the next point of landing (i.e.,takeoff to landing time). “Flight Hours” is identical to
“time in service,” as defined by GACA/FAR Part 1.Where a proviso includes a limitation on the number of flight hours permitted with an inoperative item, the timewill start at the next takeoff after discovery that the itemhas become inoperative.
10. “Flight Day” means a 24 hour period (from midnight tomidnight) Universal Coordinated Time (UCT), duringwhich at least one flight is initiated for the affectedaircraft.
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Definitions (Cont’d)
11. “Icing Conditions” meansan atmospheric environment
that may cause ice to form on the aircraft or in theengine(s).
12. “Inoperative” means a system and/or componentmalfunction to the extent that it does not accomplish itsi nt ended pur pose and/ or i s not consi st ent l yfunctioning normally within its approved operatinglimit(s) or tolerance(s).
13. “NOTES:” in Column 4 provides additional informationfor crewmember or maintenance consideration. Notesare used to identify applicable material which isintended to assist with compliance, but do not relievethe operator of the responsibility for compliance with
all applicable requirements.
14. “Inoperative components of an inoperative system”:Inoperative items which are components of a systemw hi ch i s i noper at ive ar e usuall y consider edcomponents directly associated with and having noo t h er f u nc t io n t h an t o s u p po r t t h a t s y s te m .(Warning/caution systems associated with theinoperative system must be operative unless relief isspecifically authorized per the MEL).
15. “(M)” symbol indicates a requirement for a specificmaintenance procedure which must be accomplishedprior to operation with the listed item inoperative.Normally these procedures are accomplished bymaintenance personnel; however, other personnelmay be qualified and authorized to perform certainf unct i ons. P r ocedur es r equi r i ng speci al i zedknowledge or skill, or requiring the use of tools or testequipment should be accomplished by maintenancepersonnel. The satisfactory accomplishment of allmaintenance procedures, regardless of who performsthem, is the responsibility of Technical Services.
Appropriate procedures are required to be publishedas part of Technical Services manuals or MEL.
16. “(O)” symbol indicates a requirement for a specific
operations procedure which must be accomplished inplanning for and/or operating with the listed itemi noper at i ve. N or mal l y t hese pr ocedur es ar eaccomplished by the flight crew; however, other personnel may be qualified and authorized to performcertain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, isthe responsibility of Flight Operations. Appropriateprocedures are required to be published as a part of Flight Operations manuals or MEL.
NOTES:
The (M) and (O) symbols are required in Saudi Ar ab ia n Ai rL in es ME L un le ss ot he rw is eauthorized by the GACA.
17. “Deactivated” and “Secured” means that the specifcomponent must be put into an acceptable conditfor safe flight. An acceptable method of securingdeactivating willbe established by Technical Servic
18. “Visual Flight Rules” (VFR) is as defined in FAR P91. This precludes a pilot from filing an InstrumFlight Rules (IFR) flight plan.
19. “Visual Meteorological Conditions” (VMC) means atmospheric environment is such that would allowflight to proceed under the visual flight rules applicato the flight. This does not preclude operating undInstrument Flight Rules.
20. “Visible Moisture” means an atmospheric environmcontaining water in any form that can be seennatural or artificial light; for example, clouds, fog, rasleet, hail, or snow.
21. “Passenger Convenience Items” , Deleted, See N32.
22. “Non-combustible materials” means metallic objethat will not sustain a fire.
23. “ R e p a ir ” a n d “ R e p l a ce m e n t ” r e f e r t o s u
maintenance action as necessary to restore inoperative item to an operative condition.
24. “Crewmember “ means a person assigned to perfoduty in an aircraft during flight time.
25. Repair Intervals: All users of an MEL approved unFAR 121, 125, 129 and 135 must effect repairsinoperative systems or components, deferredaccordance with the MEL, at or prior to the repair timestablished by the following letter designators:
Category A. Items in this category shall be repai
within the time interval specified in
remarks column of the operato
approved MEL.
Category B. Items in this category shall be repai
within three (3) consecutive calen
days (72 hours), excluding the day th
Definitions (Cont’d)
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malfunction was recorded in the aircraft
maintenance record/logbook. For
example, if it were recorded at 1000
UCT on January 26th, the three day
interval would begin at midnight the 26thand end at midnight the 29th.
Category C. Items in this category shall be repaired
within ten (10) consecutive calendar
days (240 hours), excluding the day the
malfunction was recorded in the aircraft
maintenance record/logbook. For
example, if it were recorded at 1000
UCT on January 26th, the 10 day
interval would begin at midnight the 26th
and end at midnight February 5th.
Category D. Items in this category shall be repairedw i t hi n one hundr ed t w ent y ( 120)
consecutive calendar days (2880
h o ur s) , e x cl ud in g t he d a y t he
malfunction was recorded in the aircraft
maintenance record/logbook.
The letter designators are inserted adjacent toColumn 2.
26. Electronic Fault Alerting System - General
New generation aircraft display system faultindications to the flight crew by use of computerized
display systems. Each aircraft manufacturer hasincorporated individual design philosophies indetermining the data that would be represented. Thefollowing customized definition may be used to helpdetermine the level of messages affectingthe aircraft’sdispatch status.
a. AIRBUS (A320, A321, A330)
Airbus aircraft equipped with Electronic Centralized
Aircraft Monitoring (ECAM) provide different levels
of system condition messages (WARNING,
CAUTION, STATUS and ADVISORY). A-320/321
and A-330 also provide MAINTENANCE status
messages.
Any message that affects airplane distpatchability
will normally be at the WARNING, CAUTION or
STATUS level. MAINTENANCE messages (A-
320/321 and A-330 only) are also indicated on
ECAM Status Page below the white Maintenance
label.
A MAINTENANCE status (Class II) message on
ECAM indicates the presence of a system fault
which can be identified by CFDS (A-320/321) or
CMS (A-330) interrogation. The systems are
designed to be fault tolerant; however for any
MAINTENANCE status (ClassII) message the A-3120/321 MEL must be verified for dispatch
capability. For the A-330, MAINTENANCE status
messages do not affect dispatch.
b. BOEING (B-747-468, B-777)
Boeing aircraft equipped with Engine Indicating and
Crew Alerting Systems (EICAS), provide different
priority levels of system messages (WARNING,
C AU TI ON , A DV IS OR Y, S TA TU S a nd
MAINTENANCE). Any messages that affects
aircraft dispatch status will be displayed as a
STATUS message level or higher. The absence of
an EICAS STATUS or higher level (WARNING,CAUTION, ADVISORY) message indicates that the
system/component is operating within its approved
operating limits or tolerances.
System conditions that result only in a maintenance
level message, i.e., no correlation with a higher
level EICAS message, do not affect dispatch and do
not require action other than as addressed within an
operator’s standard maintenance program.
c. DOUGLAS (MD-11, MD-90)
Some Douglas aircraft are equipped with an
alerting function which is a subsystem within the
Electronic Instrument System (EIS). The alertingfunction provides various levels of system condition
alerts (WARNING, CAUTION, ADVISORY,
MAINTENANCE and STATUS).
Alerts that affect aircraft dispatch will include
WA RN I NG , C AU TI O N, S TA TU S o r
MAINTENANCE level. MAINTENANCE alerts are
displayed on the status page of the EIS display
panel under the maintenance heading.
A MAINTENANCE alert on the EIS indicates the
presence of a system fault which can be identified
by the Central Fault Display System (CFDS for MD-
11), or Engine and Alert Display (EAD for MD-90)interrogation. The systems are designed to be fault
tolerant, however, for any MAINTENANCE alert,
the MEL must be verified for dispatch purposes.
Definitions (Cont’d)
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d. EMBRAER ( ERJ-170)
The ERJ-170 are equipped with an Engine
indicating and crew alerting system (EICAS) that
provides three different message levels :
WARNING,CAUTION, and ADVISORY. The ERJ -
170 SERIES and STATUS messages. Failures that
effect dispatchability are presented to the flight
crew at one of these levels.other failures may be
presentes only to the maintenance personnel on
the multi function display (MFD) maintenance
pages or through the download of the Central
Maintenance Computer (CMC).
26. System conditions that result only in a maintenance
level message, I.e. No correlation with a higher levelEICAS message, do not affect dispatch and do notrequire action other than as addressed within anoperator’s standard maintenance program.
27. “ D a y o f D i s co v e r y ” i s t h e c a l e n da r d a y a nequipment/instrument malfunction was recorded inthe aircraft maintenance log and/or record. This day isexcluded from the calendar days or flight daysspecified in the MEL for the repair of an inoperativeitem of equipment. This provision is applicable to allMEL items, i.e., categories “A, B, C, and D.”
28. “Operative” or “Operates normally” - When the MEL
specifies that an item of equipment is operative or thatit operates normally, it means that the system and/or component will accomplish its intended purpose and isconsistently functioning normally within its designoperating limit(s) and tolerance(s). It does not meanthat its operational status must be verified; it is to beconsidered operativeunlessreportedor is known to bemalfunctioning.
29. “Must be verified operative” or “Must be verified tooperate normally”- When the MEL specifies that anitem of equipment must be verified operative, it meansthat it must be checked and confirmed operative at theinterval(s) specified for the item. When the MEL
specifies that an item of equipment must be verifiedoperative, but no interval is specified, verification isrequired only at the time of deferral.
30. A “(FD)” symbol indicates a requirement for thetechnical personnel to notify flight dispatch as soon asa relevant MEL item becomes open on the hold itemlist and must be shown on the flight dispatch release,or an amendment made. Such items normally involve
restrictions associated with flight level, speed, weigetc.
31. “Considered inoperative”,as used in the provismeans that item must be treated for dispatch, taxi a
flight purposes as though it were inoperative. The itshall not be used or operated until the original deferi t em i s r epair ed. A ddit i onal act ions i ncludocumenting the item on the dispatch releaseapplicable), placarding, and complying with remarks, exceptions, and related MMEL provisioincluding any (M) and (O) procedures and observthe repaircategory.
32. Nonessential equipment and furnishings (NEF) those items installed on the aircraft as part of original certification,supplemental type certificateengineering order that have no effect on the s
operation of flight and would not be required by applicable certification rules or operational rules. Thare those item that if inoperative, damaged or misshave no effect on the aircraft’s ability to be operatsafely under all operational conditions.
Weight Reductions
The MEL weight reductions must be applied to maximum performance limited weights, as follows:
1. Takeoff - Weight penalty is applied to the m
restrective of the Zero Wind weight
Climb Limit weight.
2. Enroute - Weight penalty is applied to cruise a
o n e e n g i n e i n o p e r a t i v e A l t i t u
Capability limited weights.
3. Landing - Weight penalty is applied to the m
restrective of tailored landing cha
field length or landing climb limi
weight.
Dispatch Fuel Penalty
The percentage increase in the fuel must be appliedthe minimum dispatch fuel requirement.
Minimum dispatch fuel required is the sum of trip fualternate fuel and reserve fuel.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.01
MEL INTRODUCTIO
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01.01.06MEL INTRODUCTION
A320/321MEL/CDL
MEL
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ECAM WARNINGS / MEL ENTRY
The following pages give correspondence between ACAM caution/warning messages and MEL item number:
CAUTION
1) This section is, normally, not intended to cover false cautions/warnings.
However, if a caution/warning is determined to be false by troubleshooting, the crew should refer to the concerne
caution/warning message item (if listed) in the associated ATA chapter 01.
2) In order to help the crew to determine the MEL ENTRY point corresponding to a caution/warning message, the
REMARK column contains the text:
a) “Actual warning” or “Actual caution”.The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions correspondin
to an actual failure of the system/ component monitored by the caution/warning.
b) “False warning” or “False caution”.
The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions correspondin
to the failure of the warning, determined by troubleshooting. The system/component monitored by the
caution/warning being still operative.
3) When the REMARK column contains neither, “Actual caution/warning”, nor “False caution/warning” textes, the ME
ENTRY point corresponds to an actual warning which indicates an actual failure of the system/component monitored
the caution/warning.
4) When either an actual, or a false caution/warning is activated, this section gives the MEL ENTRY point to be
considered.
But the crew MUST CHECK THAT THE AIRCRAFT SYSTEMS/COMPONENTS ARE IN A CONDITION WHCIH
COMPLIES WITH THE DISPTACH CONDITIONS.
IF NOT, AIRCRAFT DISPATCH IS NOT ALLOWED.
5) When a caution/warning is associated with the wording “Not applicable” in the Display Condition column, this mean
that the MEL is not appropriate document to be consulted.
When such caution/warnins have been triggered, application of associated procedure, if any , (refer to FCOM
Abnormal/Emergency procedures), and/or accomplishment of maintenance action, if required, would permit to fix theproblem.
( Cont'd on next page )
12 FEB 12MEL
A320/321MEL/CDL 01.02
GENER
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ECAM WARNINGS / MEL ENTRY ( Cont'd )
ECAM
The A320/321 Family aircraft is equipped with Electronic Centralized Aircraft Monitoring (ECAM) which provides
different levels of aircraft systems monitoring messages:
- ECAM warning. - ECAM advisory. - ECAM caution. -ECAM memo.
ECAM warning and ECAM caution messages are listed in the “MEL Entries” section.
ECAM advisory and ECAM memo messages are not listed in the “MEL Entries” section.
CONDITION OF DISPATCH COLUMN
- NO DISPATCH: It is not permitted to dispatch the aircraft when the ECAM displays this alert.
- NOT APPLICABLE: The ECAM alert does not report a system failure and is not related to MEL. The MEL shall not be
used.
This is not a NO-GO situation. The corrective action to revert to normal condition is immediate, obvious or well known
by flight crew and/or maintenance personnel.
EXAMPLES
1) If the “BAT FAULT” caution message is displayed on ECAM, the crew must refer to MEL 24-30-02 (Battery channel).
2) If the “ac bus 1 fault fault” CAUTION MESSAGE IS DISPLAYED ON ecam, a/c DISPATCH IS NOT ALLOWED.
3) If the “GEN 1 OFF” caution message is displayed on ECAM no MEL entry is required, and the text “Not applicable” is
written in the Remark column.
In this example, the crew must switch on the generator pb sw.
4) If ”PACK 1 + 2 FAULT” caution message is displayed the crew must refer to FCOM for “FLIGHT WITHOUT
PRESURIZATION”.
Note : The ECAM warnings and cautions listed in section 00E in the column “ECAM WARNINGS” are generic.
*example :
ECAM WARNING DISPATCH CONDITION REMARK
FCU 1(2) (1 + 2) FAULT Refer to MEL 22-81-01
Wording FCU 1(2) (1 + 2) FAULT represents the three messages ; “FCU 1 FAULT” “FCU 2 FAULT” “FCU 1 + 2
FAULT”.
* * *
01.02.02GENERAL
A320/321MEL/CDL 12 FEB 12
MEL
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ATA 21 AIR CONDITIONING
ECAM WARNING ACTION DISPATCH CONDITION
AIR
AFT CRG VENT FAULT Refer to MEL 21-28-03
COND CTL 1(2)-A(B) Refer to MEL 21-63-04
PACK 1(2) FAULT Refer to MEL 21-52-01
PACK 1+ 2 FAULT Refer to FCOM/PRO-SPO-20
PACK 1(2) OFF Refer to MEL 21-52-01
PACK 1(2) OVHT Refer to MEL 21-52-01
PACK 1 (2) REGUL FAULT Refer to MEL 21-27-01-01 If pack outlet temperature is
affected
Refer to MEL 21-07-01-03 If pack compressor outlet
temperature is affected
Refer to MEL 21-51-03 If pack flow sensor is affecte
Refer to MEL 21-52-01 If pack flow control valve is
affected
Refer to MEL 21-52-02 If pack ram air inlet is affecte
Refer to MEL 21-61-01 If turbine bypass valve
affected
CAB PR
EXCESS CAB ALT Not applicable
EXCESS RESIDUAL PR Apply ECAM procedure
LDG ELEV FAULT Refer to MEL 21-31-04
LO DIFF PR Not applicable
OFV NOT OPEN NO DISPATCH
SAFETY VALVE OPEN Refer to FCOM/PRO-SPO-20 Actual alert
Refer to MEL 21-09-03 False alert
SYS 1(2) FAULT Refer to MEL 21-31-01
SYS 1+2 FAULT Refer to FCOM/PRO-SPO-20
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 21 AIR CONDITIONING
ECAM WARNING ACTION DISPATCH CONDITION
COND
AFT CAB DUCT OVHT Refer to MEL 21-63-02
AFT CARGO DUCT OVHT Refer to MEL 21-43-02
AFT CRG HEAT FAULT Refer to MEL 21-43-02
AFT CRG ISOL VALVE Refer to MEL 21-28-04
CKPT DUCT OVHT Refer to MEL 21-63-02
FWD CAB DUCT OVHT Refer to MEL 21-63-02
HOT AIR FAULT Refer to MEL 21-63-03
L + R CAB FAN FAULT NO DISPATCH
LAV + GALLEY FAN FAULT Refer to MEL 21-23-01
TRIM AIR SYS FAULT Not applicable If the trim air valves are colsed
Refer to MEL 21-63-02 If the associated AFT CAB
TRIM VALVE message is
displayed
Refer to MEL 21-63-02 If the associated FWD CAB
TRIM VALVE message is
displayed
Refer to MEL 21-63-02 If the associated CKPT TRIM
VALVE message is displayed
Refer to MEL 21-63-02 If the associated TRIM AIR HI
PR message is displayed
VENT
AVNCS SYS FAULT Refer to MEL 21-26-04 If the VENT SKIN VALVE
FAULT alert is displayed on the
EWD.
Refer to MEL 21-26-05 If the VENT SKIN VALVE
FAULT alert is displayed on the
EWD.
Refer to MEL 21-26-03, or
Refer to MEL 21-26-08, or
Refer to MEL 21-26-06, or
Refer to MEL 21-26-10
01.03.02ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 21 AIR CONDITIONING
ECAM WARNING ACTION DISPATCH CONDITION
VENT
BLOWER FAULT Refer to MEL 21-26-01 Actual caution
Refer to MEL 21-09-01 False caution
EXTRACT FAULT Refer to MEL 21-26-02 Actual caution
Refer to MEL 21-09-02 False caution
SKIN VALVE FAULT Refer to MEL 21-26-04 Faulty valve
determined on the
CAB PRESS page
Refer to MEL 21-26-05
ATA 22 AUTO FLIGHT
ECAM WARNING ACTION DISPATCH CONDITION
AUTO FLT
A/THR LIMITED Not applicable
A/THR OFF Refer to MEL 22-30-01 Actual caution
Refer to MEL 22-30-03 False caution
AP OFF Refer to MEL 22-10-01 Actual warning
Refer to MEL 22-10-06 False warning
FAC 1 FAULT Refer to MEL 22-60-01
FAC 2 FAULT Refer to MEL 22-60-02
FAC 1 + 2 FAULT NO DISPATCH
FCU 1 (2) FAULT Refer to MEL 22-81-03-01
FCU 1 + 2 FAULT NO DISPATCH
REAC W/S DET FAULT (if installed) Refer to MEL 22-60-03
RUD TRIM 1 (2) FAULT Refer to MEL 27-22-01
RUD TRIM SYS NO DISPATCH
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 22 AUTO FLIGHT
ECAM WARNING ACTION DISPATCH CONDITION
AUTO FLT
RUD TRV LIM 1 (2) Refer to MEL 27-23-01
RUD TRV LIM SYS NO DISPATCH
YAW DAMPER 1 (2) Refer to MEL 22-60-04
YAW DAMPER SYS NO DISPATCH
WINDSHEAR
DET FAULT Refer to MEL 22-60-03
ATA 23 COMMUNICATIONS
ECAM WARNING ACTION DISPATCH CONDITION
COM
ACARS FAULT (If installed) Refer to MEL 46-21-01
CIDS 1 + 2 FAULT NO DISPATCH
HF 1 (2) DATA FAULT (If installed) Refer to MEL 23-10-01
HF 1 (2) EMITTING (If installed) Refer to MEL 23-51-03 If hand microphone
selector is jammed in
the transmitting
position
Refer to MEL 23-51-06 If side stick radio
selector is jammed in
the transmitting
position
Refer to MEL 23-52-05 If a transmission Key
on one ACP is
jammed in the
transmitting position.
Refer to MEL 23-09-01 False alert
01.03.04EICAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 23 COMMUNICATIONS
ECAM WARNING ACTION DISPATCH CONDITION
COM
SATCOM DATA FAULT (If installed) Refer to MEL 23-10-03, and
Refer to MEL 23-20-02
SATCOM FAULT (If installed) Refer to MEL 23-10-03, and
Refer to MEL 23-20-02
VHF 3 DATA FAULT Refer to MEL 23-10-02
VHF 1(2)(3) EMITTING Refer to MEL 23-51-03, If hand microphone
selector is jammedthe transmitting
position
Refer to MEL 23-51-06 If side stick radio
selector is jammed
the transmitting
position
Refer to MEL 23-52-05 If a transmission K
on one ACP is
jammed in the
transmitting positio
Refer to MEL 23-09-02 False caution
ATA 24 ELECTRICAL POWER
ECAM WARNING ACTION DISPATCH CONDITION
C/B
TRIPPED Refer to affected systems Actual alert
Refer to MEL 24-09-02 False alert
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 24 ELECTRICAL POWER
ECAM WARNING ACTION DISPATCH CONDITION
ELEC
AC BUS 1 FAULT NO DISPATCH
AC BUS 2 FAULT NO DISPATCH
AC ESS BUS ALTN NO DISPATCH
AC ESS BUS FAULT NO DISPATCH
AC ESS BUS SHED NO DISPATCH Actual caution
Refer to MEL 24-09-01 False caution
APU GEN FAULT Refer to MEL 24-23-01
BAT 1(2) FAULT NO DISPATCH
BAT 1 (2) OFF Not applicable
BCL 1 (2) FAULT Refer to MEL 24-38-02 Actual caution
DC BAT BUS FAULT NO DISPATCH
DC BUS 1 + 2 FAULT NO DISPATCH
DC BUS 1 FAULT NO DISPATCH
DC BUS 2 FAULT NO DISPATCH
DC EMER CONFIG NO DISPATCH
DC ESS BUS FAULT NO DISPATCHDC ESS BUS SHED NO DISPATCH
EMER CONFIG NO DISPATCH
EMER GEN 1 LINE OFF Not applicable
ESS BUSSES ON BAT NO DISPATCH
ESS TR FAULT Refer to MEL 24-34-01
GEN 1 (2) FAULT Refer to MEL 24-22-01
GEN 1 (2) OFF Not applicable
GEN 1 (2) (APU GEN) OVERLOAD Refer to MEL 24-26-01
IDG DISCONNECTED Refer to MEL 24-22-01
IDG 1 (2) OIL LO PR Refer to MEL 24-22-01
IDG 1 (2) OIL OVHT Refer to MEL 24-22-01
STATIC INV FAULT NO DISPATCH
TR 1 (2) FAULT Refer to MEL 24-32-01
01.03.06ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 26 FIRE PROTECTION
ECAM WARNING ACTION DISPATCH CONDITION
APU FIRE NO DISPATCH Actual alert
Refer to MEL 49-10-01 False alert
APU
FIRE DET FAULT Refer to MEL 26-13-01, and
Refer to MEL 26-13-02
FIRE LOOP A(B) FAULT Refer to MEL 26-13-01 If loop A is failed
Refer to MEL 26-13-02 If loop B is failed
AVIONICS SMOKE NO DISPATCHr Actual alert
Refer to MEL 26-15-01 False alert
ENG 1(2)FIRE NO DISPATCH
ENG 1(2)
FIRE DET FAULT NO DISPATCH
FIRE LOOP A FAULT Refer to MEL 26-12-01 If engine 1 is affected
Refer to MEL 26-12-02 If engine 2 is affected
FIRE LOOP B FAULT Refer to MEL 26-12-03 If engine 1 is affected
Refer to MEL 26-12-04 If engine 2 is affected
SMOKE
AFT CARGO SMOKE NO DISPATCH Actaual alert
Refer to MEL 26-16-02 False alert
AFT CRG BTL FAULT Refer to MEL 26-23-02 If the SMOKE FWD CRG BT
FAULT alert is not displayed
on the EWDRefer to MEL 26-23-01 If the SMOKE FWD CRG BT
FAULT alert is displayed on
the EWD
AFT CRG DET FAULT Refer to MEL 26-16-02
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 26 FIRE PROTECTION
ECAM WARNING ACTION DISPATCH CONDITION
SMOKE
FWD CARGO SMOKE NO DISPATCH Actual alert
Refer to MEL 26-16-01 False alert
FWD CRG BTL FAULT Refer to MEL 26-23-02 If the SMOKE AFT CRG BTL
FAULT alert is not displayed on
the EWD
Refer to MEL 26-23-01 If the SMOKE AFT CRG BTL
FAULT alert is displayed on the
EWD
FWD CRG DET FAULT Refer to MEL 26-16-01
DET FAULT Refer to MEL 23-73-10-01
LAVATORY DET FAULT Refer to MEL 26-17-01
LAVATORY SMOKE NO DISPATCH Actual alert
Refer to MEL 26-17-01 False alert
ATA 27 FLIGHT CONTROLS
ECAM WARNING ACTION DISPATCH CONDITION
CONFIG
L(R) SIDESTICK FAULT NO DISPATCH
PITCH TRIM NOT IN T.O. RANGE NO DISPATCH
RUD TRIM NOT IN T.O. RANGE NO DISPATCH
SLATS (FLAPS) NOT IN T.O. CONFIG NO DISPATCH
SPEED BRK NOT RETRACTED NO DISPATCH
01.03.08ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 27 FLIGHT CONTROLS
ECAM WARNING ACTION DISPATCH CONDITION
F/CTL
AIL SERVO FAULT Refer to MEL 27-14-01, or
Refer to MEL 27-14-02, or
Refer to MEL 27-14-03, or
Refer to MEL 27-14-04
ALTN LAW NO DISPATCH
DIRECT LAW NO DISPATCH
ELAC 1 FAULT Refer to MEL 27-93-01
ELAC 1 PITCH FAULT Refer to MEL 27-93-01
ELAC 2 FAULT NO DISPATCH
ELAC 2 PITCH FAULT NO DISPATCH
ELEV SERVO FAULT NO DISPATCH If servocontrol is affected
Refer to MEL 27-34-02 If servocontrol position
transducer is affected
FCDC 1 FAULT NO DISPATCH
FCDC 2 FAULT Refer to MEL 27-95-02
FCDC 1+2 FAULT NO DISPATCH
FLAP ATTACH SENSOR NO DISPATCHFLAP LVR NOT ZERO Not applicable
FLAP SYS 1 FAULT NO DISPATCH
Refer to MEL 27-54-01 If the maintenance confirms
that the F/CTL FLAP SYS 1
FAULT alert is displayed on
the EWD due to a flap motor
failure
FLAP SYS 2 FAULT Refer to MEL 27-51-01
Refer to MEL 27-54-01 If the maintenance confirms
that the FTCL FLAP SYS 2
FAULT alert is displayed on
the EWD due to a flap motor
failure.
FLAP TIP BRK FAULT Refer to MEL 27-51-03
FLAPS (SLATS) FAULT NO DISPATCH
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 27 FLIGHT CONTROLS
ECAM WARNING ACTION DISPATCH CONDITION
F/CTL
FLAPS (SLATS) LOCKED NO DISPATCH
GND SPLR FAULT Refer to MEL 32-42-06 If the braking system is affected
Refer to MEL 27-92-02 If the braking system is not
affected
GND SPLR (1 + 2)(3 + 4) FAULT Refer to MEL 27-92-02
L(R) AIL FAULT NO DISPATCH
L(R) ELEV FAULT NO DISPATCH
L + R ELEV FAULT NO DISPATCH
L(R) SIDESTICK FAULT NO DISPATCH
SEC 1 FAULT Refer to MEL 27-94-01
SEC 2 FAULT Refer to MEL 27-94-02
SEC 3 FAULT Refer to MEL 27-94-03
SIDESTICK PRIORITY Refer to FCOM/PRO-ABN-27
SLAT SYS 1 FAULT NO DISPATCH
Refer to MEL 27-84-01 If the maintenance confirms the
F/CTL SLAT SYS 1 FAULT
alert is displayed on the EWDdue to a slat motor failure.
SLAT SYS 2 FAULT Refer to MEL 27-51-02
Refer to MEL 27-84-01 If the maintenance confirms the
F/CTL SLAT SYS 2 FAULT
alert is displayed on the EWD
due to a slat motor failure.
SLAT TIP BRK FAULT Refer to MEL 27-81-01
SPD BRK DISAGREE Refer to MEL 27-92-01
SPD BRK FAULT Refer to MEL 27-92-01
SPD BRK STILL OUT Not applicable
SPD BRK 2(3 + 4) FAULT Refer to MEL 27-92-01
01.03.10ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 27 FLIGHT CONTROLS
ECAM WARNING ACTION DISPATCH CONDITION
F/CTL
SPLR FAULT Refer to MEL 27-64-01,
Refer to MEL 27-64-02,
Refer to MEL 27-64-03,
Refer to MEL 27-64-04, or
Refer to MEL 27-64-05
STABILIZER JAM NO DISPTACH
ATA 28 FUEL
ECAM WARNING ACTION DISPATCH CONDITION
FUEL
ACT PUMP LO PR Refer to MEL 28-28-03
ACT UNUSABLE Not applicable
ACT XFR FAULT Refer to MEL 28-12-05, or Actual alert
Refer to MEL 28-46-02, or
Refer to MEL 28-28-01, or
Refer to MEL 28-28-02, or
Refer to MEL 28-28-04, or
Refer to MEL 28-28-05, or
Refer to MEL 28-28-06, or
Refer to MEL 28-28-09, or
Refer to MEL 28-46-05
Refer to MEL 28-09-03 False alert
APU LP VALVE FAULT Refer to MEL 28-29-01
AUTO FEED FAULT Refer to MEL 28-20-01
AUTO TRANSFER FAULT Refer to MEL 28-26-01
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 28 FUEL
ECAM WARNING ACTION DISPATCH CONDITION
FUEL
CTR TK PUMP 1(2) LO PR Refer to MEL 28-21-02
CTR TK PUMPS LO PR Refer to MEL 28-21-02
CTR TK PUMPS OFF Not applicable
CTR TK XFR OFF Not applicable
ENG 1(2) LP VALVE OPEN Refer to MEL 28-24-01
FQI CH 1(2) FAULT Refer to MEL 28-50-01
F.USED/FOB DISAGREE Not applicable
L(R) INNER (OUTER) TK HI TEMP Disptach possible only if
“delay T.O.” is not displayed
on ECAM
Actual alert
Refer to MEL 28-09-01 False alert
L(R) WING TK HI TEMP Disptach possible only if
“delay T.O.” is not displayed
on ECAM
Actual alert
Refer to MEL 28-09-01 False alert
L(R) INNER (OUTER) TK LO TEMP NO DISPATCH Actual alert
Refer to MEL 28-09-02 False alertL(R) WING TK LO TEMP NO DISPATCH Actual alert
Refer to MEL 28-09-02 False alert
L(R) TK PUMP 1(2) LO PR Refer to MEL 28-21-01
L(R) TK PUMP 1 + 2 LO PR NO DISPATCH
L(R) WING TK LO LVL NO DISPATCH Actual alert
Refer to MEL 28-46-04 False alert
L+R WING TK LO LVL NO DISPATCH
L(R) WING TK OVERFLOW NO DISPATCH
L(R) XFR VALVE CLOSED or OPEN Refer to MEL 28-15-01, or
Refer to MEL 28-15-02
L(R) XFR VALVE FAULT Refer to MEL 28-21-02
X FEED VALVE FAULT NO DISPATCH
XFR VALVES FAULT Refer to MEL 28-21-02
01.03.12ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 29 HYDRAULIC POWER
ECAM WARNING ACTION DISPATCH CONDITION
HYD
B ELEC PUMP LO PR NO DISPATCH Actual caution
Refer to MEL 29-09-01 False caution
B ELEC PUMP OVHT NO DISPATCH Actual caution
Refer to MEL 29-09-02 False caution
B RSVR LO AIR PR NO DISPATCH Actual caution
Refer to MEL 29-09-04 False caution
B RSVR LO LVL NO DISPATCH Actual caution
Refer to MEL 29-09-05 False caution
B RSVR OVHT NO DISPATCH Actual caution
Refer to MEL 29-09-06 False caution
B SYS LO PR NO DISPATCH Actual caution
Refer to MEL 29-09-09 False caution
B + G SYS LO PR NO DISPATCH Actual warning
Refer to MEL 29-09-09 False warning
B + Y SYS LO PR NO DISPATCH Actual warning
Refer to MEL 29-09-09 False warning
G ENG 1 PUMP LO PR NO DISPATCH Actual caution
Refer to MEL 29-09-03 False caution
G RSVR LO AIR PR NO DISPATCH Actual caution
Refer to MEL 29-09-04 False caution
G RSVR LO LVL NO DISPATCH Actual alert
Refer to MEL 29-09-05 False alert
G RSVR OVHT NO DISPATCH Actual caution
Refer to MEL 29-09-06 False caution
G SYS LO PR NO DISPATCH Actual caution
Refer to MEL 29-09-09 False caution
G + Y SYS LO PR NO DISPATCH Actual warning
Refer to MEL 29-09-09 False warning
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 29 HYDRAULIC POWER
ECAM WARNING ACTION DISPATCH CONDITION
HYD
PTU FAULT NO DISPATCH Actual caution
Refer to MEL 29-09-07 False caution
RAT FAULT NO DISPTACH Actual caution
Refer to MEL 29-09-08 False caution
Y ELEC PUMP LO PR Refer to MEL 29-24-01 Actual caution
Refer to MEL 29-09-01 False caution
Y ELEC PUMP OVHT Refer to MEL 29-24-01 Actual alert
Refer to MEL 29-09-02 False alert
Y ENG 2 PUMP LO PR NO DISPATCH Actual caution
Refer to MEL 29-09-03 False caution
Y RSVR LO AIR PR NO DISPATCH Actual caution
Refer to MEL 29-09-04 False caution
Y RSVR LO LVL NO DISPATCH Actual caution
Refer to MEL 29-09-05 False caution
Y RSVR OVHT NO DISPATCH Actual caution
Refer to MEL 29-09-06 False caution
Y SYS LO PR NO DISPATCH Actual caution
Refer to MEL 29-09-09 False caution
01.03.14ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 30 ICE AND RAIN PROTECTION
ECAM WARNING ACTION DISPATCH CONDITION
ANTI ICE
ALL PITOT NO DISPATCH
CAPT (F/O) (STBY) AOA Refer to MEL 30-31-04
CAPT (F/0) (STBY) L(R) STAT Refer to MEL 30-31-03
CAPT (F/O) (STBY) PITOT Refer to MEL 30-31-02
CAPT + F/O PITOT NO DISPATCH
CAPT + STBY PITOT NO DISPATCH
CAPT (F/O) (STBY) PROBES Refer to MEL 30-31-01
CAPT (F/O) TAT Refer to MEL 30-31-05
DETECT FAULT Refer to MEL 30-81-01
ENG 1(2) VALVE CLSD or OPEN Refer to MEL 30-21-01
F/O + STBY PITOT NO DISPATCH
ICE DETECTED Not applicable
L(R) WINDOW Refer to MEL 30-42-01 If Window Heat Computer
affected
Refer to MEL 30-42-02
L(R) WINSHIELD Refer to MEL 30-42-01 If Window Heat Computer
affected
Refer to MEL 30-42-03
L + R WINSHIELD NO DISPATCH
SEVERE
ICE DETECTED Not applicable
WING ANTI ICE
L(R) HI PR Refer to MEL 30-11-01BL(R) VALVE OPEN Refer to MEL 30-11-01
OPEN ON GND Refer to MEL 30-11-01
SYS FAULT Refer to MEL 30-11-01
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 31 INDICATING/RECORDING SYSTEMS
ECAM WARNING ACTION DISPATCH CONDITION
EIS
DMC 1 FAULT Refer to MEL 31-62-01
DMC 2 FAULT Refer to MEL 31-62-02
DMC 3 FAULT Refer to MEL 31-62-03
FWS
FWC 1 FAULT NO DISPATCH
FWC 2 FAULT Refer to MEL 31-53-01
FWC 1 + 2 FAULT NO DISPATCH
OEB/FWC DISCREPANCY NO DISPATCH
SDAC 1 FAULT NO DISPATCH
SDAC 2 FAULT Refer to MEL 31-55-01
SDAC 1 + 2 FAULT NO DISPATCH
RECORDER
DFDR FAULT Refer to MEL 31-30-03
SYS FAULT Refer to MEL 31-30-05
01.03.16EICAS MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 32 LANDING GEAR
ECAM WARNING ACTION DISPATCH CONDITION
BRAKES
ALTN BRK FAULT NO DISPATCH
ALTN L(R) RELEASED NO DISPATCH
A/SKID N/WS FAULT NO DISPATCH
A/SKID N/WS OFF Not applicable
AUTO BRK FAULT Refer to MEL 32-42-05
BRK Y ACCU LO PR NO DISPATCH Actual caution
Refer to MEL 32-44-02 False cautionSYS 1 FAULT Refer to MEL 32-42-03
SYS 2 FAULT Refer to MEL 32-42-04
HOT NO DISPATCH Actual caution
Refer to MEL 32-07-01 False caution
NORM BRK FAULT NO DISPATCH
NORM + ALT FAULT NO DISPATCH
PARK BRK ON Not applicable
RELEASED Refer to MEL 32-42-02 If green brake supply affecte
Refer to MEL 32-42-06 If a tachometer affected
BRAKES-N/WS
MINOR FAULT Refer to MEL 32-09-01
CONFIG
PARK BRK ON NO DISPATCH
L/G
DOORS NOT CLOSED NO DISPATCH
GEAR NOT DOWN Not applicable
GEAR NOT DOWNLOCKED Not applicable
GEAR NOT UPLOCKED Not applicable
GEAR UPLOCK FAULT Refer to MEL 32-31-02
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 32 LANDING GEAR
ECAM WARNING ACTION DISPATCH CONDITION
L/G
LGCIU 1 FAULT NO DISPATCH
LGCIU 2 FAULT Refer to MEL 32-31-01 If the LGCIU 2 is inoperative
Refer to MEL 32-32-02, or If a RH L/G proximity detector
associated with the LGCIU 2 is
inoperative: apply the relevant
item
Refer to MEL 32-32-05, or
Refer to MEL 32-32-08, or Refer to MEL 32-32-11, or
Refer to MEL 32-32-14
Refer to MEL 32-32-03, or If a LH L/G proximity detector
associated with the LGCIU 2 is
inoperative: apply the relevant
item
Refer to MEL 32-32-06, or
Refer to MEL 32-32-09, or
Refer to MEL 32-32-12, or
Refer to MEL 32-32-15
Refer to MEL 32-32-04, or If a Nose L/G proximity detector
associated with the LGCIU 2 is
inoperative: apply the relevant
item
Refer to MEL 32-32-07, or
Refer to MEL 32-32-10, or
Refer to MEL 32-32-13, or
Refer to MEL 32-32-16
SHOCK ABSORBER FAULT NO DISPATCHSYS DISAGREE NO DISPATCH
01.03.18ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 32 LANDING GEAR
ECAM WARNING ACTION DISPATCH CONDITION
WHEEL
HYD SEL FAULT NO DISPATCH
N/W STRG FAULT Refer to MEL 32-51-01
TYRE LO PR NO DISPATCH Actual caution
Refer to MEL 32-09-02 False caution
ATA 34 NAVIGATION
ECAM WARNING ACTION DISPATCH CONDITION
NAV
ADR 1 FAULT Refer to MEL 34-10-01
ADR 2 FAULT Refer to MEL 34-10-02
ADR 3 FAULT Refer to MEL 34-10-03
ADR (1+2)(1+3)(2+3) FAULT NO DISPATCH
ADR 1+2+3 FAULT NO DISPATCH
ALTI DISCREPANCY Refer to MEL 34-10-01, or
Refer to MEL 34-10-02, or
Refer to MEL 34-10-03
ADR DISAGREE NO DISPATCH
ATT DISCREPANCY Refer to MEL 34-10-04, or
Refer to MEL 34-10-05, or
Refer to MEL 34-10-06, or
Refer to MEL 34-10-07
CAPT (F/O)(STBY) AOA FAULT Refer to MEL 34-11-01
FM/GPS POS DISAGREE Not applicable
GPS 1(2) FAULT Refer to MEL 34-50-09
GPWS FAULT Refer to MEL 34-40-01
GPWS TERR DET FAULT Refer to MEL 34-40-01
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 34 NAVIGATION
ECAM WARNING ACTION DISPATCH CONDITION
NAV
HDG DISCREPANCY Refer to MEL 34-10-04, or
Refer to MEL 34-10-05, or
Refer to MEL 34-10-06, or
Refer to MEL 34-10-07
IAS DISCREPANCY Refer to MEL 34-10-01, or
Refer to MEL 34-10-02, or Refer to MEL 34-10-03
ILS 1(2) (1 + 2) FAULT Refer to MEL 34-30-04
IR DISAGREE NO DISPATCH
IR NOT ALIGNED Refer to MEL 34-10-04, or
Refer to MEL 34-10-05, or
Refer to MEL 34-10-06, or
Refer to MEL 34-10-07
IR 1 FAULT Refer to MEL 34-10-04
IR 2 FAULT Refer to MEL 34-10-05
IR 3 FAULT Refer to MEL 34-10-06, or
Refer to MEL 34-10-07
IR (1+2)(1+3)(2+3) FAULT NO DISPATCH
LS 1(2)(1+2) FAULT Refer to MEL 34-30-04
PRED W/S DET FAULT (If installed) Refer to MEL 34-40-06
RA DEGRADED Refer to MEL 34-40-03
RA 1(2) FAULT Refer to MEL 34-40-03
TCAS FAULT Refer to MEL 34-40-04TCAS STANDBY Not applicable
OVERSPEED Not applicable
01.03.20ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 36 PNEUMATIC
ECAM WARNING ACTION DISPATCH CONDITION
AIR
APU BLEED FAULT Refer to MEL 36-12-02
APU BLEED LEAK Refer to MEL 36-12-01 Actual caution
Refer to MEL 36-22-03 False caution
BLEED 1(2) OFF Refer to MEL 36-11-01
ENG HP VALVE FAULT Refer to MEL 36-11-07
ENG 1(2) BLEED ABNORM PR Refer to MEL 36-11-01
ENG 1(2) BLEED FAULT Refer to MEL 36-11-01ENG 1(2) BLEED LEAK NO DISPATCH Actual caution
Refer to MEL 36-22-01 False caution
ENG 1(2) (1 + 2) BLEED LO TEMP Refer to MEL 36-11-04
ENG 1(2) BLEED NOT CLSD Refer to MEL 36-11-02
ENG 1(2) LEAK DET FAULT Refer to MEL 36-22-01
L(R) WING LEAK NO DISPATCH
L(R) WING LEAK DET FAULT NO DISPATCH
X BLEED FAULT Refer to MEL 36-12-04
BLEED
MONITORING FAULT NO DISPATCH
MONIT SYS 1(2) FAULT Refer to MEL 36-11-08
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 46 INFORMATION SYSTEM
ECAM WARNING ACTION DISPATCH CONDITION
DATALINK
ATC FAULT Refer to MEL 46-21-01
ATSU FAULT Refer to MEL 46-21-01
COMPANY FAULT Refer to MEL 46-21-01
ATA 49 AIRBORNE AUXILIARY POWER
ECAM WARNING ACTION DISPATCH CONDITION
APU
AUTO (EMER) SHUT DOWN Refer to MEL 49-10-01
ATA 52 DOORS
ECAM WARNING ACTION DISPATCH CONDITION
DOOR
AFT (BULK) (FWD) CARGO NO DISPTACH Actual caution
Refer to MEL 52-07-05 False caution
L(R) AFT AVIONICS NO DISPATCH Actual caution
Refer to MEL 52-07-06 False caution
L(R) AFT CABIN NO DISPATCH Actual caution
Refer to MEL 52-07-01 False caution
L(R) EMER EXIT (A320) NO DISPATCH Actual caution
Refer to MEL 52-07-03 False caution
L(R) EMER EXIT (A321) NO DISPATCH Actual caution
Refer to MEL 52-07-01 False caution
L(R) FWD AVIONICS NO DISPATCH Actual alert
Refer to MEL 52-07-06 False alert
L(R) FWD CABIN NO DISPATCH Actual caution
Refer to MEL 52-07-01 False caution
01.03.22ECAM MESSAGES
A320/A321MEL/CDL 12 FEB 12
MEL
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ATA 52 DOORS
ECAM WARNING ACTION DISPATCH CONDITION
DOOR
L(R) FWD EMER EXIT (A320) NO DISPATCH Actual alert
Refer to MEL 52-07-03 False alert
L(R) FWD EMER EXIT (A321) NO DISPATCH Actual alert
Refer to MEL 52-07-01 False alert
ATA 70 ENGINE
ECAM WARNING ACTION DISPATCH CONDITION
ENG
COMPRESSOR VANE NO DISPATCH
DUAL FAILURE Not applicable
THR LEVERS NOT SET Refer to MEL 73-20-01
REV SET Not applicable
THRUST LOCKED Not applicable
TYPE DISAGREE NO DISPATCH
VIB SYS FAULT Refer to MEL 77-07-02-05, or
Refer to MEL 77-07-02-06
ENG 1(2)
BLEED STATUS FAULT Apply ECAM procedure If this alert is displayed on th
EWD before the first engine
start, check that no amber
cross is displayed on the EN
SD page for OIL TEMP
indication of the affected
engine. If an amber cross is
displayed, the associated EIUmay be the cause of the
failure (associated engine
start not possible).
12 FEB 12MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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ATA 70 ENGINE
ECAM WARNING ACTION DISPATCH CONDITION
ENG 1(2)
COMPRESSOR VANE NO DISPATCH
CTL VALVE FAULT NO DISPATCH
EGT (FF)(N1)(N2) DISCREPANCY NO DISPATCH
EIU FAULT NO DISPATCH
FADEC A(B) FAULT NO DISPATCH
FADEC ALTERNATOR NO DISPATCHFADEC FAULT NO DISPATCH
FADEC HI TEMP NO DISPATCH
FAIL Not applicable
FUEL CTL FAULT NO DISPATCH
FUEL FILTER CLOG NO DISPATCH Actual alert
Refer to MEL 73-09-01 False alert
FUEL RETURN VALVE Refer to MEL 73-10-01
HP FUEL VALVE NO DISPATCH
IGN A(B) FAULT Refer to MEL 74-31-01 or
MEL 74-31-02
Actual alert
Refer to MEL 74-09-01 False alert
IGN A+B FAULT NO DISPATCH Actual alert
Refer to MEL 74-09-01 False alert
LOW N1 NO DISPATCH
N1(N2)(EGT) OVER LIMIT Not applicable
OIL FILTER CLOG NO DISPATCH Actual alert
Refer to MEL 79-09-02 False alert
OIL HI TEMP NO DISPATCH
OIL LO PR NO DISPATCH Actual alert
Refer to MEL 79-09-01 False alert
ONE TLA FAULT Refer to MEL 76-11-01
01.03.24ECAM MESSAGES
A320/A321MEL/CDL 01 MAY 12
MEL
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ATA 70 ENGINE
ECAM WARNING ACTION DISPATCH CONDITION
ENG 1(2)
OVSPD PROT FAULT NO DISPATCH
PROBES FAULT
ENG 1(2) REV INHIBITED Refer to MEL 78-30-01
NO DISPATCH
REV ISOL FAULT Refer to MEL 78-30-03
REV PRESSUREIZED NO DISPATCH
REV SWITCH FAULT Refer to MEL 78-30-02
REVERSE UNLOCKED NO DISPATCH
REVERSER FAULT Refer to MEL 78-30-01
SENSOR FAULT NO DISPATCH
SHUT DOWN Not applicable
STALL Not applicable
START FAULT Apply ECAM procedure If the associated THR LEVER
NOT AT IDLE message is
displayed
Refer to FCOM/PRO-SUP-70
START VALVE FAULT Refer to MEL 80-11-01
THR LEVER ABV IDLE Not applicable
THR LEVER DISAGREE NO DISPATCH
THR LEVER FAULT NO DISPATCH
* * *
MEL
A320/A321MEL/CDL 01.03
ECAM MESSAG
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THIS PAGE INTENTIONALLY LEFT BLANK
01.03.26ECAM MESSAGES
A320/A321MEL/CDL
MEL
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21 AIR CONDITIONING
21-00 MAINTENANCE
Messages on the
STATUS SD page
21-00-03 AFT CRG HEAT
MAINTENANCE
Message
21-00-03A C 1 - AFT CRG HEAT MAINTENANCE message may be
displayed on the STATUS SD page.
21-00-04 TEMP CTL 1(2)
MAINTENANCE
Message
21-00-04A C 2 - TEMP CTL 1(2) MAINTENANCE message may be
displayed on the STATUS SD page.
21-01 Overhead Panels
21-01-01 AIR COND
Overhead Panel
21-01-01-01 PACK pb-sw
FAULT light
21-01-01-01A C 2 0 One or both may be inoperative provided ECAM BLEED
page displaying system operative.
21-01-01-02 PACK pb-sw
OFF light
21-01-01-02A C 2 0 One or both may be inoperative provided ECAM BLEED
page displaying system operative.
21-01-01-03 HOT AIR pb-swFAULT light
21-01-01-03A C 1 0 May be inoperative provided that all zone duct
temperature indications are operative on the COND SD
page.
12 FEB 12MEL
A320/321MEL/CDL 01.21.01
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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21 AIR CONDITIONING
21-01 Overhead Panels
21-01-01 AIR COND
Overhead Panel
21-01-01-04 HOT AIR pb-sw
OFF light
21-01-01-04A C 1 0 May be inoperative.
21-01-02 CABIN PRESS
Overhead Panel
21-01-02-01 CABIN PRESS
MODE SEL pb-
sw FAULT light
21-01-02-01A C 1 0 May be inoperative.
21-01-03 CARGO VENT
Overhead Panel
21-01-03-02 AFT ISOLVALVE pb-sw
FAULT light
21-01-03-02A C 1 0 May be inoperative.
21-01-04 VENTILATION
Overhead Panel
21-01-04-01 CAB FANS pb-
sw OFF light
21-01-04-01A C 1 0 May be inoperative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.02
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-01 Overhead Panels
21-01-04 VENTILATION
Overhead Panel
21-01-04-02 BLOWER pb-sw
FAULT light
21-01-04-02A C 1 0 May be inoperative.
21-01-04-03 EXTRACT pb-sw
FAULT light
21-01-04-03A C 1 0 May be inoperative.
21-07 Indications on SD
pages
21-07-01 Indications on theBLEED SD page
21-07-01-01 Pack Outlet
Temperature
Indication on the
BLEED SD page
21-07-01-01A C 2 0 One or both may be inoperative.
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.03
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-07 Indications on SD
pages
21-07-01 Indications on the
BLEED SD page
21-07-01-02 Pack Turbine
Bypass Valve
Position
Indication on the
BLEED SD page
21-07-01-02A C 2 0 One or both may be inoperative.
21-07-01-03 Pack
Compressor
Outlet
Temperature
Indication on the
BLEED SD page
21-07-01-03A C 2 0 One or both may be inoperative.
21-07-01-04Pack Flow
Indication on the
BLEED SD page
21-07-01-04A C 2 0 One or both may be inoperative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.04
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-07 Indications on SD
pages
21-07-01 Indications on the
BLEED SD page
21-07-01-05 Pack Flow
Control Valve
Position
Indication on the
BLEED SD page
21-07-01-05A C 2 0 One or both may be inoperative.
21-07-01-06Emergency Ram
Air Inlet Indication
on the BLEED SD
page
21-07-01-06A C 1 0 May be inoperative.
21-07-02 Indications on the
CAB PRESS SDpage
21-07-02-01INLET and
EXTRACT
Indications on the
CAB PRESS SD
page
21-07-02-01A C 2 0 One or both may be inoperative.
Note:
During ground operations, correctavionics ventilation should be provided.
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.05
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-07 Indications on SD
pages
21-07-02 Indications on the
CAB PRESS SD
page
21-07-02-02 Pressure Safety
Valves Position
Indication on theCAB PRESS SD
page
21-07-02-02A C 1 0 (M) Pressure safety valves may be indicated open provided
that both valves are visually checked closed.
MAINTENACE PROCEDURE
Refer to AMM 21-31-00-040-004
21-07-02-03 Pack 1 and 2
Indications on
the CAB PRESSSD page
21-07-02-03A C 2 0 One or both may be inoperative.
21-07-03 Indications on the
COND SD page
21-07-03-01Indications on the
COND SD page
21-07-03-01A C 2 0 One or more indications may be inoperative.
21-07-04 Indications on the
CRUISE SD page
21-07-04-01A C 2 0 Cabin and cockpit zone indications may be inoperative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.06
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-09 ECAM Alerts
21-09-01 VENT BLOWER
FAULT Alert
Note:
During ground operations, correct
avionics ventilation should be provided.
21-09-01A Blower fan
operative
C 1 0 (O)(M) May be displayed provided that:
1) The blower fan is checked operative before each flight,
and
2) The VENT AVNCS SYS FAULT alert is checkedoperative before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Disregard the VENT BLOWER FAULT alert displayed on
the EWD.
Disregard the BLOWER pb-sw FAULT light illuminated on
the VENTILATION Overhead Panel.
Note:
If the ground horn sounds:
EIS/HORN/SPLY (121VU P09)
C/B . . . . . . . . . . . . . . . . . . . . . . . . .Pull
The C/B must be closed again after first
engine start
If the ground horn sounds after landing
when engines are off, it can be silenced
again. In this case, the ADIRS must be
set to OFF before leaving the aircraft.
MAINTENACE PROCEDURE
Refer to AMM 21-26-00-040-010
21-09-01B Blower fan
inoperative
C 1 0 May be displayed provided that the avionics blower fan is
considered inoperative.
Refer to Item 21-26-01 Avionics Blower Fan
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.07
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-09 ECAM Alerts
21-09-02 VENT EXTRACT
FAULT Alert
Note:
During ground operations, correct
avionics ventilation should be provided.
21-09-02A Extract fan
operative
C 1 0 (O)(M) May be displayed provided that:
1) The extract fan is checked operative before eachflight, and
2) The VENT AVNCS SYS FAULT alert is checkedoperative before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Disregard the VENT EXTRACT FAULT alert displayed on
the EWD.
MAINTENACE PROCEDURE
Refer to AMM 21-26-00-040-011
21-09-02B Extract fan
inoperative
C 1 0 May be displayed provided that the avionics extract fan is
considered inoperative.
Refer to Item 21-26-02 Avionics Extract Fan
21-09-03 CAB PR SAFETY
VALVE OPEN
Alert
21-09-03A C 1 0 (M) May be displayed provided that both safety valves are
visually checked closed.
MAINTENACE PROCEDURE
Refer to AMM 21-31-00-040-005
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.08
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-21 Air Distribution
and Recirculation
21-21-01 Cabin Fan
21-21-01A C 2 1 One may be inoperative.
21-23 Lavatory and
Galley Ventilation
21-23-01 Lavatory and
Galley Extraction
Fan
21-23-01B C 1 0 (O) May be inoperative provided that all duct temperatures
indications for the cabin are operative on the COND SD
page.
OPERATING PROCEDURES
GENERAL INFORMATION
Two amber crosses replace the cabin zone temperature
indications on the COND SD page.Refer to Item 21-07-03-01 Indications on the COND SD
page
The INOP SYS column on the STATUS SD page may
display the LAV DET message.
The cabin zone temperature regulation is lost.
The Air Conditioning System Controller commands FWD
and AFT cabin ducts temperature using the position of the
FWD CABIN selector and the AFT CABIN selector on the
AIR COND overhead panel.
Slight effect on cabin comfort may occur.
The cockpit temperature regulation is still operative.
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.09
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-01 Avionics Blower
Fan
Note:
During ground operation, correct
avionics ventilation should be provided.
21-26-01A VENT AVNCS
SYS FAULT not
displayed
C 1 0 (O) May be inoperative provided that:
1) The BLOWER pb-sw is set to OVRD,
2) Both air conditioning packs are operative, and
3) The VENT AVNCS SYS FAULT alert is notdisplayed.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning correctly operates with
both air conditioning packs set to on.
- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Check that the VENT AVNCS SYS FAULT and VENT
EXTRACT FAULT alerts are not displayed on the EWD.
· If the VENT EXTRACT FAULT alert is displayed on
the EWD, the blower fan may be seized. In that case:
- Contact the maintenance personnel to exchange the
blower fan and the extract fan.
Only the VENT EXTRACT FAULT alert must then be
displayed on the EWD.
- When the blower and extract fans are exchanged, Refer
to Item 21-26-02 Avionics Extract Fan
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.10
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-01 Avionics Blower
Fan
21-26-01B Air conditioning
inlet valve
checked open
C 1 0 (O)(M) May be inoperative provided that:
1) The BLOWER pb-sw is set to OVRD,
2) Both air conditioning packs are operative, and
3) The air conditioning inlet valve is checked open beforeeach flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning correctly operates with
both air conditioning packs set to on.
- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Check that the VENT EXTRACT FAULT alert is not
displayed on the EWD
· If the VENT EXTRACT FAULT alert is displayed on
the EWD, the blower fan may be seized. In that case:
- Contact the maintenance personnel to exchange the
blower fan and the extract fan.
Only the VENT EXTRACT FAULT alert must then be
displayed on the EWD.
- When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract Fan
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-006
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.11
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-01 Avionics Blower
Fan
21-26-01C Avionics
ventilation
system checked
C 1 0 (O)(M) May be inoperative provided that:
1) The BLOWER pb-sw is set to OVRD,
2) Both air conditioning packs are operative,
3) The air conditioning inlet valve is secured in theopen position, and
4) The avionics ventilation system is checked beforeeach flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that air the conditioning correctly operates with
both air conditioning packs set to on.
- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Check that the VENT EXTRACT FAULT alert is not
displayed on the EWD
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert using the CLR
pb.
The VENT AVNCS SYS FAULT alert will be displayedafter landing
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.12
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-01 Avionics Blower
Fan
21-26-01C Avionics
ventilation
system checked
(cont’d) OPERATING PROCEDURES (cont’d)
· If the VENT EXTRACT FAULT alert is displayed on
the EWD, the blower fan may be seized. In that case:
- Contact the maintenance personnel to exchange the
blower fan and the extract fan.
Only the VENT EXTRACT FAULT alert must then be
displayed on the EWD.
- When the blower and extract fans are exchanged, Refer
to Item 21-26-02 Avionics Extract Fan
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-013
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.13
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-02 Avionics Extract
Fan
Note:
During ground operation, correct
avionics ventilation should be provided.
21-26-02A VENT AVNCS
SYS FAULT not
displayed
C 1 0 (O) May be inoperative provided that:
1) The blower fan is operative,
2) The EXTRACT pb-sw is set to OVRD,
3) Both air conditioning packs are operative, and
4) The VENT AVNCS SYS FAULT alert is notdisplayed.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Time limitation on ground with electrical network supplied:
OAT (°C) £ 38 £ 45 £ 55
MAX TIME No limit 3 h 35 min
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning correctly operates with
both air conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Clear the VENT EXTRACT FAULT alert using the CLR
pb.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.14
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-02 Avionics Extract
Fan
21-26-02A VENT AVNCS
SYS FAULT
not displayed
(cont’d)
OPERATING PROCEDURES (Cont’d)
- AVNCS VENT/EXTC/FAN (123VU AE2) (A320)
- AVNCS VENT/EXTC/FAN (123VU AC4) (A321)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
- Check that the VENT AVNCS SYS FAULT alert is not
displayed on the EWD.
Note:
If the ground horn sounds:
EIS/HORN/SPLY (121VU P09)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . Pull
The C/B must be closed again after first
engine start
If the ground horn sounds after landing
when engines are off, it can be silenced
again. In this case, the ADIRS must be
set to OFF before leaving the aircraft.
21-26-02B Air conditioning
inlet valve
checked open
C 1 0 (O)(M) May be inoperative provided that:
1) The blower fan is operative,
2) The EXTRACT pb-sw is set to OVRD,
3) Both air conditioning packs are operative, and
4) The air conditioning inlet valve is checked open beforeeach flight.
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.15
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-02 Avionics Extract
Fan
21-26-02B Air conditioning
inlet valve
checked open
(cont’d)
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Time limitation on ground with electrical network supplied:
OAT (°C) £ 38 £ 45 £ 55
MAX TIME No limit 3 h 35 min
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning correctly operates withboth air conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Clear the VENT EXTRACT FAULT alert using the CLR
pb.
- AVNCS VENT/EXTC/FAN (123VU AE2 or AC4)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.16
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-02 Avionics Extract
Fan
21-26-02B Air conditioning
inlet valve
checked open
OPERATING PROCEDURES (cont’d)
Note:
If the ground horn sounds:
EIS/HORN/SPLY (121VU P09)
C/B. . . . . . . . . . . . . . . . . . . . . . . . . . Pull
The C/B must be closed again after first
engine start
If the ground horn sounds after landing
when engines are off, it can be silenced
again. In this case, the ADIRS must be
set to OFF before leaving the aircraft.
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-007
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.17
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-02 Avionics Extract
Fan
21-26-02C Avionics
ventilation
system checked
C 1 0 (O)(M) May be inoperative provided that:
1) The blower fan is operative,
2) The EXTRACT pb-sw is set to OVRD,
3) Both air conditioning packs are operative,
4) The air conditioning inlet valve is secured in theopen position, and
5) The avionics ventilation system is checked beforeeach flight.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Time limitation on ground with electrical network supplied:
OAT (°C) £ 38 £ 45 £ 55
MAX TIME No limit 3 h 35 min
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning correctly operates with
both air conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Clear the VENT EXTRACT FAULT alert using the CLR
pb.
- AVNCS VENT/EXTC/FAN (123VU AE2 or AC4)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.18
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-02 Avionics Extract
Fan
21-26-02C Avionics
ventilation
system checked
(cont’d)
OPERATING PROCEDURES (Cont’d)
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert using the CLR
pb.
The VENT AVNCS SYS FAULT alert will be displayed
after landing.
Note:
If the ground horn sounds:
EIS/HORN/SPLY (121VU P09)
C/B. . . . . . . . . . . . . . . . . . . . . . . . . . PullThe C/B must be closed again after first
engine start
If the ground horn sounds after landing
when engines are off, it can be silenced
again. In this case, the ADIRS must be
set to OFF before leaving the aircraft.
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-015
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.19
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-03 Avionics Skin
Exchanger Inlet
Bypass Valve
21-26-03A C 1 0 (O)(M) May be inoperative provided that:
1) The avionics skin exchanger inlet bypass valve is
manually secured in the closed position, and2) The avionics ventilation system is checked before
each flight.
Note:
During ground operations, correct
avionics ventilation should be provided.
OPERATING PROCEDURES
ON GROUND
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed
after landing.
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-001
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.20
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-04 Avionics Skin Air
Outlet Valve
21-26-04A C 1 0 (O)(M) May be inoperative provided that:
1) The internal flap is manually secured in the openposition,
2) The skin air outlet valve is displayed in a partially openposition amber or green on the CAB PRESS SD page,
3) Both air conditioning packs are operative,
4) The skin exchanger isolation valve is secured in theopen position, and
5) The avionics ventilation system is checked beforeeach flight.
Note:
During ground operations, correct
avionics ventilation should be provided.
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.21
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-04 Avionics Skin Air
Outlet Valve
21-26-04A (cont’d) OPERATING PROCEDURES
ON GROUND
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed
after landing.
· If the VENT SKIN VALVE FAULT alert is displayed
on the EWD:
Apply the ECAM procedure.
Note: Avionics smoke may be not perceptible
from the cockpit due to the opening of
the internal flap of the valve.
In the case of AVIONICS SMOKE alert:
Apply the ECAM procedure even if the
smoke is not perceptible.
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-002
21-26-05 Avionics Skin Air Inlet Valve
Note:
During ground operations, correct
avionics ventilation should be provided.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.22
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-05 Avionics Skin Air
Inlet Valve (cont’d)
21-26-05A Air Conditioning
Inlet Valve open
on ground
C 1 0 (O)(M) May be inoperative provided that:
1) The avionics skin air inlet valve is manually secured in
the closed position,2) The air conditioning inlet valve is open on ground, and
3) The avionics ventilation system is checked beforeeach flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning is operating with both air
conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Check that the skin air inlet valve is closed on the CAB
PRESS SD page.
- Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
Note:
With only one air conditioning pack
operative, operating time on ground is
limited to 1 h.
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.23
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-05 Avionics Skin Air
Inlet Valve
21-26-05A Air Conditioning
Inlet Valve open
on ground
(cont’d) OPERATING PROCEDURES (Cont’d)
AFTER TAKEOFF
EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
AFTER LANDING
EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-004
21-26-05B Air Conditioning
Inlet Valve
Secured Open
C 1 0 (O)(M) May be inoperative provided that:
1) The avionics skin air inlet valve is manually securedin the closed position,
2) The air conditioning inlet valve is secured in theopen position, and
3) The avionics ventilation system is checked beforeeach flight.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.24
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-05 Avionics Skin Air
Inlet Valve
21-26-05B Air Conditioning
Inlet Valve
Secured Open
(Cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning is operating with both air
conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Check that the skin air inlet valve is closed on the CAB
PRESS SD page.
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed
after landing.
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.25
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-05 Avionics Skin Air
Inlet Valve
21-26-05B Air Conditioning
Inlet Valve
Secured Open
(cont’d) OPERATING PROCEDURES (Cont’d)
Note:
With only one air conditioning pack
operative, operating time on ground is
limited to 1 h.
AFTER TAKEOFF
EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
AFTER LANDING
EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-014
21-26-06 Avionics Skin
Exchanger
Isolation Valve
Note:
During ground operations, correct
avionics ventilation should be provided.
21-26-06A Valve
inoperative in
the open
position
C 1 0 (O)(M) May be inoperative in the open position provided that the
avionics ventilation system is checked before each flight.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.26
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-06 Avionics Skin
Exchanger
Isolation Valve
21-26-06A Valve
inoperative in
the open
position (cont’d) OPERATING PROCEDURES
ON GROUND
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
MAINTETNANCE PROCEDURE
Refer to AMM 21-26-00-040-008
21-26-06B Valve secured
open
C 1 0 (O)(M) May be inoperative provided that:
1) The avionics skin exchanger isolation valve is securedin the open position, and
Note:
If the valve cannot be secured in the
open position, it can be interchanged
with the skin exchanger outlet bypass
valve.
2) The avionics ventilation system is checked before
each flight.
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.27
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-06 Avionics Skin
Exchanger
Isolation Valve
21-26-06B Valve secured
open (Cont’d) OPERATING PROCEDURES
ON GROUND
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
MAINTETNANCE PROCEDURE
Refer to AMM 21-26-00-040-016
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.28
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-07 Avionics Skin
Exchanger Outlet
Bypass Valve
21-26-07A C 1 0 May be inoperative.
Note:
During ground operations, correct
avionics ventilation should be provided.
21-26-08 Avionics Air
Conditioning Inlet
Valve
21-26-08A C 1 0 (O)(M) May be inoperative provided that:
1) The avionics air conditioning inlet valve is manuallysecured in the open position,
2) Both air conditioning packs are operative, and3) The avionics ventilation is checked before each flight.
Note:
During ground operations, correct
avionics ventilation should be provided.
OPERATING PROCEDURES
ON GROUND
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
MAINTETNANCE PROCEDURE
Refer to AMM 21-26-00-040-003
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.29
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-09 Avionics
Ventilation Filte
Note:
During ground operations, correct
avionics ventilation should be provided.
21-26-09A VENT AVNCS
SYS FAULT notdisplayed
C 1 0 (O) May be inoperative (clogged) provided that:
1) The blower and extract fans are operative,
2) The EXTRACT pb-sw is set to OVRD,
3) Both air conditioning packs are operative, and
4) The VENT AVNCS SYS FAULT alert is notdisplayed.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning is operating with both air
conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- Check that the VENT AVNCS SYS FAULT alert is not
displayed on the EWD.
21-26-09B Valve checked
open
C 1 0 (O)(M) May be inoperative (clogged) provided that:
1) The blower and extract fans are operative,
2) The EXTRACT pb-sw is set to OVRD,3) Both air conditioning packs are operative, and
4) The air conditioning inlet valve is checked openbefore each flight.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.30
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-09 Avionics
Ventilation Filte
21-26-09B Valve checked
open (cont’d)
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning is operating with both air
conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
MAINTETNANCE PROCEDURE
Refer to AMM 21-26-00-040-009
21-26-09C Valve secured
open
C 1 0 (O)(M) May be inoperative (clogged) provided that:
1) The blower and extract fans are operative,
2) The EXTRACT pb-sw is set to OVRD,
3) Both air conditioning packs are operative,
4) The air conditioning inlet valve is secured in the openposition, and
5) The avionics ventilation system is checked beforeeach flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the air conditioning is operating with both air
conditioning packs set to on.
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.31
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-09 Avionics
Ventilation Filte
21-26-09C Valve secured
open (cont’d) OPERATING PROCEDURES (Cont’d)
· After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed
after landing.
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-017
21-26-10 Avionics
Equipment
VentilationComputer (AEVC)
21-26-10A C 1 0 (O)(M) May be inoperative provided that:
1) Both air conditioning packs are operative,
2) The BLOWER pb-sw and the EXTRACT pb-sw areset to OVRD,
3) The air conditioning inlet valve and the skin air outletvalve are checked in the correct position beforeeach flight,
4) The extract fan is checked operative before eachflight, and
5) The skin air inlet valve is secured in the closedposition.
Note:
During ground operations, correct
avionics ventilation should be provided.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.32
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics
Equipment
Ventilation
21-26-10 Avionics
Equipment
Ventilation
Computer (AEVC)
21-26-10A (cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- Supply the aircraft electrical network.
- Check that the conditioning is operating with both air
conditioning packs set to on.
- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
Note:
If the ground horn sounds:EIS/HORN/SPLY (121VU P09)
C/B. . . . . . . . . . . . . . . . . . . . . . . . . . Pull
The C/B must be closed again after first
engine start
If the ground horn sounds after landing
when engines are off, it can be silenced
again. In this case, the ADIRS must be
set to OFF before leaving the aircraft.
Note:
In the case of a low pressure in the
avionics compartment ventilation ducts,
the weather radar image may not be
displayed on the ND on ground.
Clear the VENT AVNCS SYS FAULT alert displayed on
the EWD using the CLR pb
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.33
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-26 Avionics Equipment
Ventilation
21-26-10 Avionics
Equipment
Ventilation
Computer (AEVC)
21-26-10A (cont’d) OPERATING PROCEDURES (Cont’d)
IN FLIGHT
· In the case of an air conditioning pack failure:
- The cabin altitude may reach about 9 700 ft, and
- The CAB PR EXCESS CAB ALT alert may be displayed
on the EWD.
MAINTENANCE PROCEDURE
Refer to AMM 21-26-00-040-005
21-28 Cargo CompartmentVentilation
21-28-03 AFT Cargo
Extraction Fan
21-28-03A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Live animals must not be carried in the aft cargo
compartment.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.34
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-28 Cargo
Compartment
Ventilation
21-28-04 AFT Cargo
Isolation Valve
21-28-04A AFT ISOL
VALVE pb-sw
FAULT light
operative
C 2 0 (O) One or both may be inoperative provided that:
1) Both valves are checked closed, and
2) AFT ISOL VALVE pb-sw FAULT light is checkedoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Live animals must not be carried in the aft cargo
compartment.
DURING COCKPIT PREPARATION
- ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . TEST
- Check that the AFT ISOL VALVE pb-sw FAULT light
comes on
- ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . BRT or
DIM
- AFT ISOL VALVE pb-sw. . . . . . . . . . . . . . . . . . . OFF
- Check that the AFT ISOL VALVE pb-sw FAULT light
does not come on.
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.35
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-28 Cargo Compartment
Ventilation
21-28-04 AFT Cargo
Isolation Valve
21-28-04A AFT ISOL
VALVE pb-sw
FAULT light
operative
(cont’d) OPERATING PROCEDURES (cont’d)
Note:
· If the AFT ISOL VALVE pb-sw FAULT light comes
on:
The AFT cargo isolation valve must be secured in the
closed position. Refer to Item 21-28-04B AFT Cargo
Isolation Valve
21-28-04B Both valves
secured closed
C 1 0 (O)(M) One or both may be inoperative provided that both valves
are secured in the closed position.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Live animals must not be carried in the aft cargo
compartment.
ON GROUND
· When the AFT cargo isolation valves are secured in
the closed position:
The AFT isolation valves are displayed open green on theCOND SD page.
MAINTENANCE PROCEDURE
Refer to AMM 21-28-00-040-002
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.36
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-31 Pressure Control
and Monitoring
21-31-01 Automatic Cabin
Pressure Control
System (CPC,
Outflow Valve
AUTO Channel)
21-31-01A Automatic CPC
1 inoperative
A 2 1 (O)(M) Automatic cabin pressure control system 1 may be
inoperative for three flight days provided that:
1) It is deactivated,
2) The cabin pressure indications on the CAB PRESS SDpage are checked operative in manual mode,
3) The LDG ELEV selector MAN function is operative,and
4)Extanded overwater flight is prohibited.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
· If CPC 1 is affected:
AIR COND/CAB/PRESS/CTL 1 (49VU D09)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
· If CPC 2 is affected:
AIR COND/CAB/PRESS/CTL 2 (122VU Y22)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
- RPCU (122VU X23) C/B . . . . . . . . . . . . . . . . . . . Pull
- MODE SEL pb-sw. . . . . . . . . . . . . . . . . . . . . . . . MAN
- On the CAB PRESS SD page, check that the cabin
differential pressure, the cabin vertical speed, the cabin
altitude, and the outflow valve position are available.
(Cont’d on next page)
I T E M
30 JUN 12MEL
A320/321MEL/CDL 01.21.37
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-31 Pressure Control and
Monitoring
21-31-01 Automatic Cabin
Pressure Control
System (CPC,
Outflow Valve
AUTO Channel)
21-31-01A Automatic CPC
1 inoperative
(cont’d) OPERATING PROCEDURES (cont’d)
- MAN V/S CTL sw . . . . . . . . . . . . . . . . . . . . . . . . DN
- On the CAB PRESS SD page, check outflow valve
movement.
- RPCU (122VU X23) C/B . . . . . . . . . . . . . . . . . . . Push
- MODE SEL pb-sw. . . . . . . . . . . . . . . . . . . . . . . . AUTO
21-31-01B Automatic CPC
2 inoperative
C 2 1 (O)(M) Automatic cabin pressure control system 2 may be
inoperative provided that:
1) It is deactivated,
2) The cabin pressure indications on the CAB PRESSSD page are checked operative in manual mode,and
3) The LDG ELEV selector MAN function is operative.
OPERATING PROCEDURES
Refer to item 21-31-01A for operating procedures
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.38
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-31 Pressure Control
and Monitoring
21-31-01 Automatic Cabin
Pressure Control
System (CPC,
Outflow Valve
AUTO Channel)
21-31-01C Both automatic
CPCs
inoperative
C 2 0 Both may be inoperative provided that:
1) The manual cabin pressure control system isoperative, and
2) The flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Fligt Without Cabin
Pressurized.
Flight must conducted in accordance with FOPM CH 8
Maintenance Ferry Flights.
21-31-02 Manual CabinPressure Control
System (MAN V/S
CTL selector,
Outflow Valve
MAN Channel)
21-31-02A C 1 0 (M) May be inoperative provided that:
1) The LDG ELEV selector MAN function is operative,and
2) Both automatic cabin pressure control systems arechecked operative before each flight.
MAINTENANCE PROCEDURE
Refer to AMM 21-31-00-040-002
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.39
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-31 Pressure Control and
Monitoring
21-31-03 Pressure Safety
Valve
21-31-03A C 2 1 (M) One may be inoperative in the closed position provided
that:
1) Both automatic cabin pressure control systems are
operative, and2) The three outflow valve motors are checked
operative.
MAINTENANCE PROCEDURE
Refer to AMM 21-31-00-040-001
21-31-04 Landing Elevation
Selection AUTO
Function
21-31-04A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
BEFORE TAKEOFF
- Set the LDG ELEV selector on the CABIN PRESS panel
at the destination airport altitude.
- On the CAB PRESS SD page, check that the LDG ELEV
MAN message is displayed .
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.40
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-31 Pressure Control
and Monitoring
21-31-05 Landing Elevation
Selection MAN
Function
21-31-05A C 1 0 (O) May be inoperative provided that:
1) The landing elevation selection AUTO function is
operative, and2) Both FMGCs are operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
On the CAB PRESS SD page, check that the LDG ELEV
AUTO message is displayed to confirm correct position of
the LDG ELEV selector.
Note:
The landing field elevation of the
destination airport may not be correctly
displayed on the CAB PRESS SD page.
It is automatically corrected after first
engine start.
21-43 Cargo
Compartment
Heating
21-43-02 AFT Cargo
Compartment
Heating
21-43-02A HOT AIR pb-sw
OFF
C 1 0 (O) Hot air pressure regulating valve or trim air valve may be
inoperative provided that:
1) The HOT AIR pb-sw on the CARGO HEAT overheadpanel is set to OFF, and
2) The operative valve is indicated closed on the CONDSD page.
(Cont’d on next page)
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.21.41
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-43 Cargo Compartment
Heating
21-43-02 AFT Cargo
Compartment
Heating
21-43-02A HOT AIR pb-sw
OFF (cont’d)
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
AFT CARGO compartment heat is not be available. Live
animals and/or temperature sensitive cargo, must not be
carried in the aft cargo compartment.
DURING COCKPIT PREPARATION
- HOT AIR pb-sw (on the CARGO HEAT overhead
panel)...................................................... OFF
- On the COND SD page, check that the operative valve
(either the hot air pressure regulating valve or the trim air
valve) is indicated closed.
21-43-02B Valves secured
closed
C 1 0 (O)(M) Hot air pressure regulating valve or trim air valve may be
inoperative provided that one of these valves is secured in
the closed position.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
AFT CARGO compartment heat is not be available. Live
animals and/or temperature sensitive cargo, must not be
carried in the aft cargo compartment.
MAINTENANCE PROCEDURERefer to AMM task
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.42
AIR CONDITIONING
A320/321MEL/CDL
12 FEB 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-51 Pack Flow Control
21-51-02 Pack Flow
Selection
21-51-02A C 1 0 May be inoperative.
21-51-03 Pack Flow Sensor
21-51-03A C 2 1 (O) One may be inoperative.
OPERATING PROCEDURE
GENERAL INFORMATION
The hot air pressure regulating valve automatically closes.
The Flow Control Valve on the affected side operates in
pneumatic backup mode.
DURING COCKPIT PREPERATION
AIR COND HOT AIR pb-sw. . . . . . . . . . . . . . . . . . OFF
21-52 Air Cooling
System
21-52-01 Air Conditioning
Pack
21-52-01D No FL
limitation
C 2 1 (O)(M)
(FD)
One may be inoperative provided that:
1) The following alerts:
AIR PACK 1(2) REGUL FAULT AIR COND CTL 1(2)-A FAULT AIR COND CTL 1(2)-B FAULTassociated with the operative pack are not displayed
on the EWD, and
2) The affected PACK 1(2) pb-sw is set to OFF, and
3) The speedbrakes are operative, and
4) The associated pack flow control valve is secured inthe closed position.
(Cont’d on next page)
I T E M
01 MAY 12MEL
A320/321MEL/CDL 01.21.43
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-52 Air Cooling System
21-52-01 Air Conditioning
Pack
21-52-01D No FL
limitation
(cont’d)
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
PACK FLOW pb-sw (A320) . . . . . . . . . . . . . . . . . HI
ECON FLOW pb-sw (A321) . . . . . . . . . . . . . . . . . Off
IN FLIGHT
· If BLOWER pb-sw and EXTRACT pb-sw are set to
OVRD:
- The cabin altitude may reach about 9,700 ft, and
- The CAB PR EXCESS CAB ALT alert may be displayed
on the EWD
MAINTENANCE PROCEDURE
Refer to AMM 21-51-00-040-002
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.21.44
AIR CONDITIONING
A320/321MEL/CDL
01 MAY 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-52 Air Cooling
System
21-52-01 Air Conditioning
Pack
21-52-01E Limitation to
31 500 ft
C 2 1 (O)(M)
(FD)
One may be inoperative provided that:
1) The flight altitude is limited to 31 500 ft, and
2) The following alerts:
AIR PACK 1(2) REGUL FAULT AIR COND CTL 1(2)-A FAULT AIR COND CTL 1(2)-B FAULTassociated with the operative pack are not displayedon the EWD, and
3) The affected PACK 1(2) pb-sw is set to OFF, and
4) The associated pack flow control valve is secured inthe closed position.
OPERATING PROCEDURES
Refer to Item 21-52-01D
MAINTENANCE PROCEDURE
Refer to AMM 21-51-00-040-002
I T E M
01 MAY 12MEL
A320/321MEL/CDL 01.21.45
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-52 Air Cooling System
21-52-01 Air Conditioning
Pack
21-52-01G Air cycle
machine failed
C 2 1 (O)(FD) One may be operated on heat exchanger cooling only (air
cycle machine failure) provided that:
1) The following alerts:
AIR COND CTL 1(2)-A FAULT
AIR COND CTL 1(2)-B FAULTassociated with the operative pack are not displayedon the EWD, and
2) The affected pack outlet temperature indication isoperative on the BLEED SD page.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
PACK 1(2) pb-sw in "heat exchanger
cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
IN FLIGHT
· When the TAT is equal to or less than 12° C:
PACK 1(2) pb-sw in "heat exchanger
cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
· If the non affected air conditioning pack fails:
Maximum flight altitude . . . . . . . . . . . . . . . . . . . . .31,500 ft
(Cont’d on next page)
I T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.21.46
AIR CONDITIONING
A320/321MEL/CDL
01 MAY 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-52 Air Cooling
System
21-52-01 Air Conditioning
Pack (cont’d)
21-52-01G Air cycle
machine failed
(cont’d) OPERATING PROCEDURES (Cont’d)
DURING DESCENT
· If the TAT is above 12° C:
PACK 1(2) pb-sw in "heat exchanger
cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
AT THE END OF THE DESCENT, BEFORE LANDING
PACK 1(2) pb-sw in "heat exchanger cooling
only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
21-52-01H Non
pressurizedflight
C 2 0 Both may be inoperative provided that the flight is not
pressurized.
Refer to FCOM/PRO-SPO-20 Fligt Without Cabin
Pressurized.
Refer to FOPM CH 8 Maintenance Ferry Flights
21-52-02 Air Conditioning
Pack Ram Air Inlet
Flap
21-52-02A Flap
deactivated
C 2 0 (M) One or both may be inoperative provided that the affected
flap is deactivated in the open position.
MAINTENANCE PROCEDURE
Refer to AMM 21-61-00-040-002
21-52-02B Only one
inoperative
C 2 1 One may be inoperative in the closed position provided
that the associated air conditioning pack is considered
inoperative.
Refer to Item 21-52-01 Air Conditioning Pack
I T E M
01 MAY 12MEL
A320/321MEL/CDL 01.21.47
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONING
21-52 Air Cooling System
21-52-02 Air Conditioning
Pack Ram Air Inlet
Flap
21-52-02C Non
pressurized
flight
C 2 0 Both may be inoperative in the closed position provided
that the flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Fligt Without CabinPressurized.
Refer to FOPM CH 8 Maintenance Ferry Flights
21-55 Emergency Ram Air
Inlet
21-55-01 Emergency Ram
Air Inlet
21-55-01A Ram air inlet
deactivated
C 1 0 (M) May be inoperative provided:
1) The emergency ram air inlet is deactivated in theclosed position, and
2) Both air conditioning packs are checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 21-55-00-040-002
21-55-01B Non
pressurized
flight
C 1 0 May be inoperative in the open position provided that:
1) Extended overwater flight is not conducted, and
2) The flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Fligt Without Cabin
Pressurized.
Refer to FOPM CH 8 Maintenance Ferry Flights
I T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.21.48
AIR CONDITIONING
A320/321MEL/CDL
01 MAY 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONIN
21-61 Pack Temperature
Control
21-61-01 Pack Turbine
Bypass Valve
21-61-01A C 2 1 One may be inoperative.
21-63 Cockpit and Cabin
Temperature
Control
21-63-02 Cockpit and Cabin
Trim Air Valve
21-63-02A Affected valve
checked closed
C 3 0 (O) One or more may be inoperative provided that the
affected valve is checked closed on the COND SD page.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
On the COND SD page page, check that the affected trim
air valve is closed amber.
IN FLIGHT
· If the affected zone temperature becomes
uncomfortable:
HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
21-63-02B Hot air pressure
valve checked
operative
C 3 0 (O) One or more may be inoperative provided that the hot air
pressure regulating valve is checked operative on the
COND SD page.
(Cont’d on next page)
I T E M
01 MAY 12MEL
A320/321MEL/CDL 01.21.49
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONIN
21-63 Cockpit and Cabin
Temperature Control
21-63-02 Cockpit and Cabin
Trim Air Valve
21-63-02B Hot air pressure
valve checked
operative
(cont’d)
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- HOT AIR pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OFFthen on
- On the COND SD page, check that the hot air pressure
regulating valve follows the HOT AIR pb-sw command.
IN FLIGHT
· If affected zone temperature becomes
uncomfortable:
HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
21-63-02E Hot air pressurevalve
considered
inoperative
C 3 0 One or more may be inoperative provided that the hot air pressure regulating valve is considered inoperative.
Refer to Item 21-63-03 Hot Air Pressure Regulating Valve
21-63-03 Hot Air Pressure
Regulating Valve
21-63-03A Hot air pressure
valve checked
closed
C 1 0 (O) May be inoperative in the closed position provided that:
1) HOT AIR pb-sw is set to OFF, and
2) Hot Air Pressure Regulating Valve is checked closedon the COND SD page.
(Cont’d on next page)
I T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.21.50
AIR CONDITIONING
A320/321MEL/CDL
01 MAY 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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21 AIR CONDITIONIN
21-63 Cockpit and Cabin
Temperature
Control
21-63-03 Hot Air Pressure
Regulating Valve
21-63-03A Hot air pressure
valve checked
closed (cont’d)
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- On the COND SD page page, check that the hot air
pressure regulating valve is closed amber.
21-63-03B All trim valve
checked closed
C 1 0 (O) May be inoperative in the open position provided that:
1) HOT AIR pb-sw is set to OFF, and
2) All Trim Air Valves are checked closed on the CONDSD page.
OPERATING PROCEDURES
GENERAL INFORMATION
On the COND SD page, the hot air pressure regulating
valve is displayed amber open.
DURING COCKPIT PREPARATION
- HOT AIR pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- On the COND SD page, check that all the trim air valves
are closed amber.
21-63-03C Hot air pressure
valve secured
closed
C 1 0 (O)(M) May be inoperative provided that the hot air pressure
regulating valve is secured in the closed position.
(Cont’d on next page)
01 MAY 12MEL
A320/321MEL/CDL 01.21.51
AIR CONDITIONING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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21 AIR CONDITIONING
21-63 Cockpit and Cabin
Temperature Control
21-63-03 Hot Air Pressure
Regulating Valve
21-63-03C Hot air pressure
valve secured
closed (cont’d) OPERATING PROCEDURES
GENERAL INFORMATION
On the COND SD page, the hot air pressure regulating
valve is displayed closed amber.
MAINTENANCE PROCEDURE
Refer to AMM 21-63-00-040-002
21-63-04 Air Conditioning
System Controller
Channel (COND
CTL 1(2)-A(B))
21-63-04A C 4 2 One may be inoperative on each side.
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.21.52
AIR CONDITIONING
A320/321MEL/CDL
01 MAY 12MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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22 AUTO FLIGHT
22-01 FLT CTL
Overhead Panel
22-01-01 FAC pb-sw
FAULT light
22-01-01A C 2 1 One may be inoperative.
22-01-02 FAC pb-sw OFF
light
22-01-02A C 2 0 One or both may be inoperative.
22-05 FMA Indications
on the PFD
22-05-01 AP Related
Indications on
the FMA
22-05-01A B 2 1 One or more indications may be inoperative on one
FMA.
22-05-01B B 2 0 (O) One or more indications may be inoperative on both
FMAs provided that that AP is not used.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
RVSM operations are not permitted.
Maximum landing capability is CAT I.
22-05-02 A/THR Related
Indications on
the FMA
22-05-02A B 2 1 One or more indications may be inoperative on one
FMA.
22-05-02B B 2 0 One or more indications may be inoperative on both
FMAs provided that the autothrust (A/THR) is considered
inoperative.
Refer to Item 22-30-01 Autothrust (A/THR)
12 FEB 12MEL
A320/321MEL/CDL 01.22.01
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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22 AUTO FLIGHT
22-05 FMA Indications on
the PFD
22-05-03 Approach and
Landing
Capabilities on
the FMA
22-05-03A C 2 0 (O) One or more may be inoperative on one or both FMAs.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I.
22-05-04 Special
Messages on the
FMA
22-05-04A B 2 1 “MAN PITCH TRIM ONLY” is required on one side.
22-10 Autopilot/Flight
Director (AP/FD)
22-10-01 Autopilot (AP)
22-10-01A B 2 1 (O) One may be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
- When one AP is inoperative:
Landing capability is CAT II.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.22.02
AUTO FLIGHT
A320/321MEL/CDL 01 MAY 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-10 Autopilot/Flight
Director (AP/FD)
22-10-01 Autopilot
(AP)(Cont’d)
22-10-01B A 2 0 (O)(FD) Both may be inoperative provided:
1) Current weather enroute does not indicatethrunderstorm, activites, and approach minimums
are limited to CAT I or higher,2) Aircraft is not dispatched into RVSM airspace,
3) For international flight Aircraft is released for one legfly ( 2 ½ hours maximum) to a maintenance stationfor repair,
4) For domestic flight Aircraft is released for two leg fly( 2 hours total ) to a maintenance station for repair,
OPERATING PROCEDURES
- When both APs are inoperative:
RVSM operations are not permitted.Maximum landing capability is CAT I.
22-10-02 Flight Director
(FD)
22-10-02A B 2 1 (O)(FD) One may be inoperative.
OPERATING PROCEDURES
FOR TAKEOFF
- For a takeoff without one FD:
Refer to FCOM /PRO No Flight Director Takeoff
22-10-03 Take-over pbPriority Function
22-10-03A 2 2 Both must be operative.
12 FEB 12MEL
A320/321MEL/CDL 01.22.03
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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22 AUTO FLIGHT
22-10 Autopilot/Flight
Director (AP/FD)
22-10-04 Take-over pb AP
Disconnection
Function
22-10-04A B 2 1 (O)(FD) One may be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I.
BEFORE ENGINE START
- AP 1 · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Operative take-over pb · · · · · · · · · · · · · · · · · · · · Press
- Check that the red AP OFF message is displayed onthe EWD.
- AP 2 · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Operative take-over pb · · · · · · · · · · · · · · · · · · · · Press
- Check that the red AP OFF message is displayed onthe EWD.
BEFORE APPROACH
- If the AP is used for approach:
The operative AP disconnect pb must be assigned tothe PF.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.04
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
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22 AUTO FLIGHT
22-10 Autopilot/Flight
Director (AP/FD)
22-10-05 AUTO LAND
lights
22-10-05A C 2 0 (O)(FD) One or both may be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
- If Captain side or both lights are inoperative:
Maximum landing capability is CAT I.
22-10-06 AP
Disengagement
Warning
22-10-06A C 1 0 (O)(FD) May be inoperative provided that the AP is not engaged.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
RVSM operations are not permitted.
Maximum landing capability is CAT I.
22-10-07 Sticks and
Rudder Pedals
Locking
Solenoid in AP
Mode
22-10-07A C 3 1 (O)(FD) One or two may be inoperative unlocked provided that
no autoland is performed.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I.
01 MAY 12MEL
A320/321MEL/CDL 01.22.05
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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22 AUTO FLIGHT
22-30 Autothrust
22-30-01 Autothrust
(A/THR)
22-30-01A B 1 0 (O)(FD) May be inoperative provided that the autothrust (A/THR)
is disconnected before each flight.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum Landing capability is CAT I.
AFTER ENGINE START
- Press and hold either autothrust instinctive disconnectpb for at least 15 seconds.
- The A/THR system is permanently disconnected for the entire flight.
Check that A/THR INOP SYS is displayed on theSTATUS SD page.
- All A/THR functions including ALPHA FLOORprotection are lost.
22-30-02 Autothrust
Instinctive
Disconnect pb
22-30-02A C 2 1 (O) One may be inoperative provided that the ability to
disconnect the autothrust (A/THR) via the remaining
Instinctive Disconnect pb and by the FCU A/THR pb is
checked before each flight.
OPERATING PROCEDURES
The purpose of the procedure is to check the A/THRdisconnection via the remaining Instinctive Disconnect
pb and via the A/THR pb on the FCU.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.06
AUTO FLIGHT
A320/321MEL/CDL 01 MAY 12
MEL
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22 AUTO FLIGHT
22-30 Autothrust
22-30-02 Autothrust
Instinctive
Disconnect pb
22-30-02A (Cont’d) OPERATING PROCEDURES(Cont’d)
AFTER IRS ALIGNMENT
Note:
Disregard alerts during the test. Use the
EMER CANCEL pb on the ECAM
control panel as necessary.
Aircraft configuration for the check via the FMS 1:
- ENG/FADEC GND PWR 1 and 2· · · · · · · · · · · · · ON
- Both thrust levers· · · · · · · · · · · · · · · · · · · · · · · · MCT
- FD· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Off
- AUTO FLT/FMGC/2 (121 VU M17) C/B · · · · · · · Pull
- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Check that green SPEED and white A/THRindications appear on the PFD.
- Check that A/THR pb light bars are ON.
Check of the A/THR disconnection via the remaining
Instinctive Disconnect pb:
- A/THR instinctive disconnect pb (non affectedautothrust) · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push
- Check that the A/THR pb light bars are OFF.
- Check that green SPEED and white A/THR
indications are no more displayed on the PFD.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.22.07
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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22 AUTO FLIGHT
22-30 Autothrust
22-30-02 Autothrust
Instinctive
Disconnect pb
22-30-02A (Cont’d) OPERATING PROCEDURES(Cont’d)
- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Check that the A/THR pb light bars are ON.
- Check that green SPEED and white A/THR indicationsare displayed on the PFD.
Check of the A/THR disconnection via the A/THR pb on
the FCU:
- A/THR pb (on the FCU) · · · · · · · · · · · · · · · · · · · · · · Off
- Check that the A/THR pb light bars are OFF.
- Check that green SPEED and white A/THR indicationsare no more displayed on the PFD.
- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
Aircraft configuration for the check via the FMS 2:
- AUTO FLT/FMGC/2 (121VU M17) C/B · · · · · · · · Push
- AUTO FLT/FMGC/1 (49VU B02) C/B · · · · · · · · · · · Pull
- Wait 2 min.
Check of the A/THR disconnection via the remaining
Instinctive Disconnect pb:
- A/THR instinctive disconnect pb (non affectedautothrust)· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push
- Check that the A/THR pb light bars are OFF.
- Check that green SPEED and white A/THR indicationsare no more displayed on the PFD.
- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Check that the A/THR pb light bars are ON.
- Check that green SPEED and white A/THR indicationsare displayed on the PFD.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.08
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
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22 AUTO FLIGHT
22-30 Autothrust
22-30-02 Autothrust
Instinctive
Disconnect pb
22-30-02A (Cont’d) OPERATING PROCEDURES(Cont’d)
Check of the A/THR disconnection via the A/THR pb on
the FCU:
- A/THR pb (on the FCU) · · · · · · · · · · · · · · · · · · · · Off
- Check that the A/THR pb light bars are OFF.
- Check that green SPEED and white A/THRindications are no more displayed on the PFD.
- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
Restore normal aircraft configuration:
- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Off
- AUTO FLT/FMGC/1 (49VU B02) C/B · · · · · · · · Push
- ENG/FADEC GND PWR 1 and 2 · · · · · · · · · · · · · Off
- Both thrust levers· · · · · · · · · · · · · · · · · · · · · · · · IDLE
- RCL pb (on the ECAM control panel) · · · · · · · · Push
- Wait 2 min before using the MCDU and the FD.
22-30-03 Autothrust
Disengagement
Warning
22-30-03A B 1 0 May be inoperative provided that the autothrust (A/THR)
is considered inoperative.
Refer to Item 22-30-01 Autothrust (A/THR)
12 FEB 12MEL
A320/321MEL/CDL 01.22.09
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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22 AUTO FLIGHT
22-60 Flight Augmentation
(FAC)
22-60-01 FAC 1
22-60-01A 1 1 (M) Must be operative.
Note:
The AUTO FLT FAC 1 FAULT alert may
be displayed with the associated AUTOFLT/FAC1/28VDC C/B tripped.
This may be due to a short circuit within
either rudder trim actuator channel 1 or
rudder travel actuator channel 1.
In this case, the FAC 1 may be
recovered provided that the affected
part of the faulty actuator is deactivated
using the associated maintenance
procedure.
Refer to AMM 27-22-00-040-001, or
Refer to AMM 27-23-00-040-01.
Refer to Item 27-22-01 Rudder Trim
System, or
Refer to Item 27-23-01 Rudder Travel
Limiter System (Including Rudder and
Pedals Travel Limiter Units)
MAINTENANCE PROCEDURE
Refer to AMM task.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.10
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
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22 AUTO FLIGHT
22-60 Flight
Augmentation
(FAC)
22-60-02 FAC 2
22-60-02A C 1 0 (O)(FD) May be inoperative provided that:
1) All ADIRSs, ELACs, SECs, SFCCs, LGCIUs andRAs are operative, and
2) The Rudder Travel Limiter System 2 is consideredinoperative.
Refer to item 22-60-04 Yaw Damper System, and
Refer to item 27-22-01 Rudder Trim System, and
Refer to Item 27-23-01 Rudder Travel Limiter System
(Including Rudder and Pedals Travel Limiter Units)
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
ON GROUND
- If the AUTO FLT FAC 2 FAULT alert is displayedon the EWD
Or
- If erroneous speeds are displayed:
- AUTO FLT/FAC 2/28VDC (121VU M19) C/B
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
- FAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . OFF
12 FEB 12MEL
A320/321MEL/CDL 01.22.11
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-60 Flight Augmentation
(FAC)
22-60-03 Windshear
Detection
System
Predictive
22-60-03A C 1 0 (O) May be inoperative provided:
1)Alternate procedures are established and used,and
2)GPWS windshear alert mode (Mode 7) is operative.
OPERATING PROCEDURES
Flight Crewmember must refer to the winshear section,
in the FCOM . prior to their first departure of the day.
22-60-03B A 1 0 (O)(FD) May be inoperativeprovided:
1)alternate procedures are estalished and used
2)Takeoff and landings are not condcuted in known or forecast windshear conditions, and
3)Repairs are made within three flight days.
OPERATING PROCEDURES
Flight Crewmember must refer to the winshear section,
in the FCOM prior to their first departure of the day.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.12
AUTO FLIGHT
A320/321MEL/CDL 01 MAY 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-60 Flight
Augmentation
(FAC)
22-60-04 Yaw Damper
System
22-60-04A C 2 1 (O)(M)
(FD)
One may be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
MAINTENANCE PROCEDURE
Refer to AMM 27-26-00-040-001
22-70 Flight
Management
System (FMS)
22-70-01 Flight
Management
System (FMS)
22-70-01A FMS 1
inoperative with
IR 1 (NAV
mode) or GPS
1 operative
C 2 1 (O) The FMS 1 may be inoperative provided that:
1) Two MCDUs are operative, and
2) The IR 1 NAV mode or GPS 1 is operative.
OPERATING PROCEDURES
IN FLIGHT
- In the case of FMS 1+2 failure:
MCDU NAV B/UP · · · · · · · · · · · · · · · · · · · · · · · · UseRefer to FCOM/DSC-22-20-60-130 (MCDU BACKUP NAVIGATION).
12 FEB 12MEL
A320/321MEL/CDL 01.22.13
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-70 Flight Management
System (FMS)
22-70-01B FMS 2
inoperative
with IR 1
(NAV mode)
or GPS 1
operative
C 2 1 (O) The FMS 2 may be inoperative provided that the IR 1
NAV mode or GPS 1is operative.
OPERATING PROCEDURES
Refer to MEL 22-70-01A
22-70-01C FMS 1
inoperative
C 2 1 The FMS1 may be inoperative provided that the flight
remains within radio navaids coverage.
22-70-02 NavigationDatabase
22-70-02A C 2 0 (O)(FD) May be out of currency provided:
1)Current Aeronautical Charts are used to verifyNavigation Fixes before dispatch, and
2)Procedures are established and used to verify statusand suitability of Navigation Facilties used to defineroute of flight.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.14
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-70 Flight
Management
System (FMS)
22-70-02 Navigation
Database
22-70-02A (cont’d) OPERATING PROCEDURES
1. Both, pilots and dispatch must check the flight plan
route against current aerounautical cfhart(s) andNOTAMs for suitability and serviceability of NAVFixes.
2. Pilot must ensure that all applicable charts for enroute to destination and alternate(s) are availableon board.
3. All required terminal and approach plates areavailable on board, and
4. Cross check FMGS waypoints using current flighcrew navigation charts.
22-70-03 Performance
Information
22-70-03A C 2 0 One or both may be inoperative.
22-70-04 Fuel/Time
Prediction
22-70-04A C 2 0 One or both may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.22.15
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-81 Flight Control Unit
(FCU)
22-81-01 Auto Flight
Control Panel
(FCU)
22-81-01-01 AP Engagement
pb
22-81-01-01A B 2 1 One may be inoperative provided that the associated
autopilot (AP) is considered inoperative.
Refer to Item 22-10-01A Autopilot (AP)
22-81-01-01B A 2 0 Both may be inoperative provided that both autopilots
(AP) is considered inoperative.
Refer to Item 22-10-01B Autopilot (AP)
22-81-01-02 A/THR Arming
pb
22-81-01-02A B 1 0 May be inoperative provided that the autothrust (A/THR)is considered inoperative.
Refer to Item 22-30-01 Autothrust (A/THR)
22-81-01-03 Mode
Engagement pb
(LOC, EXPED,
APPR)
22-81-01-03A B 3 0 One or more may be inoperative.
22-81-01-04 Selection knob
(ALT, HDG-TRK,SPD-MACH)
22-81-01-04A 3 3 Must be operative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.16
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-81 Flight Control Unit
(FCU)
22-81-01 Auto Flight
Control Panel
(FCU)
22-81-01-05 V/S-FPA
Selection knob
22-81-01-05A B 1 0 May be inoperative provided that operations do not
required its use.
22-81-01-06 HDG-V/S/TRK-
FPA Change
Over pb
22-81-01-06A B 1 0 May be inoperative provided that the HDG-V/S selection
is operative.
22-81-01-07 SPD/MACH
Change Over pb
22-81-01-07A C 1 0 May be inoperative provided that the SPD selection is
operative.
22-81-01-08 METRIC ALT pb
22-81-01-08A C 1 0 May be inoperative.
22-81-01-09 Selection
Window (SPD-
MACH, HDG-
TRK, ALT, V/S-
FPA)
22-81-01-09B C 4 0 One or more may be inoperative provided that the
associated indications are operative on both PFDs and
both Nds.
12 FEB 12MEL
A320/321MEL/CDL 01.22.17
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-81 Flight Control Unit
(FCU)
22-81-02 EFIS Control
Panel (FCU)
22-81-01-10 AP1, AP2 and
A/THR pb light
Bars
22-81-01-10A C 3 0 One or more may be inoperative provided that the
associated indication is operative on both PFDs.
22-81-01-11 Mode
Engagement
(LOC, EXPED,
APPR) pb light
Bars
22-81-01-11A C 3 0 One or more may be inoperative.
22-81-02-01 Baro Reference
Display Window
22-81-02-01A C 2 1 One may be inoperative.
22-81-02-02 Baro Reference
selector Outer
Ring (in Hg/hPa)
22-81-02-02A C 2 1 One may be inoperative provided that the unit required
for the intended flight is operative on both EFIS control
panels.
22-81-02-03 Baro Reference
selector Inner knob
22-81-02-03A 2 2 Both must be operative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.18
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-81 Flight Control Unit
(FCU)
22-81-02 EFIS Control
Panel (FCU)
22-81-02-04 FD pb
22-81-02-04A B 2 1 One may be inoperative provided that the associated FD
is considered inoperative.
Refer to Item 22-10-02 Flight Director (FD)
22-81-02-05 LS pb
22-81-02-05A C 2 1 One may be inoperative provided that the associated ILS
is considered inoperative.
Refer to Item 34-30-04 Instrument Landing System (ILS)
22-81-02-06 Optional Data
(ARPT, NDB,
VOR.D, WPT,
CSTR) Displaypb
22-81-02-06A C 10 0 One or more may be inoperative.
22-81-02-07 ND Range
selector
22-81-02-07A B 2 1 One may be inoperative provided that the ND unit
associated with the operative ND range selector is
operative.
22-81-02-08 ND Mode
selector
22-81-02-08A B 2 1 One may be inoperative provided that the ND unit
associated with the operative ND mode selector is
operative.
12 FEB 12MEL
A320/321MEL/CDL 01.22.19
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-81 Flight Control Unit
(FCU)
22-81-02 EFIS Control
Panel (FCU)
22-81-02-09 ADF/VOR sw
22-81-02-09A C 4 0 One or more may be inoperative provided that the
associated ADF/VOR indication on ND is consideredinoperative.
Refer to Item 34-50-03A ( ADF )
Refer to Item 34-50-05A ( VOR )
Refer to Item 34-06-06 Radio Navaids Indications on the
ND
22-81-02-10 LS and FD pb
light Bars
22-81-02-10A C 4 2 One per each side may be inoperative provided that the
associated indication is displayed on both PFDs.
22-81-02-11 Optional Data
(ARPT, NDB,
VOR.D, WPT,
CSTR) Display
pb light Bars
22-81-02-11A C 10 0 One or more may be inoperative.
22-81-03 FCU Channel
22-81-03-01 FCU Channel
22-81-03-01A C 2 1 One channel may be inoperative provided that Two
RMPs, all DUs, both RAs, both LGCIUs, both FACs,
both Automatic Cabin Pressure Control Systems, all
ADIRUs and the ISIS Baro-altimeter function are
operative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.20
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
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22 AUTO FLIGHT
22-82 Multipurpose
Control and
Display Unit
(MCDU)
22-82-01 MCDU 1
22-82-01B B 1 0 May be inoperative provided that:
1) The MCDU 2 is operative, and
2) The flight remains within radio navaids coverage.
22-82-02 MCDU 2
22-82-02B Flight within
navaids
coverage
B 1 0 May be inoperative provided that the flight remains
within radio navaids coverage.
22-82-04 MCDUAnnunciator
light
22-82-04A C 8 0 One or more may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.22.21
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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22 AUTO FLIGHT
22-83 Flight Management
and Guidance
Computer (FMGC)
22-83-01 Flight
Management
and Guidance
Computer
(FMGC)
22-83-01A FMGC 1
inoperative
A 2 1 (O) One may be inoperative for three flight days provided
that:
1)FMGC 1 is deactivated,
2) FMS 1 is considered inoperative,
Refer to Item 22-70-01 Flight Management System(FMS), and
3)The terrain function of TAWS is consideredinoperative.
Refer to Item 34-40-01 Ground Proximity Warning
System (GPWS)/Terrain Awareness and Warning
System (TAWS)
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING COCKPIT PREPARATION
- If FMGC 1 is affected:
AUTO FLT/FMGC/1 (49VU B02 or 121VU M16) C/B· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
- If ADS-B is required for the intended flight:
ATC selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
- If FMGC 2 is affected:
AUTO FLT/FMGC/2 (121VU M17) C/B· · · · · · · · · · Pull
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.22
AUTO FLIGHT
A320/321MEL/CDL 12 FEB 12
MEL
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22 AUTO FLIGHT
22-83 Flight
Management and
Guidance
Computer (FMGC)
22-83-01 Flight
Management
and Guidance
Computer
(FMGC)
22-83-01A FMGC 1
inoperative
(Cont’d)
OPERATING PROCEDURES (Cont’d)
Note:
During IR alignment, when the FMGC 2
is deactivated, IRS IN ALIGN memo
cannot be displayed until the FD 1 is
engaged.
- If ADS-B is required for the intended flight: ATC selector · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · 1
22-83-01B FMGC 2
inoperative
C 2 1 (O) FMGC 2 may be inoperative provided that:
1) FMGC 2 is deactivated, and
2) FMS 2 is considered inoperative.
Refer to Item 22-70-01 Flight Management System
(FMS)
OPERATING PROCEDURES
Refer to MEL 22-83-01A for operating procedure.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.22.23
AUTO FLIGHT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.22.24
AUTO FLIGHT
A320/321MEL/CDL
MEL
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23 COMMUNICATIONS
23-00 MAINTENANCE
Message on the
STATUS SD page
23-00-01 CIDS 1(2)
MAINTENANCE
Message
23-00-01A C 1 - CIDS 1(2) MAINTENANCE message may be displayed on
the STATUS SD page.
23-01 Overhead Panels
23-01-01 RCDR Overhead
Panel
22-01-01-01 RCDR GND CTL
pb-sw ON light
23-01-01-01A C 1 0 May be inoperative.
22-01-01-31 RCDR GND CTL
pb-sw
22-01-01-31A AUTO Position C 1 0 (O) May be inoperative in the AUTO position.
OPERATING PROCEDURES
ON GROUND
CVR can only be tested through the CVR test pb-sw
during the first 5 minutes after supply of the aircraft
electrical network.
22-01-01-31B ON Position C 1 0 (O) May be inoperative in the ON position.
OPERATING PROCEDURES
AFTER LANDING
- To stop CVR recording, if needed:
COM/CVR/SPLY (49 VU E14) C/B · · · · · · · · · · · PULL
22-01-01-31C CVR
Considered
Inoperative
A 1 0 May be inoperative provided that the CVR is considered
inoperative.
Refer to Item 23-71-01 Cockpit Voice Recorder (CVR)
12 FEB 12MEL
A320/321MEL/CDL 01.23.01
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-01 Overhead Panels
23-01-01 RCDR Overhead
Panel
23-01-01-32 CVR ERASE pb
23-01-01-32A C 1 0 May be inoperative.
23-01-01-33 CVR TEST pb
23-01-01-33A A 1 0 May be inoperative provided that the Cockpit Voice
Recorder (CVR) is considered inoperative.
Refer to Item 23-71-01 Cockpit Voice Recorder (CVR)
23-01-02 CALLS Overhead
Panel
23-01-02-31 CALLS ALL pb
23-01-02-31A C 1 0 May be inoperative.
23-01-02-32 CALLS EMER pb
CALLS FWD pb,
CALLS MID pb,
CALLS EXIT pb,
CALLS AFT pb
23-01-02-32A Use of
Passenger
address system
C 1 0 (O) May be inoperative provided that the passenger address
system is used for communication between the cockpit
and the cabin.
OPERATING PROCEDURES
PIC will brief cabin crew that he will use passenger
address system for communications.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.02COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
MEL
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23 COMMUNICATIONS
23-01 Overhead Panels
23-01-02 CALLS
Overhead Panel
23-01-02-32 CALLS EMER pb
CALLS FWD pb,
CALLS MID pb,
CALLS EXIT pb,
CALLS AFT pb
23-01-02-32B Use of Cockpit
handset
interphone
C 1 0 (O) May be inoperative provided that the cockpit handset
interphone is used for communication between the cockpit
and the cabin.
OPERATING PROCEDURES
PIC will brief cabin crew that he will use cockpit handset
interphone for communications.
12 FEB 12MEL
A320/321MEL/CDL 01.23.03
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-09 ECAM Alerts
23-09-01 COM HF 1(2)
EMITTING Alert
23-09-01A Refer to Item 23-10-01 HF System
23-09-02 COM VHF 1(2)(3)
EMITTING Alert
23-09-02A C 3 2 (O) One may be displayed provided that :
1) The alert is confirmed to be false by troubleshooting,and
2) The affected VHF is deactivated and consideredinoperative.
Refer to Item 23-10-02 VHF System
OPERATING PROCEDURES
GENERAL INFORMATION
To make troubleshooting easier, Refer to FCOM/PRO- ABN-23 COM VHF 1(2)(3)/HF 1(2) EMITTING.
DURING COCKPIT PREPARATION
· To deactivate the VHF1 system, apply:
COM/VHF/1 (49 VU G09) C/B . . . . . . . . . . . . . . . . PULL
· To deactivate the VHF2 system, apply:
COM NAV/VHF/2 (121 VU L04) C/B . . . . . . . . . . . PULL
· To deactivate the VHF3 system, apply:
COM NAV/VHF/3 (121 VU L05) C/B . . . . . . . . . . . PULL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.04COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
MEL
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23 COMMUNICATIONS
23-10 Speech
Communication
23-10-01 HF System
23-10-01A 1 1 (FD) Must be operative on routes that require HF
communication with ATSU, provided SATCOM Voice
Mode is available for use by that unit.
C 1 0 (FD) May be inoperative provided SATCOM Voice Mode isoperative.
23-10-02 VHF System
23-10-02B C 3 2 VHF 2 or VHF 3 may be inoperative.
Note:
The VHF 3 may be used as one of the
VHFs required by regulations, provided
that the VHF 3 is set to VOICE mode
before each flight.
23-10-03 SATCOM Voice
Mode
23-10-03A 1 1 (FD) Must be operative on routes that require HF
communication with ATSU.
C 1 0 (FD) May be inoperative provided HF System and SELCAL
Function are operative.
23-13 Radio Management
23-13-01 RadioManagement
Panel (RMP)
23-13-01B C 3 2 RMP 2 may be inoperative.
01 MAY 12MEL
A320/321MEL/CDL 01.23.05
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-13 Radio Management
23-13-02 RMP Selection Key
23-13-02A C 3 2 One may be inoperative on each RMP provided that :
1) VHF 1 selection key is operative on RMP 1, and
2) If HF is required, HF 1 selection key is operative onRMP 1.
23-20 Data Transmissionand Automatic Calling
23-20-01 Aircraft
Communications
Addressing
Reporting System
(ACARS)
23-20-01A B 1 0 (O)(FD) May be inoperative provided altenate procedures are
used.
OPERATING PROCEDURES
1. Flight crew must transmit depature, enroute, and thearrival reports in accordance with the route manualcommunication requirement.
2. Flight crew must complete the in-flight cruiseperformance data records if required.
NOTE:
Any portion of the system that is
operative may be used.
23-20-02 SATCOM Data
Mode
23-20-02A B 1 0 May be inoperativeprovided operation or procedures do
not requier its use.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.06COMMUNICATIONS
A320/321MEL/CDL 01 MAY 12
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23 COMMUNICATIONS
23-31 Passenger Address
System
23-31-01 Passenger
Address System
23-31-01A 1 1 Must be operative.
Note:
i. In the case of partial failure of thepassenger address system, refer to
the item(s) of the affected system(s).
ii. Total failure of the passenger
address system (indicated by the
COM CIDS 1+2 FAULT alert
displayed on the EWD) is not
permitted.
23-40 Interphone
23-40-01 Ground External
Horn
23-40-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
ON GROUND
- When the aircraft electrical network is supplied:
Monitor the avionics equipment ventilation in thecockpit.
BEFORE LEAVING THE AIRCRAFT
Set the three ADIRS Mode selectors to OFF.
23-40-02 Flight Crew
Interphone
System
23-40-02A 1 1 Must be operative for each person on cockpit duty.
12 FEB 12MEL
A320/321MEL/CDL 01.23.07
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-40 Interphone
23-40-03 Flight Crew to
Ground
Communication
System
23-40-03A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
Instruct ground crew to connect to flight interphone jack
and establish communications through flight interphone.
23-40-04 Service Interphone
Jack
23-40-04A C 8 0 (O) One or more may be inoperative.
OPERATING PROCEDURES
Instruct ground crew to connect to flight interphone jack
and establish communications through flight interphone.
23-51 Audio Management
23-51-01 SELCAL Function
23-51-01A 1 1 (FD) Must be operative for dispatch from Kingdom on routes
that require HF communication with ATSU and SATCOM
Voice Mode must be operative.
C 1 0 (FD) May be inoperative for dispatch back to Kingdom on
routes that require HF communication with ATSU
provided:
1) Crew continuously monitors HF communication, and
2) SATCOM Voice Mode is operative.
C 1 0 (FD) May be inoperative provided SATCOM Voice Mode is
operative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.08COMMUNICATIONS
A320/321MEL/CDL 01 MAY 12
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23 COMMUNICATIONS
23-51 Audio Management
23-51-02 Boomset
23-51-02A A 2 0 May be inoperative provided:
1) Flight data recorder and hand mic are operative, and
2) Repaire are made within three flight days.
23-51-03 Hand
Microphone
23-51-03A C 2 1 One may be inoperative provided both associated boom
micrphones are operative.
23-51-04 Cockpit
Loudspeaker
23-51-04A C 2 1 Only F/O loudspeaker may be inoperative provided that at
least one crewmember on cockpit duty wears a boomset
compatible with the quick donning oxygen mask.
23-51-05 CockpitLoudspeaker
Volume Control
23-51-05A C 2 1 (O) Only F/O side may be inoperative provided that the
affected crewmember on cockpit duty wears a boomset
compatible with the quick donning oxygen mask.
OPERATING PROCEDURES
Cockpit crew will be aware and prepared for monitoring
communications during the flight.
12 FEB 12MEL
A320/321MEL/CDL 01.23.09
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-51-06 Sidestick PTT sw
23-51-06B C 2 1 (M) Only F/O side may be inoperative in the open position (non
transmitting position) provided that the INT/RAD sw on
CAPT ACP, on F/O ACP and on ACP 3 are operative.
Note:
Apply the maintenance procedure only
when the operative sidestick radio
selector is failed in the closed position(transmitting position).
MAINTENANCE PROCEDURE
Refer to AMM 23-51-00-040-001
23-52 Audio Control Panel
(ACP)
23-52-01 CAPT and F/O
ACP
23-52-01A C 2 1 (O) One may be inoperative provided that :1) ACP 3 is operative, and
2) The AUDIO SWITCHING selector is operative.
OPERATING PROCEDURES
In order to recover audio channel on the affected side :
AUDIO SWITCHING.................................CAPT 3 (F/O 3)
23-52-02 ACP 3
23-52-02A C 1 0 May be inoperative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.10COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
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23 COMMUNICATIONS
23-52 Audio Control Panel
(ACP)
23-52-03 Fourth Occupant
ACP
23-52-03A C 1 0 May be inoperative.
23-52-04 ACP in the
Avionics
Compartment
23-52-04A D 1 0 May be inoperative.
23-52-05 ACP
Transmission
Key
23-52-05A C 14 12 One may be inoperative on each ACP provided that :
1) VHF 1 transmission key is operative either on CAPT ACP or on F/O ACP, and
2) If HF is required, HF 1 transmission key is operativeeither on CAPT ACP or on F/O ACP.
23-52-06 ACP Reception
knob
23-52-06A C 16 14 One may be inoperative on each ACP provided that :
1) VHF 1 reception knob is operative either on CAPT ACP or on F/O ACP, and
2) If HF is required, HF 1 reception knob is operativeeither on CAPT ACP or on F/O ACP,and
3) If ILS is required for approach, one ILS reception knob
is operative either on CAPT ACP or on F/O ACP.
23-52-07 ACP Reception
knob light
23-52-07A C 14 0 May be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.23.11
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-53 AUDIO SWITCHING
Panel on the Center
Pedestal
23-53-01 AUDIO
SWITCHING
selector
23-53-01A C 1 0 May be inoperative.
23-71 Cockpit Voice
Recorder (CVR)
23-71-01 Cockpit Voice
Recorder (CVR)
23-71-01A A 1 0 May be inoperative provided:
1) Flight Data Recorder (FDR) is operative, and
2) Repair is made within three flight days.
23-72 Cockpit Door
Surveillance System(CDSS)
23-72-01 Cockpit Door
Surveillance
System (CDSS)
23-72-01A C 1 0 (O)(FD) May be inoperative provided:
1) An alternate means of viewing the area on the cabinside of the flight crew compartment is available andfunctions,
2) Alternate procedures are established and used of ensuring the security of the area outside the fligh crewcompartment door,
3) With the forward camera inoperative, the cabin area infront of the cockpit must be illuminated when the cabinis in darkness, and
4) With the forward camera inoperative, an additionalcrew member must be assigned for duty in the cockpit.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.12COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
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23 COMMUNICATIONS
23-72 Cockpit Door
Surveillance System
(CDSS)
23-72-01 Cockpit Door
Surveillance
System (CDSS)
23-72-01A (Cont’d) OPERATING PROCEDURES
1. When the forward camera which provides a view of thearea directly in front of the cockpit is inoperative(camera 1), an additional crew member must beassigned for duty in the cockpit.
2. Before the cockpit door is opened, he/she must lookthrough the door viewing lens, identify the personseeking admission and confirm with the PIC TO OPENTHE DOOR.
3. Ensure that the cabin ceiling light of the area in front of the cockpit door is operative and ON when requireed.
4. When any of the cameras 2, 3, inoperataive, another flight attendant must assure that the crew
member/flight crew member required to enter thecockpit is not followed by passenger(s).
Note:
Any portion of the system which is
operative may be used.
12 FEB 12MEL
A320/321MEL/CDL 01.23.13
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-01 Cabin
Intercommunicatio
n Data System
(CIDS)
23-73-01-01Cabin
Intercommunicatio
n Data System
(CIDS) Function
23-73-01-01A 1 1 (M) The CIDS function must be operative.
Note:
i. Failure of a single CIDS director is indicated
by a MAINTENANCE message on the
STATUS SD page.
Refer to Item 23-00-01 CIDS 1(2)
MAINTENANCE Message
ii. In the case of disturbance of the CIDS
function, the deactivation of the affected
CIDS director may recover normal operation
of the CIDS function.
Refer to AMM TASK 23-73-00-040-001
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.14COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
MEL
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-02 DEU A
23-73-02-01 Cabin DEU A
23-73-02-01A C 21 0 (O) One or more may be inoperative and affected passenger
seat may be occupied provided that :
1) The passenger announcement can be heardthroughout the cabin during the flight, and
2) The passenger address system is used to alert thepassengers when "Return to Seat / Fasten Seat Belt /No Smoking" signs are requested.
OPERATING PROCEDURES
GENERAL INFORMATION
On the affected cabin area:
- general cabin illumination is set to full brightness,
- Passenger Call is not available,
- The (No Smoking/Fasten Seat Belt/No PortableElectric Device) Signs are not available.
IN FLIGHT
- When return to seat is requested,
or
When seat belts should be fasten,
or
When smoking is prohibited,
or
When portable electric device use is prohibited,
Use the passenger address system to alert cabinattendants and passengers.
12 FEB 12MEL
A320/321MEL/CDL 01.23.15
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-02 DEU A
23-73-02-01 Cabin DEU A
23-73-02-01B C 21 0 (FD) One or more may be inoperative provided that the affected
seats are blocked and placarded inoperative.
23-73-02-02 Lavatory DEU A
23-73-02-02A C 3 2 (FD) May be inoperative provided that the affected lavatory is
closed and placarded inoperative.
NOTE:
In case foreword lavatory placarded
extra pilot should be assigned to
operate the flight as a safety pilot to
relieve the pilot when leaving the cockpit
for personal reasons.
23-73-03 DEU B
23-73-03-01 Cabin DEU B
23-73-03-01B C 18 0 (O) One or more may be inoperative provided that:
1) One DEU B and the associated handset are operativeat each pair of floor level exit doors, and
2) The slide bottle pressure and door bottle pressureassociated with each affected DEU B are checked onthe associated direct reading pressure gauge beforethe first flight of each day, and
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.16COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-03 DEU B
23-73-03-01 Cabin DEU B
23-73-03-01B (cont’d) 3) The associated lavatory fire extinguisher system ischecked operative, and
4) The absence of smoke in the affected lavatory isperiodically checked.Refer to Item 25-62-06 Passenger Door SlidePressure Message on the PTP/FAP (If Installed), and Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on the PTP/FAP, and Refer to Item 26-17-01 Lavatory Smoke DetectionSystem.
OPERATING PROCEDURES
PIC will brief cabin crew for the use of one cabin handset
per pair of floor level exit doors, if necessary. Define the
cabin handset location to be used by the purser, if
necessary.
12 FEB 12MEL
A320/321MEL/CDL 01.23.17
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-04 Cabin Individual
Call
23-73-04-01 Passenger Call
23-73-04-01A C 42 0 One or more may be inoperative.
23-73-05 Cabin
Loudspeaker
23-73-05-01 Cabin
Loudspeaker
23-73-05-01A C 42 0 (FD) One or more may be inoperative provided that no seat is
occupied from which a passenger cannot hear a
passenger announcement.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.18COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-05 Cabin
Loudspeaker
23-73-05-02 Lavatory
Loudspeaker
23-73-05-02A C 3 0 (O)(FD) One or more may be inoperative provided lavatory is not
used for passengers.
It may used by crew member.
OPERATING PROCEDURES
Flight attendant must be briefed to assure that affected
lavatory is not used by any passenger.
23-73-06 Handset
23-73-06-01 Cockpit Handset
23-73-06-01A C 1 0 May be inoperative provided that the cockpit audio controlpanel (ACP) is used for the communication between the
cockpit and the cabin.
23-73-06-02 Cabin Handset
23-73-06-02A (A320)
(A321)
C
C
3
5
2
4
(O) One may be inoperative provided that one handset is
operative at each pair of floor level exit doors.
OPERATING PROCEDURES
1. The PIC in his briefing must inform all crew members
wich handset(s) is/are inoperative and the affectedflight attendant(s) should use the next availableoperative station or communicat in person when theneed arises.
2. FAIC must be seated in aposition having an operativehandset during Takeoff & Landing.
12 FEB 12MEL
A320/321MEL/CDL 01.23.19
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-06 Handset
23-73-06-03 Cabin Handset
Key
23-73-06-03A Passenger
address and
Cabin to cockpit
interphone
operative
(A320)
(A321)
C
C
3
5
1
3
One or more may be inoperative provided that:
1) Passenger address from the affected handset isoperative, and
2) Cabin to cockpit interphone from affected handset isoperative.
23-73-06-03B Refer to Item 23-73-06-02 Cabin Handset
23-73-07 Prerecorded
Announcement
and Music
Reproducer
(PRAM)
23-73-07-01 Prerecorded
Announcement
and Music
Reproducer
(PRAM)
23-73-07-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
Procedure to replace the perecorded announcement must
be established and necessary demonstation equipment
must be provided onboard.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
01.23.20COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-08 Cabin
Assignment
Module (CAM)
23-73-08-01 Cabin
Assignment
Module (CAM)
23-73-08-01A C 1 0 May be inoperative or missing.
23-73-10 Smoke Detection
Function
23-73-10-01 Smoke Detection
Function (CIDS-
SDF)
23-73-10-01A C 1 0 (FD) May be inoperative provided that:
1) The cargo compartments are empty or do not containflammable or combustible materials, and
2) The lavatory smoke detection system is consideredinoperative.Refer to Item 26-17-01 Lavatory Smoke DetectionSystem
Note:
Failure of a single CIDS-SDF channel is
indicated by a MAINTENANCE
message on the STATUS SD page.
Refer to Item 26-00-01 SDCU/SMOKE
MAINTENANCE Message
12 FEB 12MEL
A320/321MEL/CDL 01.23.21
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-73 Cabin
Intercommunication
Data System
23-73-10 Smoke Detection
Function
23-73-10-01 Smoke Detection
Function (CIDS-
SDF)
23-73-10-01B C 1 0 May be inoperative provided that the restrictions
concerning lavatory smoke detection system and cargo
smoke detection system are applied.
Refer to Item 26-17-01 Lavatory Smoke Detection System,
and
Refer to Item 26-16-01 Smoke Detector in the FWD Cargo
Compartment (if FWD cargo compartment smoke
detection system installed) and
Refer to Item 26-16-02 Smoke Detector in the AFT and the
BULK Cargo Compartments (if AFT cargo compartmentsmoke detection system installed).
Note:
Failure of a single CIDS-SDF channel is
indicated by a MAINTENANCE
message on the STATUS SD page.
Refer to Item 26-00-01 SDCU/SMOKE
MAINTENANCE Message
01.23.22COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-74 Cabin Crew Panel
23-74-01 FAP Display Unit
23-74-01A C 1 0 (O) May be inoperative provided that the safety related
messages on the FAP are considered inoperative.
Refer to Item 52-10-06 DOOR PRESS LOW/CHECK
DOOR PRESSURE Message on the PTP/FAP, and
Refer to Item 25-62-06 Passenger Door Slide PressureMessage on the PTP/FAP (If Installed), and
Refer to Item 25-62-07 Emergency Exit Slide Pressure
Message on the PTP/FAP
OPERATING PROCEDURES
GENERAL INFORMATION
The cabin lighting may be dimmed through the Additional Attendant Panel (AAP) (If available).
23-74-02 EMER pb on
Hardkey FAPSub-panel
23-74-02A 1 1 Must be operative.
23-74-03 Other Controls
on Hardkey FAP
Sub-panel
23-74-03A D 1 0 May be inoperative.
23-74-06 Door Bottle
Pressure
Monitoring on
the FAP
23-74-06A (A320)
(A321)
C
C
4
8
0
0
Refer to Item 52-10-06 DOOR PRESS LOW/CHECK
DOOR PRESSURE Message on the PTP/FAP
12 FEB 12MEL
A320/321MEL/CDL 01.23.23
COMMUNICATIONS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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23 COMMUNICATIONS
23-74 Cabin Crew Panel
23-74-08 Slide Pressure
Monitoring on the
FAP
23-74-08A Refer to Item 25-62-06 Passenger Door Slide Pressure
Message on the PTP/FAP
Refer to Item 25-62-07 Emergency Exit Slide Pressure
Message on the PTP/FAP
Note:
Apply both MEL Items.
23-74-09 Area Call Panel
23-74-09A C 1 0 May be inoperative.
23-74-10 Attendant
Information Panel
(AIP)
23-74-10A C 1 0 May be inoperative.
23-74-11 Additional
Attendant Panel
(AAP)
23-74-11A C 1 0 May be inoperative.
* * *
01.23.24COMMUNICATIONS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-00 MAINTENANCE
Messages on the
STATUS SD page
24-00-01 DC BUS TIE
MAINTENANCE
Message
24-00-01A C 1 - DC BUS TIE MAINTENANCE message may be displayed
on the STATUS SD page.
24-00-03 AC GEN
MAINTENANCE
Message
24-00-03A C 1 - AC GEN MAINTENANCE message may be displayed on
the STATUS SD page.
24-01 Overhead Panels
24-01-01 ELEC Overhead
Panel
24-01-01-01 BAT 1(2) pb-sw
FAULT light
24-01-01-01A C 2 0 One or both may be inoperative.
24-01-01-02 BAT 1(2) pb-sw
OFF light
24-01-01-02A C 2 0 One or both may be inoperative.
24-01-01-03 GEN pb-sw
FAULT light and
APU GEN pb-swFAULT light
24-01-01-03A C 3 1 One GEN pb-sw FAULT light and/or the APU GEN pb-sw
FAULT light may be inoperative provided that the
associated generator indications are operative on the
ELEC SD page.
12 FEB 12MEL
A320/321MEL/CDL 01.24.01
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-01 Overhead Panels
24-01-01 ELEC Overhead
Panel
24-01-01-04 GEN pb-sw OFF
light and APU
GEN pb-sw OFF
light
24-01-01-04A C 3 0 One or more may be inoperative.
24-01-01-05 AC ESS FEED
pb-sw FAULT
light
24-01-01-05A C 1 0 May be inoperative provided that the AC ESS bus
indication is operative on the ELEC SD page.
24-01-01-06 AC ESS FEED
pb-sw ALTN
light
24-01-01-06A C 1 0 May be inoperative provided that the AC ESS bus
indication is operative on the ELEC SD page.
24-01-01-07 EXT PWR pb-sw
AVAIL light
24-01-01-07A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
BEFORE PUSHBACK
Confirm the external power disconnection either on the
ELEC SD page or with the ground crew.
PARKING
- If the APU is not available:
- EXT PWR pb-sw. . . . . . . . . . . . . . . . . . . . . . . . ON
- Confirm the external power connection either on
the ELEC SD page or with the ground crew before
engine shutdown.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.02ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-01 Overhead Panels
24-01-01 ELEC Overhead
Panel
24-01-01-08 EXT PWR pb-sw
ON light
24-01-01-08A C 1 0 May be inoperative.
24-01-01-09 GALY & CAB pb-
sw FAULT light
24-01-01-09A C 1 0 (O) One may be inoperative provided that:
1) For each generator, the AC load indication is operativeon the ELEC SD page, and
2) The GALY & CAB automatic load shed system ischecked operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check of the galley automatic load shed system:
- Supply the electrical network from the APU or theexternal power.
- GALY & CAB pb-sw · · · · · · · · · · · · · · · · · · · · · · AUTO
- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
- Check that a part of the operative galley equipmentdoes not operate.
- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push
Note:
Disregard this procedure if main galleys
are not connected.
12 FEB 12MEL
A320/321MEL/CDL 01.24.03
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-01 Overhead Panels
24-01-01 ELEC Overhead
Panel
24-01-01-10 GALY & CAB pb-
sw OFF light
24-01-01-10A C 1 0 May be inoperative.
24-01-01-11 COMMERCIAL
pb-sw OFF light
24-01-01-11A C 1 0 May be inoperative.
24-01-01-12 BUS TIE pb-sw
OFF light
24-01-01-12A C 1 0 May be inoperative.
24-01-01-13 IDG pb-sw
FAULT light
24-01-01-13A C 2 1 One may be inoperative provided that the frequency and
the temperature indications of the affected generator are
operative on the ELEC SD page.
24-01-02 EMER ELEC
PWR Overhead
Panel
24-01-02-01 RAT & EMER
GEN FAULT
light
24-01-02-01A B 1 0 May be inoperative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.04ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-07 Indications on the
ELEC SD page
24-07-01 AC Generation
Indications on
the ELEC SD
page
24-07-01A C 3 0 (O) One or more indications related to the AC generation may
be inoperative provided that:
1) The load, voltage, and frequency indications areoperative on one engine driven generator , and
2) The associated ELEC GEN 1(2) FAULT alert isoperative, and
3) The galley automatic load shed system is checkedoperative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check that GEN 1(2) pb-sw FAULT light is on (with the
GEN 1(2) pb-sw in the on position).
Check of the galley automatic load shed system:
- Supply the electrical network from the APU or theexternal power.
- GALY & CAB pb-sw · · · · · · · · · · · · · · · · · · · · · · AUTO
- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
- Check that a part of the operative galley equipmentdoes not operate.
- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)
C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push
Note:
Disregard this procedure if main galleys
are not connected.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.24.05
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-07 Indications on the
ELEC SD page
24-07-02 DC Generation
Indications on
the ELEC SD
page (Cont’d)
24-07-02A C 2 0 One or more indications related to the DC generation may
be inoperative.
24-07-03 AC ESS BUS
SHED Indication
on the ELEC SD
page
24-07-03A C 1 0 May be displayed.
24-09 ECAM Alerts
24-09-01 ELEC AC ESS
BUS SHED Alert
24-09-01A C 1 0 (O) May be displayed provided that:
1) The alert is confirmed to be false by troubleshooting,and
2) The AC ESS BUS SHED is checked operative beforeeach flight, and
3) HF 1 is deactivated.
Refer to Item 23-10-01 HF System
OPERATING PROCEDURES
GENERAL INFORMATION
When the ELEC AC ESS BUS SHED alert is displayed onthe EWD:
- The AC ESS BUS SHED message may appear on theELEC SD page,
- The CAPT AOA message may be displayed in theINOP SYS column on the STATUS SD page,
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.06ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-09 ECAM Alerts
24-09-01 ELEC AC ESS
BUS SHED Alert
24-09-01A (Cont’d) OPERATING PROCEDURES(Cont’d)
- The ELEC/AC BUS/8XP/MONG (49VU H11) C/B maytrip.
DURING COCKPIT PREPARATION
COM/HF1 (49VU HA14) C/B · · · · · · · · · · · · · · · · · Pull
Check of the AC ESS BUS SHED:- Supply the electrical network from the APU or the
external power.
- Check that the CAPT right DU is operative.
IN FLIGHT
- If either the ANTI ICE F/O AOA alert or the ANTI ICEF/O PROBES alert is displayed on the EWD, andicing conditions cannot be avoided:- ADR 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- AIR DATA sw . . . . . . . . . . . . . . . . . . . . . . . . . . F/O 3
Note:
If the ADR 2 pb-sw is set to OFF, takeoff
in CONF 1+F is not permitted.
- If either the ANTI ICE STBY AOA alert or the ANTIICE STBY PROBES alert is displayed on the EWD,and icing conditions cannot be avoided:
ADR 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
24-09-02 C/B TRIPPED
Alert
24-09-02A C 1 0 (M) May be displayed provided that the alert is confirmed to be
false by troubleshooting.
MAINTENANCE PROCEDURE
Refer to AMM 24-50-00-040-001
12 FEB 12MEL
A320/321MEL/CDL 01.24.07
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-22 AC Main Generation
24-22-01 AC Main
Generation (IDG,
GCU, Line
Contactor)
24-22-01A B 2 1 (O)(M)
(FD)
One may be inoperative provided that:
1) The flight altitude is limited to 33 000 ft, and
2) The APU and AC auxiliary generation are operativeand used throughout the flight, and
3) The APU fuel pump is operative, and
4) The APU oil consumption is checked adequate for theintended flight, and
5) All busses have power, and
6) The indications and alerts for the remaining AC maingeneration and the AC auxiliary generation areoperative, and
7) The galley automatic load shed system is checkedoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
landing capability is CAT II.
APU fuel consumption with APU GEN pb-sw On:
Note:
When the External Power isdisconnected, the IFE is lost until the
APU supplies the electrical network.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.08ELECTRICAL POWER
A320/321MEL/CDL 30 JUN 12
MEL
I T E M
FL GND 200 250 300 335 390
KG/H 100 63 57 54 49 42
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-22 AC Main
Generation
24-22-01 AC Main
Generation (IDG,
GCU, Line
Contactor)
24-22-01A (Cont’d) OPERATING PROCEDURES(Cont’d)
DURING COCKPIT PREPARATION
Check of the galley automatic load shed system:
- Supply the electrical network from the APU or theexternal power.
- GALY & CAB pb-sw · · · · · · · · · · · · · · · · · · · · · · AUTO
- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
- Check that a part of the operative galley equipmentdoes not operate.
- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push
Note:
Disregard this procedure if main galleys
are not connected.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.24.09
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-22 AC Main Generation
24-22-01 AC Main
Generation (IDG,
GCU, Line
Contactor)
24-22-01A (Cont’d) OPERATING PROCEDURES(Cont’d)
AFTER ENGINE START
Check that the electrical busses have power:
- APU MASTER SW pb-sw · · · · · · · · · · · · · · · · · · · · ON
- APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- GEN 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- GEN 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- On the ELEC SD page, check that all AC busses havepower.
- GEN pb-sw (operative)· · · · · · · · · · · · · · · · · · · · · · · On
- APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- On the ELEC SD page, check that all AC busses havepower.
- APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · On
Note:
If necessary, the IDG may be
disconnected.
CAUTION
For economical reason, the IDG should
not operate for more than 50 flight hours
in the disconnected mode.
MAINTENANCE PROCEDURE
Refer to AMM 24-20-00-040-001
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.10ELECTRICAL POWER
A320321MEL/CDL 12 FEB 12
MEL
I T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-22 AC Main
Generation
24-22-02 AC Bus Tie
Control Function
24-22-02A 1 1 Must be operative.
24-23 AC Auxiliary
Generation
24-23-01 AC Auxiliary
Generation (APU
Generator, GCU,
Line Contactor)
Note:
When the GPCU and the APU
Generator are both inoperative, the
engines cannot be started.
24-23-01A C 1 0 May be inoperative provided that the APU GEN pb-sw is
set to OFF.
24-23-01B A 1 0 May be inoperative for four flights provided that the APU
GEN pb-sw is set to OFF.
24-24 AC EmergencyGeneration
24-24-01 Emergency
Generator
24-24-01A 1 1 Must be operative.
24-24-02 RAT Extension
Automatic
Control
24-24-02A B 1 0 (M) May be inoperative provided that the RAT extension
manual control is checked operative every day.
MAINTENANCE PROCEDURE
Refer to AMM 24-20-00-040-002
12 FEB 12MEL
A320/321MEL/CDL 01.24.11
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-24 AC Emergency
Generation
24-24-03 RAT Extension
Manual Control
24-24-03A B 1 0 May be inoperative.
24-25 AC Essential
Generation
Switching
24-25-01 Manual Transfer
to the AC BUS 2
(ALTN Function)
24-25-01A C 1 0 (O) May be inoperative provided that:
1) The AC ESS FEED pb-sw is set to NORM, and
2) It is checked on the ELEC SD page that the AC BUS 1supplies the AC ESS BUS, and
3) The TR 2 is operative.
OPERATING PROCEDURES
DURING PRELIMINARY COCKPIT PREPARATION
On the ELEC SD page, check that the AC BUS 1supplies the AC ESS BUS.
24-25-02 Automatic
Transfer to the
AC BUS 2
24-25-02A C 1 0 (O) May be inoperative provided that:
1) The AC ESS FEED pb-sw is set to NORM, and2) It is checked on the ELEC SD page that the AC BUS 1
supplies the AC ESS BUS, and
3) The TR 2 is operative.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.12ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
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24 ELECTRICAL POWER
24-24 AC Emergency
Generation
24-25-02 Automatic
Transfer to the
AC BUS 2
24-25-02A (Cont’d) OPERATING PROCEDURES
DURING PRELIMINARY COCKPIT PREPARATION
On the ELEC SD page, check that the AC BUS 1supplies the AC ESS BUS.
24-26 Galley and
Commercial
Supply System
24-26-01 GALY & CAB
Automatic Load
Shed System
24-26-01A Manual Load
Shed System
Operative
C 1 0 May be inoperative provided that the manual load shed
system and the GALY & CAB pb-sw FAULT light are
operative.
24-26-01B All GALY &
CAB Loads
disconnected
C 1 0 (M) May be inoperative provided that all GALY & CAB loads
are disconnected.
MAINTENANCE PROCEDURE
Refer to AMM 24-56-00-040-001
12 FEB 12MEL
A320/321MEL/CDL 01.24.13
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-26 Galley and
Commercial Supply
System
24-26-02 GALY & CAB
Manual Load
Shed System
(GALY & CAB
pb-sw)
24-26-02A All GALY &
CAB loads
disconnected
C 1 0 (M) May be inoperative provided that all GALY & CAB loads
are disconnected.
MAINTENANCE PROCEDURE
Refer to AMM 24-56-00-040-002
24-26-02B COMMERCIAL
supply system
operative
C 1 0 (O)(M) May be inoperative provided that the COMMERCIAL
supply system is checked operative.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- If the AVNCS SMOKE emergency procedure isapplied or if the AVIONICS SMOKE alert isdisplayed on the EWD replace the action to set theGALY & CAB pb-sw to OFF by the followingactions:- EMER EXIT LT selector. . . . . . . . . . . . As required
- COMMERCIAL pb-sw . . . . . . . . . . . . . . . . . . . OFF
Note:
When the COMMERCIAL pb-sw is set
to OFF, the normal cabin lighting goes
off.Minimum cabin lighting is recovered
when the EMER EXIT LT selector is set
to ON.
MAINTENANCE PROCEDURE
Refer to AMM 24-51-00-040-001
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.14ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
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24 ELECTRICAL POWER
24-26 Galley and
Commercial
Supply System
24-26-03 Commercial
Supply System
24-26-03A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- If the AVNCS SMOKE emergency procedure isapplied or if the AVIONICS SMOKE alert isdisplayed on the EWD replace the action to set theCOMMERCIAL pb-sw to OFF by the followingactions:- BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
The F/O PFDU, the F/O NDU, and the ECAM lower display are lost.- If the smoke persists:
- GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
When the GEN 2 pb-sw is set to on, all the
electrical busses are recovered but the TR 2
remains inoperative
- BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Before the landing gear extension:
- GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
When the GEN 2 pb-sw is set to on, all the electrical
busses are recovered but the TR 2 remains
inoperative
- BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
24-28-01 Static Inverter
AC Generation
24-28-01A 1 1 Must be operative.
12 FEB 12MEL
A320/321MEL/CDL 01.24.15
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-32 DC Main Generation
(TR 1, TR 2)
24-32-01 DC Main
Generation (TR
1, TR 2)
24-32-01A TR1 inoperative A 2 1 (O)(FD) TR 1 may be inoperative provided repairs are made within
two flight days.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING PRELIMINARY COCKPIT PREPARATION
TR 1/CNTOR/SPLY (125VU CF01) C/B· · · · · · · · · Pull
On the ELEC SD page, check that the TR 2 and theESS TR voltages are both equal to or above 27 V.On the battery voltage indicator, check that the BAT 1and the BAT 2 voltages are both equal to or above25.5 V.
The batteries must be set to OFF during this check.
24-32-01B TR 2 inoprative A 2 1 (O)(M)
(FD)
TR 2 may be inoperative provided that:
1) The AC ESS FEED control is checked operative everyday, and
2) The ISIS airspeedindication is operative, and
3) The ISIS altitude indication is operative, and
4) The ISIS aircraft attitude indication is operative, and
5) The standby compass is operative, and
6) Repairs are made with two flight days.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.16ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
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24 ELECTRICAL POWER
24-32 DC Main
Generation (TR 1,
TR 2)
24-32-01 DC Main
Generation (TR
1, TR 2)
24-32-01B (Cont’d) OPERATING PROCEDURES(Cont’d)
DURING PRELIMINARY COCKPIT PREPARATION
TR 2/CNTOR/SPLY (124VU BC01) C/B· · · · · · · · · Pull
On the ELEC SD page, check that the TR 1 and theESS TR voltages are both equal to or above 27 V.On the battery voltage indicator, check that the BAT 1and the BAT 2 voltages are both equal to or above25.5 V.The batteries must be set to OFF during this check.
AC ESS FEED pb-sw · · · · · · · · · · · · · · · · · · · · · ALTN
IN FLIGHT
- In the case of failure of the AC BUS 2, all DUs are
lost. In this case: AC ESS FEED pb-sw· · · · · · · · · · · · · · · · · · · · · · Norm
- In the case of failure of the AC BUS 1:
RAT MAN ON pb-sw (on HYD overheadpanel)....................................................................Set
MAINTENANCE PROCEDURE
Refer to AMM 24-30-00-040-002
24-34 DC Emergency
Generation (ESS
TR)
24-34-01 DC Emergency
Generation (ESS
TR)
24-34-01A 1 1 Must be operative.
12 FEB 12MEL
A320/321MEL/CDL 01.24.17
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-35 DC Essential and
Normal Generation
Switching
24-35-01 DC TIE
Contactor 1PC1
(DC BUS 1-DC
BAT BUS), 4PC
(DC ESS BUS-
DC BAT BUS)
24-35-01A C 2 1 One may be inoperative in the open position.
24-35-02 DC TIE
Contactor 1PC2
(DC BUS 2-DC
BAT BUS)
24-35-02A 1 1 Must be operative.
24-38 DC Battery
Generation
24-38-01 BAT 1(2)
Channel
24-38-01A 2 2 Must be operative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.18ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
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24 ELECTRICAL POWER
24-38 DC Battery
Generation
24-38-02 Battery Charger
Limiter (BCL)
24-38-02A A 2 1 (O)(M)
(FD)
One may be inoperative for 10 flights provided that:
1) No APU start is attempted neither on ground nor inflight, and
2) Both AC main generations are operative, and
3) The refueling is made with an external power unitconnected, and
4) The battery associated with the inoperative BCL ischarged before each flight.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Do not use the APU.
Use a ground power unit to start the engines onground.
DURING PRELIMINARY COCKPIT PREPARATION
- If BAT 1 is affected:
BAT 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- If BAT 2 is affected:
BAT 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
MAINTENANCE PROCEDURE
Refer to AMM 24-30-00-040-001
24-38-03 Battery
Voltmeter
24-38-03A C 2 0 One or both may be inoperative provided that the
associated voltage indication is operative on the ELEC SD
page.
12 FEB 12MEL
A320/321MEL/CDL 01.24.19
ELECTRICAL POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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24 ELECTRICAL POWER
24-41 AC External Power
Control
24-41-01 Ground Power
Control Unit
(GPCU)
24-41-01A C 1 0 May be inoperative provided APU Generator is operative.
Note:
When the GPCU and the APU
Generator are both inoperative, the
engines cannot be started.
24-41-02 External Power
Receptacle
24-41-02A C 1 0 (M) May be inoperative provided that the receptacle is
placarded inoperative and not used.
Note:
When the GPCU and the APU
Generator are both inoperative, the
engines cannot be started.
MAINTENANCE PROCEDURE
Refer to AMM 24-41-00-040-001
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.24.20ELECTRICAL POWER
A320/321MEL/CDL 12 FEB 12
MEL
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25 EQUIPMENT/FURNISHINGS
25-07 Indications on the
DOOR/OXY SD
page
25-07-01 Passenger Door
Slide Permanently
Indicated Armed
(A320)
(M) Note:
The correct indication may be recovered
by performing the AMM task 52-70-00-
040-07.
25-07-01A C 4 0 (O) One or more may be permanently indicated in the armed
position provided that the associated slide is visually
checked to be armed before each flight.
OPERATING PROCEDURES
ON GROUND
Cabin crew must confirm before each flight that the
associated slide is armed.
25-07-01 Cabin Passenger Door / Emergency
Exit Slide
Permanently
Indicated Armed
(A321)
(M) Note:
The correct indication may be recovered
by performing the AMM task 52-70-00-
040-07.
25-07-01A C 8 0 (O) One or more may be permanently indicated in the armed
position provided that the associated slide is visually
checked to be armed before each flight.
OPERATING PROCEDURES
ON GROUND
Cabin crew must confirm before each flight that the
associated slide is armed.
12 FEB 12MEL
A320/321MEL/CDL
01.25.01EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-07 Indications on the
DOOR/OXY SD page
25-07-02 Passenger Door
Slide Permanently
Indicated Not
Armed
(A320)
(M) Note:
The correct indication may be recovered
by performing the AMM task 52-70-00-
040-07.
25-07-02A Associated
door
considered
operative
C 4 0 (O)(FD) One or more may be permanently indicated in the not
armed position provided that:
1) The aircraft is not operated at night, and
2) The associated slide is visually checked to be armedbefore each flight.
OPERATING PROCEDURES
ON GROUND
Cabin crew must confirm before each flight that the
associated slide is armed.
25-07-02 Cabin Passenger Door / Emergency
Exit Slide
Permanently
Indicated Not
Armed
(A321)
25-07-02A Associated
door
considered
operative
C 8 0 (O)(FD) One or more may be permanently indicated in the not
armed position provided that:
1) The aircraft is not operated at night, and
2) The associated slide is visually checked to be armed
before each flight.
OPERATING PROCEDURES
ON GROUND
Cabin crew must confirm before each flight that the
associated slide is armed.
01.25.02EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-07 Indications on the
DOOR/OXY SD
page
25-07-03 Overwing
Emergency Exit
Slide Permanently
Indicated Armed
Note:
The correct indication may be recovered
by performing the AMM task 52-70-00-
040-07.
25-07-03A C 2 0 (M) One or both may be permanently indicated in the armedposition provided that the associated slide is visually
checked to be armed before the first flight of the day.
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-008
25-07-04 Overwing
Emergency Exit
Slide Permanently
Indicated NotArmed
Note:
The correct indication may be recovered
by performing the AMM task 52-70-00-
040-07.
25-07-04A Overwing
emergency
exits
considered
operative
C 2 0 (M)(FD)One or both may be permanently indicated in the not
armed position provided that:
1) The aircraft is not operated at night, and
2) The associated slide is visually checked to be armedbefore the first flight of the day.
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-009
12 FEB 12MEL
A320/321MEL/CDL
01.25.03EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-11 Pilot Seats
25-11-01 Pilot Seat Manual
Horizontal
Adjustment
25-11-01A 2 2 Both must be operative.
25-11-02 Pilot Seat Manual
Vertical
Adjustment
25-11-02A Associated
electrical
control
operative
C 2 0 One or both may be inoperative provided that the
associated electrical control is operative.
25-11-02B Associated
electrical
control
inoperative
C 2 0 One or both may be inoperative provided that the seating
position is acceptable to the affected crewmember.
25-11-03 Pilot Seat ReclineAdjustment
25-11-03A C 2 0 (M) One or both may be inoperative provided that the seat is
secured in an upright position acceptable to the affected
crewmember.
MAINTENANCE PROCEDURE
Refer to AMM 25-11-00-040-001
25-11-04 Pilot Seat Other
Manual
Adjustments
25-11-04A C 2 0 One or more may be inoperative provided that the seating
position is acceptable to the affected crewmember.
01.25.04EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-11 Pilot Seats
25-11-05 Pilot Seat
Electrical
Adjustment
25-11-05A C 2 0 (M) One or both may be inoperative provided that the electrical
adjustment of the associated seat is deactivated.
MAINTENANCE PROCEDURE
Refer to AMM 25-11-00-040-002
25-11-06 Pilot Seat
Shoulder Harness
25-11-06A A 2 1 (O)(FD) May be inoperative on the F/O seat for three flights.
OPERATING PROCEDURES
BEFORE TAKEOFF
The takeoff briefing should include the status of the
affected seat and the position to be adopted by the F/O in
the case of RTO.
To cope with any potential RTO:
The F/O must tightly fasten operative harness strap.
DURING FLIGHT
For any phase of flight in turbulence atmosphere:
The F/O must fasten the belts accordingly.
BEFORE LANDING
The landing briefing should include the status of theaffected seat and the position to be adopted by the F/O in
the case of high deceleration at landing.
To cope with any potential high deceleration at landing:
The F/O must tightly fasten operative harness straps.
12 FEB 12MEL
A320/321MEL/CDL
01.25.05EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-11 Pilot Seats
25-11-07 Pilot Seat Fifth
Strap
25-11-07A C 2 0 (O) One or both may be inoperative.
OPERATING PROCEDURES
DURING FLIGHT
To cope with any potential turbulence situation:
The crewmember of the affected seat must tightly fasten
the operative harness straps.
25-11-08 Pilot Sidestick
Armrest Height
Adjustment
25-11-08A C 2 1 One may be inoperative provided that the associated
armrest position is acceptable to the affected
crewmember.
25-11-09 Pilot Sidestick
Armrest Pitch
Adjustment
25-11-09A C 2 1 One may be inoperative provided that the associated
armrest position is acceptable to the affected
crewmember.
25-11-10 Pilot Sidestick
Armrest Memory
Position Display
25-11-10A C 2 0 One or both may be inoperative.
01.25.06EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-11 Pilot Seats
25-11-11 Pilot Inboard
Armrest Vertical
Adjustment
25-11-11A C 2 0 One or both may be inoperative.
25-11-12 Pilot Seat
Headrest
25-11-12A C 2 0 One or both may be inoperative.
25-12 Third and Fourth
Occupant Seats
25-12-01 Third Occupant
Seat
25-12-01A Seat stowed C 1 0 (FD) May be inoperative provided that the seat is in its stowed
position.
25-12-02 Third OccupantSeat Shoulder
Harness
25-12-02A C 1 0 (FD) May be inoperative provided that the seat is not occupied
during takeoff and landing.
12 FEB 12MEL
A320/321MEL/CDL
01.25.07EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-12 Third and Fourth
Occupant Seats
25-12-03 Third Occupant
Seat Abdominal
Belt
25-12-03A C 1 0 (FD) May be inoperative provided that:
1) The seat is placarded inoperative, and
2) The seat is not occupied.
25-12-04 Third Occupant
Seat Fifth Strap
25-12-04A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
With any potential turbulance situation the crewmember
must lightly fasten the operative straps.
25-12-05 Fourth Occupant
Seat
25-12-05A Seat stowed C 1 0 May be inoperative provided that the seat is in its stowed
position.
25-12-06 Fourth Occupant
Seat Shoulder
Harness
25-12-06A C 1 0 (FD) May be inoperative provided that the seat is not occupied
during takeoff and landing.
25-12-07 Fourth Occupant
Seat Abdominal
Belt
25-12-07A C 1 0 (FD) May be inoperative provided that:
1) The seat is placarded inoperative, and
2) The seat is not occupied.
01.25.08EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-12 Third and Fourth
Occupant Seats
25-12-08 Fourth Occupant
Seat Fifth Strap
25-12-08A D 1 0 (O) May be inoperative.
OPERATING PROCEDURES
With any potential turbulance situation the crewmember must lightly fasten the operative straps.
25-13 Lining and
Furnishings
25-13-01 Pilot Sliding Table
25-13-01A Table stowed C 2 0 One or both may be inoperative in its stowed position.
25-13-02 Pilot Retractable
Footrest
25-13-02A Footreststowed
C 4 0 One or more may be inoperative in its stowed position.
25-20 Cabin Seats
25-20-01 Passenger Seat
25-20-01A (A320)
(A321)
C
C
C
132
116
165
86
70
100
(FD) May be inoperative provided:
a) Seat does not block and Emergency Exit,
b) seat does not restrict any passenger from access tothe main aircraft aisle, and
c) Affected seat(s) are blocked and placarded “DO NOTOCCUPY”.
Note 1:
A seat with an inoperative seat belt is
considered inoperative.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL
01.25.09EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-20 Cabin Seats
25-20-01 Passenger Seat
25-20-01A (Cont’d) Note 2:
Inoperative seats do not affect the
required number of Flight Attendants.
Note 3:
Affected seat(s) may include the seat(s)
behind and/or adjacent outboard seats.
25-20-03 Cabin Attendant
Seat
Note:
A cabin attendant seat with aninoperative or missing seat belt or
harness should be considered
inoperative.
(Cont’d on next page)
01.25.10EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-20 Cabin Seats
25-20-03 Cabin Attendant
Seat (cont’d)
25-20-03B Required
cabin
attendant seat
(A320)
(A321)
C
C
5
7
4
5
(O)(M)
(FD)
One required cabin attendant seat may be inoperative or
not usable provided that:
1) The cabin attendant assigned to affected seatoccupies a passenger seat as close to or closer than
nearest seated passenger to the associated exit, and2) The passenger seat to be used by cabin attendant is
correctly placarded, and
3) The cabin attendant can reach assigned exit andemergency equipment in nearly the same time as fromnormally assigned seat, and
4) The direct view of passenger cabin by flight attendantsis not impaired, and
5) The alternate procedures are established for displacedflight attendant according to national regulations, and
6) The affected seat is secured in its stowed position or
removed.OPERATING PROCEDURES
Captin brief all cabin crew regarding the passenger seat
that occupie by assigned flight attendant.
MAINTENANCE PROCEDURE
Refer to AMM 25-22-00-040-001
01 MAY 12MEL
A320/321MEL/CDL
01.25.11EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-28 Overhead Storage
25-28-01 Overhead Storage
Bin(s)/Cabin and
Galley storage
Compartment/
Closets
25-28-01A (A320)
(A321)
C
C
74
87
68
80
(M) May be inoperative provided:
a) Associated bin or compartment is placarded DO NOTUSE,
b) Any emergency equipment located in affectedcompartment is removed or considered inoperative,and
c) Cabin crew must be notified
NOTE:
These provisions are not intended to
prohibit inspections by crew members.
MAINTENANCE PROCEDURE
Refer to AMM 25-20-00-040-001
25-35 Galley Equipment
25-35-01 Galley Waste
Compartment
Flapper Door
25-35-01A C 3 0 (O)(M) One or more may be inoperative or missing provided that:
1) The galley waste compartment is empty, and
2) The associated access is secured in the closedposition to prevent waste introduction.
Note:
Non-safety related galley equipment is
not listed in this MEL.
(Cont’d on next page)
01.25.12EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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25 EQUIPMENT/FURNISHINGS
25-35 Galley Equipment
25-35-01 Galley Waste
Compartment
Flapper Door
25-35-01A (cont’d) OPERATING PROCEDURES
Inform cabin crew to essure adequate galley waste
storage capacity is maintained during periods of flightwhen affected containers are secured empty.
MAINTENANCE PROCEDURE
Refer to AMM 25-35-00-040-001
25-40 Lavatories
25-40-01 Toilet Waste
Compartment
Flapper Door
25-40-01A C 3 2 (O)(M)(FD) One may be inoperative or missing provided that:1) The toilet waste compartment is empty, and
2) The associated access is secured in the closedposition to prevent waste introduction.
Note:
Non-safety related toilet equipment is
not listed in this MEL.
OPERATING PROCEDURES
- Lavatory door placarded “INOPERATIVE-DO NOTENTER”.
- Lavatory is used only by crew members.
- Ensure that affected lavatory is kept locked and is notentered exept for crew member.
MAINTENANCE PROCEDURE
Refer to AMM 25-40-00-040-001
12 FEB 12MEL
A320/321MEL/CDL
01.25.13EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-40 Lavatories
25-40-02 Exterior Lavatory
Ashtray
25-40-02A D 4 0 One or more may be damaged or missing provided that
the flight is non-smoking.
25-40-03 Interior Lavatory
Ashtray
25-40-03A Lavatory fire
extinguishing
system
operative
C 3 0 One or more may be damaged or missing provided that
the associated lavatory fire extinguishing system is
operative.
25-40-03B Lavatory
locked closed
C 3 2 (FD) One may be damaged or missing provided t hat t he
associated lavatory is locked closed and placarded
inoperative.
25-50 CargoCompartments
25-50-01 Cargo Loading
System
25-50-01A D 2 0 (FD) May be inoperative provided Ramp Load Control
Supervisor must check and confirm to the flight crew that
cargo compartments are loaded normally.
01.25.14EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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25 EQUIPMENT/FURNISHINGS
25-50 Cargo
Compartments
25-50-02 Decompression
Panels in the
Cargo
Compartments
25-50-02A C 23 0 (FD) One or more may be damaged or missing provided that
the associated cargo compartment is empty or does not
contain flammable or combustible materials.
25-50-03 Sidewall Linings
and Ceiling Panels
in the Cargo
Compartments
25-50-03A Damaged
panel
C 41 0 (FD) One or more may be damaged provided that the
associated cargo compartment is empty or does not
contain flammable or combustible materials.
25-50-04 Cargo
CompartmentRestraint
Components
(Nets, Attach
Points,
Stanchions)
25-50-04A C 5 0 One or more may be missing or damaged provided that
the remaining operative ones are enough to secure the
load in the affected compartment.
12 FEB 12MEL
A320/321MEL/CDL
01.25.15EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-62 Cabin Escape
Facilities
25-62-01 Cabin Passenger
Door Slide or Slide
Raft
25-62-01A Slide
inoperative
4 4
25-62-02 Overwing
Emergency Exit
Slide or Slide Raft
(A320)
25-62-02A Slide
inoperative
2 2
25-62-03 Emergency ExitSlide or Slide Raft
(A321)
25-62-03A Slide
inoperative
4 4
01.25.16EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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25 EQUIPMENT/FURNISHINGS
25-62 Cabin Escape
Facilities
25-62-04 SLIDE ARMED
light
(A320)
25-62-04A C 6 0 One or more may be inoperative provided maintenance
confirm that it’s only lit problem.
25-62-04 SLIDE ARMED
light
(A321)
25-62-04A C 8 0 One or more may be inoperative provided maintenance
confirm that it’s only lit problem.
25-62-05 Survival Kit
25-62-05A 4 4 Must be attached to each required life raft for over water
flying.
25-62-06 Passenger Door CHECK SLIDE
PRESSURE
Message on Flight
Attendant Panel
(FAP)
(A320)
25-62-06A C 4 0 (M) One or more messages may be displayed provided that
the slide bottle pressure is checked before the first MMEL
dispatch and then every 600 flight hours or every 4
months, whichever occurs first.
MAINTENANCE PROCEDURE
Refer to AMM 25-62-00-040-009
12 FEB 12MEL
A320/321MEL/CDL
01.25.17EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-62 Cabin Escape
Facilities
25-62-06 Passenger Door
CHECK SLIDE
PRESSURE
Message on Flight
Attendant Panel
(FAP)
(A321)
25-62-06A C 8 0 (M) One or more messages may be displayed provided that
the slide bottle pressure is checked before the first MMEL
dispatch and then every 600 flight hours or every 4
months, whichever occurs first.
MAINTENANCE PROCEDURE
Refer to AMM 25-62-00-040-009
25-62-07 Overwing
Emergency Exit
CHECK SLIDE
PRESSUREMessage on Flight
Attendant Panel
(FAP)
(A320)
25-62-07A Check of the
slide bottle
pressure
C 2 0 (M) One or both messages may be displayed provided that the
associated slide bottle pressure is checked before the first
flight of each day.
MAINTENANCE PROCEDURE
Refer to AMM 25-62-00-040-005
01.25.18EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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25 EQUIPMENT/FURNISHINGS
25-62 Cabin Escape
Facilities
25-62-08 Overwing Escape
Life Line
25-62-08B Non extended
overwater
flight
C 2 0 (FD) One or both may be inoperative or missing provided that
extended overwater flight is not conducted.
25-63 Evacuation
Signaling
Equipment
25-63-01 Emergency
Evacuation
Signaling System
(COMMAND pb-
sw, HORN SHUT
OFF pb,
CAPT&PURS andCAPT sw)
25-63-01A B 1 0 (O) May be inoperative.
OPERATING PROCEDURES
GENERAL INFORMATION
If necessary, the information will be given through the
passenger address system or the cabin interphone
system.
12 FEB 12MEL
A320/321MEL/CDL
01.25.19EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-64 First Aid Equipment
25-64-01 First Aid Kit
25-64-01A A 3 2 One may be incomplete, missing or used provided:
1) Affected FAK is identifiable as a unit that could not bemistaken for a fully serviceable unit, and
2) Repairs or replacements are made within 3 flightcycles.
Note:
- One serviceable Firs Aid Kit is required
on ferry flights.
- A first Aid Kit is considered serviceable
when Kit contains the following contents
Adhesive bandage compresses, 1-inch 16
Antiseptic swabs 20
Ammonia inhalants 10
Bandage compresses, 4-inch 8
Triangular bandage compresses, 4-inch 5
Arm splint, non inflatable 1Leg splint, non inflatable 1
Roller bandage, 4-inch 4
Adhesive tape, 1-inch standard roll 2
Bandage scissors 1
Protective latex gloves or equivalent nonpermeable gloves 1 Pair
01.25.20EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-64 First Aid
Equipment
25-64-02 Emergency
Medical Kit
25-64-02A 1 1 Must be carried for all passenger flight. Must also be
carried for ferry flights where the aircraft is being
repositioned for a passenger flight.
Note:
Ferry flight terminating in JED do not
require the Doctor’s Emergency Kit. In
addition, ferry flight to other stations
besides Jeddah do not requir the
Doctor’s Emergency Kit if advance
coordination is none to ensure that a
Doctro’s Emergency Kit is available at
the terminatijng station to be installed
prior to the aircraft resuming passenger
service.
12 FEB 12MEL
A320/321MEL/CDL
01.25.21EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-64 First Aid Equipment
25-64-03 Automated
External
Defibrillator (AED)
25-64-03A 1 1 (M) Must be carried for all passenger flights.
MAINTENANCE PROCEDURES:
Refer to maintenance task.
01.25.22EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-65 Emergency
Equipment
25-65-01 Cockpit Flashlight
25-65-01A C 4 0 May be inoperative or missing provided flight deck
member assigned to associated station has a flashlight
with equivalent characteristics readily available.
25-65-02 Cabin Flashlight
25-65-02A C 6 0 May be inoperative or missing provided cabin
crewmember assigned to associated seat has a flashlight
with equivalent characteristics readily available.
25-65-03 Crash
Axe/Crowbar
25-65-03A 1 1 Must be available.
25-65-04 Emergency
Locator
Transmitter (ELT)
25-65-04A Survival Type
ELTs
1 1
25-65-04B Fixed ELTs 1 1 Must be operative.
12 FEB 12MEL
A320/321MEL/CDL
01.25.23EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-64 First Aid Equipment
25-65-05 Fireproof Gloves
25-65-05A All damaged
or missing
C 2 1 One may be damaged or missing.
25-65-05B One available 1 1 One must be available.
25-65-06 Megaphone
25-65-06A 2 2 Must be available and operative.
25-66 Floatation and
Survival Equipment
25-66-01 Life Vest
25-66-01A (A320)
(A321)
C
C
C
125
154
180
125
154
180
(FD) Life vest required for all over water flight , and a life vest
must be available for each passenger and crew on board.
25-66-02 Supplementary
Life Raft
25-66-02A C 1 1 (FD) Must be available for all over water flight.
01.25.24EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-70 Non-Essential
Equipment &
furnishings
25-70-01 Non-Essential
Equipment &
furnishings (NEF)
25-70-01A D 17 9 (FD) Nonessential Equipment & Furnishings (NEF) are those
items installed on the aircrfaft as part of the original
certification, supplemental type certificate, or engineering
order that have no effect on the safe operation of flight and
would not be required by the applicable certification rules
or operational rules. They are those items that if
inoperative, damaged or missing have no effect on the
aircraft ability to be operated safely under all operational
conditions. these Nonessential items may be installed in
areas including, but not limited to, the passenger
compartment, flight deck area,service areas, cargo
areas,crew rest areas,lavatories, and galley areas. Items
addressed elsewhere in this MEL are not included.
25-70-01B25-70-01C
25-70-01D
25-70-01E
25-70-01F
25-70-01J
Coffee MakersOvens
Air Chillers
Hot Cups
Hot Jugs
Bun Warmers
DD
D
D
D
D
6
2
1
1
2
5 34
1
0
0
1
(FD) Any number or combination of galley equipment may beinoperative provided the in-flight supervisor/purser is
notified and determines that the operative galley
equipment available is adequate to support the associated
passenger service throughout the flight(s).
Note:
Captain will brief the FAIC of the
location of the inoperative galley
equipment, not to use the inoperative
galley equipment and that the
inoperative galley oven(s) must remain
empty.
12 FEB 12MEL
A320/321MEL/CDL
01.25.25EQUIPMENT/
FURNISHINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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25 EQUIPMENT/FURNISHINGS
25-70 Non-Essential
Equipment &
furnishings
25-70-04 Movie/stereo
Equipment
25-70-04A D 1 0
25-70-05 Overhead Readig
Lamp
25-70-05A (A320)
(A321)
C
C
C
116
132
165
0
0
0
Any number may be inoperative
* * *
01.25.26EQUIPMENT/FURNISHINGS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-00 MAINTENANCE
Message on the
STATUS SD page
26-00-01 SMOKE
MAINTENANCE
Message
26-00-01A C 1 - SMOKE MAINTENANCE message may be displayed on
the STATUS SD page.
26-01 Overhead Panels
26-01-01 FIRE Overhead
Panel
26-01-01-01 Bulb/LED in the
ENG FIRE-PUSH
pb-sw
26-01-01-01A C 16 8 A maximum of four bulbs or LEDs may be inoperative in
each ENG FIRE-PUSH pb-sw.
26-01-01-02 ENG AGENT pb
DISCH light
26-01-01-02A One inoperative
on each engine
C 4 2 (M) One may be inoperative on each engine provided that the
associated bottle is checked before the first flight of each
day.
MAINTENANCE PROCEDURE
Refer to AMM 26-21-00-040-001
26-01-01-02B One inoperative
on one engine
A 4 2 (M) Both may be inoperative on one engine for four flights or
15 flight hours, whichever occurs first, provided that the
associated bottles are checked before each flight.
MAINTENANCE PROCEDURE
Refer to AMM 26-21-00-040-001
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.26.01
FIRE PROTECTION
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26 FIRE PROTECTION
26-01 Overhead Panels
26-01-01 FIRE Overhead
Panel
26-01-01-03 ENG AGENT pb
SQUIB light
26-01-01-03A C 4 2 (M) One may be inoperative for each engine provided Engine
extinguishing system firing circuit is checked operative
before the first flight of the day.
MAINTENANCE PROCEDURE
Refer to AMM 26-21-00-040-003
26-01-01-04 Bulb/LED in the
APU FIRE-PUSH
pb-sw
26-01-01-04A A maximum of
four bulbs or
LEDs
inoperative
C 8 4 A maximum of four bulbs or LEDs may be inoperative.
26-01-01-04B Five or more
bulbs or LEDs
inoperative
C 8 0 (M) Five or more bulbs or LEDs may be inoperative provided
that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
26-01-01-05 APU AGENT pb
DISCH light
26-01-01-05A Check of bottle
pressure
C 1 0 (M) May be inoperative provided that the bottle is checked
before the first flight of each day.
MAINTENANCE PROCEDURE
Refer to AMM 26-22-00-040-004
26-01-01-05B APU
deactivated
C 1 0 (M) May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
01.26.02FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-01 Overhead Panels
26-01-01 FIRE Overhead
Panel
26-01-01-06 APU AGENT pb
SQUIB light
26-01-01-06A C 1 0 (M) May be inoperative provided that the APU extinguishing
system firing circuit is checked operative before the first
flight of each day.
MAINTENANCE PROCEDURE
Refer to AMM 26-22-00-040-005
26-01-01-06B C 1 0 (M) May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
26-01-01-31 ENG FIRE TEST
pb
26-01-01-31 C 2 1 (M) One may be inoperative provided that the associated
engine fire extinguishing and detection systems are
checked operative before the first flight of each day.
MAINTENANCE PROCEDURE
Refer to AMM 26-21-00-040-002
12 FEB 12MEL
A320/321MEL/CDL 01.26.03
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-01 Overhead Panels
26-01-01 FIRE Overhead
Panel
26-01-01-32 APU FIRE TEST
pb
26-01-01-32A Daily check C 1 0 (M) May be inoperative provided that the APU extinguishing
system firing circuit and the bottle low pressure detection
system are checked operative before the first flight of each
day.
MAINTENANCE PROCEDURE
Refer to AMM 26-22-00-040-012
26-01-01-32B APU
deactivated
C 1 0 (M) May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
26-01-01-33 APU FIRE PUSH
pb-sw
26-01-01-33A C 1 0 (M) May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
26-01-01-34 APU AGENT pb
26-01-01-34A C 1 0 (M) May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
01.26.04FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-01 Overhead Panels
26-01-02 CARGO SMOKE
Overhead Panel
26-01-02-01 CARGO SMOKE
DISCH light
26-01-02-01A Check of bottle
weight
C 2 0 (M) May be inoperative provided that the associated bottle
weight is checked before the first flight of each day.
MAINTENANCE PROCEDURE
Refer to AMM 26-23-00-040-001
26-01-02-01B Associated
bottle
considered
inoperative
B 2 1 May be inoperative provided that the associated bottle is
considered inoperative.
Refer to Item 26-23-01 Cargo Agent Bottle
26-12 Engine Fire and
Overheat
Detection
26-12-01 Engine Fire
Detection Loop
A on the
Engine 1
26-12-01 C 1 0 One may be inoperative provided that:
1) The associated detection loop B is operative, and
2) The engine fire test is made before each flight.
26-12-02 Engine Fire
Detection Loop
A on the
Engine 2
26-12-02 C 1 0 May be inoperative provided that the engine fire test is
made before each flight.
12 FEB 12MEL
A320/321MEL/CDL 01.26.05
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-12 Engine Fire and
Overheat Detection
26-12-03 Engine Fire
Detection Loop
B on the
Engine 1
26-12-03A C 1 0 May be inoperative provided that the engine fire test is
made before each flight.
26-12-04 Engine Fire
Detection Loop
B on the
Engine 2
26-12-04A C 1 0 One may be inoperative provided that the engine fire test
is made before each flight.
26-12-05 FIRE light on the
ENG MASTER
Panel
26-12-05A C 2 0 One or both may be inoperative.
26-13 APU Fire and
Overheat Detection
26-13-01 APU Fire
Detection
Loop A
26-13-01A C 1 0 One may be inoperative provided that:
1) The associated detection loop B is operative and,
2) The APU fire test is made before each APU start, and3) During APU operations on ground, APU condition is
continuously monitored in the cockpit.
01.26.06FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-13 APU Fire and
Overheat
Detection
26-13-01 APU Fire
Detection
Loop A
26-13-01B C 1 0 (M) One may be inoperative provided that the APU is
deactivated.
Refer to Item 49-10-01C Power Plant (APU)
26-13-02 APU Fire
Detection
Loop B
26-13-02A C 1 0 One may be inoperative provided that the APU fire test is
made before each APU start.
26-13-02B C 1 0 (M) One may be inoperative provided that the APU is
deactivated.
Refer to Item 49-10-01C Power Plant (APU)
26-15 Avionics
Compartment
Smoke Detection
26-15-01 Avionics Smoke
Detection
System
26-15-01A A 1 0 (O)(FD) May be inoperative.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
Disregard the BLOWER pb-sw FAULT light and the CAB
FANS pb-sw FAULT light illuminated on the
VENTILATION overhead panel.
IN FLIGHT
In the case of an electrical smoke:
Apply the AVNCS SMOKE emergency procedure.Refer to the QRH/ABN-26-FIRE PROTECTION.
12 FEB 12MEL
A320/321MEL/CDL 01.26.07
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-16 Cargo Compartment
Smoke Detection
26-16-01 Smoke Detector
in the FWD
Cargo
Compartment
(A320)
Note:
i. The cargo smoke detection function is part
of the CIDS Smoke Detection Function
(CIDS-SDF).
Refer to Item 23-73-10-01 Smoke DetectionFunction (CIDS-SDF)
ii. Failure of a single detector in the cavity is
indicated by a MAINTENANCE message on
the STATUS SD page.
Refer to Item 26-00-01 SDCU/SMOKE
MAINTENANCE Message
iii. Depending on applicable regulation, smoke
detection system may be required for
dispatch.
26-16-01A Empty FWD
cargocompartment
C 2 0 (O)(FD) Both detectors in the cavity may be inoperative provided
that the FWD cargo compartment is empty.
OPERATING PROCEDURES
Refer to item 26-16-01D for operating procedure.
26-16-01D Check of liner
integrity
B 2 0 (O)(FD) Both detectors in the cavity may be inoperative provided
procedure are established and used to verify associated
cargo compartment remains empty or contains only empty
cargo containers, cargo handling equipment, pallets,
ballast (ballast may be loaded in ULD's).
OPERATING PROCEDURES
Ramp Load Control Supervisor to physically check and
confirm to the flight crew that cargo compartment(s) are
either empty or only contain empty cargo containers,
pallets, cargo restraint components
01.26.08FIRE PROTECTION
A320/321MEL/CDL 01 MAY 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-16 Cargo
Compartment
Smoke Detection
26-16-01 Smoke Detector
in the FWD
Cargo
Compartment
(A321)
Note:
i. The cargo smoke detection function
is part of the CIDS Smoke Detection
Function (CIDS-SDF).
Refer to Item 23-73-10-01 SmokeDetection Function (CIDS-SDF)
ii. Failure of a single detector in the
cavity is indicated by a
MAINTENANCE message on the
STATUS SD page.
Refer to Item 26-00-01
SDCU/SMOKE MAINTENANCE
Message
26-16-01A B 4 0 (O)(FD) Both detectors in one or both cavities may be inoperative
provided that the FWD cargo compartment is empty or
does not contain flammable or combustible materials.
OPERATING PROCEDURES
Ramp Load Control Supervisor to physically check and
confirm to the flight crew that cargo compartment(s) are
either empty or only contain empty cargo containers,
pallets, cargo restraint components
01 MAY 12MEL
A320/321MEL/CDL 01.26.09
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-16 Cargo Compartment
Smoke Detection
26-16-02 Smoke Detector
in the AFT and
the BULK Cargo
Compartments
(A321)
Note:
i. The cargo smoke detection function is part
of the CIDS Smoke Detection Function
(CIDS-SDF).
Refer to Item 23-73-10-01 Smoke DetectionFunction (CIDS-SDF)
ii. Failure of a single detector in the cavity is
indicated by a MAINTENANCE message on
the STATUS SD page.
Refer to Item 26-00-01 SDCU/SMOKE
MAINTENANCE Message
26-16-02A B 6 0 (O)(FD) Both detectors in one or more cavities may be inoperative
provided that the AFT and the BULK cargo compartments
are empty or do not contain flammable or combustible
materials.
OPERATING PROCEDURES
Ramp Load Control Supervisor to physically check and
confirm to the flight crew that cargo compartment(s) are
either empty or only contain empty cargo containers,
pallets, cargo restraint components
01.26.10FIRE PROTECTION
A320/321MEL/CDL 01 MAY 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-16 Cargo
Compartment
Smoke Detection
26-16-02 Smoke Detector
in the AFT and
the BULK Cargo
Compartments
(A320)
26-16-02C C 4 2 (O) Both detectors in one or both cavities may be inoperative
provided that the AFT cargo ventilation is closed.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Life animal not allowed to be on associated cargo.
DURING COCKPIT PREPARATION
AFT ISOL VALVE pb-sw . . . . . . . . . . . . . . . . . . . . OFF
26-16-02E Check of liner
integrity
B 4 0 (O) Both detectors in one or both cavities may be inoperative
provided that:
1) The liner integrity in the AFT and the BULK cargocompartments is checked before each flight, and
2) The AFT cargo ventilation is closed.
OPERATING PROCEDURES
Refer to MEL item 26-16-02C
12 FEB 12MEL
A320/321MEL/CDL 01.26.11
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-17 Lavatory Smoke
Detection
26-17-01 Lavatory Smoke
Detection
System
Note:
The lavatory smoke detection function is
part of CIDS Smoke Detection Function
(CIDS-SDF).
Refer to Item 23-73-10-01 Smoke
Detection Function (CIDS-SDF)
26-17-01A Associated
lavatory fire
extinguishing
system
operative
C 3 1 (O) One or two may be inoperative provided that:
1) The associated lavatory fire extinguishing system isoperative, and
2) A procedure is used to periodically check absence of smoke in the associated lavatory.
OPERATING PROCEDURES
PIC request the cabin purser to Ensure that the affected
lavatory is inspected and checked by crewmembers
periodically during flight.
26-17-01B Associated
lavatory not
used
C 3 2 (O)(FD) One may be inoperative provided that:
1) The associated lavatory waste receptacle is empty,and
2) The associated lavatory door is locked closed andplacarded inoperative, and
3) The lavatory is not used for storage or for any other purpose, and
4) A procedure is used to periodically check the absenceof smoke in the associated lavatory.
5) Refer to the NOTE in Operating Procedure
(Cont’d on next page)
01.26.12FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-17 Lavatory Smoke
Detection
26-17-01 Lavatory Smoke
Detection
System
26-17-01B Associated
lavatory not
used (cont’d)
OPERATING PROCEDURES
The associated lavatory is periodacally checked for the
absence of smoke by crewmembers.
NOTE:
In case foreword lavatory placarded
extra pilot should be assigned to
operate the flight as a safety pilot to
relieve the pilot when leaving the cockpit
for personal reasons.
26-22 APU Fire
Extinguishing
26-22-01 APU Automatic
Fire
Extinguishing
Control on
Ground
26-22-01A APU operations
on ground
monitored
C 1 0 May be inoperative provided that the APU condition is
continuously monitored in the cockpit during APU
operations on ground .
12 FEB 12MEL
A320/321MEL/CDL 01.26.13
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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26 FIRE PROTECTION
26-22 APU Fire
Extinguishing
26-22-02 APU Fire
Extinguisher
Overpressure
Indication (Red
Disc)
26-22-02A APU Fire
extinguisher
bottle pressure
switch operative
C 1 0 (M) May be damaged or missing provided that the APU fire
extinguisher bottle pressure switch is checked operative
before the fist flight of each day.
MAINTENANCE PROCEDURE
Refer to AMM 26-22-00-040-007
26-22-02B APU
deactivated
C 1 0 (M) May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
01.26.14FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-22 APU Fire
Extinguishing
26-22-03 Squib of the
APU Fire
Extinguisher
Bottle
26-22-03A One
inoperative
C 2 1 (M) One may be inoperative provided that the remaining squib
is checked operative before the fist flight of each day.
MAINTENANCE PROCEDURE
Refer to AMM 26-22-00-040-008
26-22-03B Both
inoperative
C 2 0 (M) Both m ay b e inoperative p rovided t hat t he A PU i s
deactivated.
Refer to Item 49-10-01C Power Plant (APU)
26-22-04 APU Fire
Extinguisher
Bottle
26-22-04A C 1 0 (M) May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)
12 FEB 12MEL
A320/321MEL/CDL 01.26.15
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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26 FIRE PROTECTION
26-22 APU Fire
Extinguishing
26-22-05 APU AUTO
EXTING TEST
pb-sw on the
Maintenance
Panel
26-22-05A C 1 0 May be inoperative provided that the APU automatic fire
extinguishing control on ground is considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing
Control on Ground
26-22-06 APU FIRE light
on the External
Power Panel
26-22-06A APU Automatic
fire
extinguishing
control on
ground
operative
C 1 0 (M) May be inoperative provided that the APU automatic fire
extinguishing control on ground is checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 26-22-00-040-010
26-22-06B APU Automatic
fire
extinguishing
control on
ground
considered
inoperative
C 1 0 May be inoperative provided that the APU automatic fire
extinguishing control on ground is considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground
01.26.16FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-22 APU Fire
Extinguishing
26-22-07 APU SHUT OFF
pb on the
External Power
Panel
26-22-07A APU Automatic
fire
extinguishing
control on
ground
operative
C 1 0 (M) May be inoperative provided that the APU automatic fire
extinguishing control on ground is checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 26-22-00-040-011
26-22-07B APU Automatic
fire
extinguishing
control on
ground
considered
inoperative
C 1 0 May be inoperative provided that the APU automatic fire
extinguishing control on ground is considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground
26-23 Cargo
Compartment Fire
Extinguishing
26-23-01 Cargo Agent
Bottle
Note:
The cargo smoke detection function is
part of CIDS Smoke Detection Function
(CIDS-SDF).
Refer to Item 23-73-10-01 Smoke
Detection Function (CIDS-SDF)
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.26.17
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-23 Cargo Compartment
Fire Extinguishing
26-23-01 Cargo Agent
Bottle (cont’d)
26-23-01A No flammable
or combustible
materials
C 1 0 (O)(FD) May be inoperative provided that the cargo compartments
are empty or do not contain flammable or combustible
materials.
OPERATING PROCEDURES
Ramp Load Control Supervisor to physically check and
confirm to the flight crew that cargo compartment(s) are
either empty or only contain empty cargo containers,
pallets, cargo restraint components.
01.26.18FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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26 FIRE PROTECTION
26-23 Cargo
Compartment Fire
Extinguishing
26-23-02 Squib of the
Cargo Bottle 1
26-23-02A No flammable
or combustible
materials
C 2 0 (O)(FD) O ne or both may be inoperative provided that the
associated cargo compartment is empty or does not
contain flammable or combustible materials.
OPERATING PROCEDURES
Ramp Load Control Supervisor to physically check and
confirm to the flight crew that cargo compartment(s) are
either empty or only contain empty carfo containers,
pallets, cargo restraint components.
26-24-01 Portable Fire
Extinguisher
26-24-01A C 4 3 One may be inoperative in the cabin or missing provided:
1) Inoperative fire extinguisher is tagged inoperative,removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit, and
2 ) Required distribution is maintained.
Note:
The fire extnguisher located in the
cockpit must always be operative.
12 FEB 12MEL
A320/321MEL/CDL 01.26.19
FIRE PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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26 FIRE PROTECTION
26-24 Portable Fire
Extinguisher
26-25 Lavatory Fire
Extinguishing
26-25-01 Lavatory Waste
Bin Fire
Extinguishing
System
26-25-01A C 3 0 One or more may be inoperative provided associated
lavatory smoke detection system is operative.
26-25-01B C 3 2 (O)(M)
(FD)
One may be inoperative provided:
1) Lavatory waste receptacle is emty,
2) Lavatory door is locked closed and placarded "
"INOPERATVIE DONT ENTER", and
3) lavatory is used only by crewmembers.
4) Refer to the NOTE in Operating Procedure.
NOTE:
These provisos are not intented to
prohibit lavatory use or inspection by
crewmembers.
OPERATING PROCEDUERS
Ensure that the affected lavatory is kept locked and is not
entered except for inspection by crewmembers.
NOTE:
In case foreword lavatory placarded extra pilot should be
assigned to operate the flight as a safety pilot to relieve
the pilot when leaving the cockpit for personal reasons.
* * *
01.26.20FIRE PROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-00 MAINTENANCE
Messages on the
STATUS SD page
27-00-01 F/CTL
MAINTENANCE
Message
27-00-01A C 1 - F/CTL MAINTENANCE message may be displayed on the
STATUS SD page.
27-00-02 SFCS
MAINTENANCE
Message
27-00-02A C 1 - SFCS MAINTENANCE message may be displayed on the
STATUS SD page.
27-01 Overhead Panels
27-01-01 FLT CTL
Overhead Panel
27-01-01-01 ELAC pb-sw
FAULT light
27-01-01-01A C 2 1 One may be inoperative.
27-01-01-02 ELAC pb-sw
OFF light
27-01-01-02A C 2 0 One or both may be inoperative.
27-01-01-03 SEC pb-sw
FAULT light
27-01-01-03A C 3 2 One may be inoperative.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.27.01
FLIGHT CONTROLS
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27 FLIGHT CONTROLS
27-01 Overhead Panels
27-01-01 FLT CTL
Overhead Panel
27-01-01-04 SEC pb-sw OFF
light
27-01-01-04A C 3 0 One or more may be inoperative.
27-07 Indications on SD
pages
27-07-01 Aileron Actuator
Indication on the
F/CTL SD page
27-07-01A C 4 0 One or more may be inoperative.
27-07-02 Aileron Position
Indication on the
F/CTL SD page
27-07-02A C 2 1 (O)(FD) One may be inoperative provided that the deflection of the
affected aileron through each servo-control is visually
checked before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic System
with:- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
(Cont’d on next page)
01.27.02FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-02 Aileron Position
Indication on the
F/CTL SD page
27-07-02A (Cont’d) OPERATING PROCEDURES(Cont’d)
- Replace any action on the YELLOW
ELEC PUMP pb-sw by a similar action on the Ground Cart or on the
YELLOW ENG 2 PUMP pb-sw in the
following procedure.
Check of the aileron control through the ELACs:
Put the aircraft in the test configuration:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON
- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
Check of the aileron control through the ELAC 1:
- Move the CAPT stick from right stop to left stop.
- Visually check the full travel of the ailerons.
CAUTION
If the expected aileron movement does
not occur, do not attempt any reset.
Contact the maintenance.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.27.03
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-02 Aileron Position
Indication on the
F/CTL SD page
27-07-02A (Cont’d) OPERATING PROCEDURES(Cont’d)
Check of the aileron control through the ELAC 2:
- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- Move the CAPT stick from right stop to left stop,then from forward stop to aft stop.
- Visually check the full travel of the ailerons.
CAUTION
If the expected aileron movement does
not occur, do not attempt any reset.
Contact the maintenance.
Return to normal configuration:- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . Off
- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
27-07-03 Elevator
Actuator
Indication on the
F/CTL SD page
27-07-03A C 4 0 One or more may be inoperative.
01.27.04FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-04 Elevator
Position
Indication on the
F/CTL SD page
27-07-04A C 2 1 (O) One may be inoperative provided that the deflection of the
affected elevator is visually checked before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic
System with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.- Replace any action on the YELLOW
ELEC PUMP pb-sw by a similar
action on the Ground Cart or on the
YELLOW ENG 2 PUMP pb-sw in the
following procedure.
Check of the elevator control:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.27.05
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-04 Elevator
Position
Indication on the
F/CTL SD page
27-07-04A (Cont’d) OPERATING PROCEDURES (Cont’d)
- Establish communication with the ground crew.
- Move the CAPT or the F/O stick to the maximumnose down position.
- Visually check that both elevators move down.
- Move the CAPT or the F/O stick to the maximumnose up position.
- Visually check that both elevators move up.
- Move the CAPT or the F/O stick to the neutralposition.
- Visually check that both elevators go back to the
neutral position.- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . Off
27-07-05 Pitch Trim
Position
Indication on the
F/CTL SD page
27-07-05A C 1 0 (O) May be inoperative provided that the pitch trim handwheel
and the stabilizer are visually checked to synchronously
operate before each flight.
(Cont’d on next page)
01.27.06FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-05 Pitch Trim
Position
Indication on the
F/CTL SD page
27-07-05A (Cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic
System with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW
ELEC PUMP pb-sw by a similar
action on the Ground Cart or on the
YELLOW ENG 2 PUMP pb-sw in the
following procedure.
Check of the stabilizer control:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- Establish communication with the ground crew.
- Move the pitch trim handwheel to the full DNposition.
- Visually check that the stabilizer moves to the fulldown position.
- Move the pitch trim handwheel to the full UPposition.
- Visually check that the stabilizer moves to the fullup position.
- Move the pitch trim handwheel to the requiredposition.
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
12 FEB 12MEL
A320/321MEL/CDL 01.27.07
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-06 Rudder Position
Indication on the
F/CTL SD page
27-07-06A B 1 0 (O) May be inoperative provided that the deflection of the
rudder is visually checked before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic System
with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW ELECPUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2
PUMP pb-sw in the following procedure.
Check of the rudder control:
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- Establish communication with the ground crew.
- On the CAPT or the F/O side, apply left rudder.
- Visually check that the rudder moves to the left.
- On the CAPT or the F/O side, apply right rudder.- Visually check that the rudder moves to the right.
- On the CAPT or the F/O side, release the pedals.
- Visually check that the rudder moves to the neutralposition.
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
01.27.08FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-07 Rudder Trim
Position
Indication on the
F/CTL SD page
27-07-07A Rudder trim
position
indication
operative on the
center pedestal
C 1 0 May be inoperative provided that the rudder trim position
indication is operative on the center pedestal .
27-07-07B Rudder position
checked at zero
C 1 0 May be inoperative provided that the rudder position is
checked at zero on the F/CTL SD page before takeoff.
27-07-08 Rudder Travel
Limiter Position
Indication on the
F/CTL SD page
27-07-08A C 1 0 May be inoperative.
27-07-09 ELAC Indication
on the F/CTL SD
page
27-07-09A C 2 1 One may be inoperative.
27-07-10 SEC Indication
on the F/CTL SD
page
27-07-10A C 3 0 One or more may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.27.09
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-11 Spoilers/
Speedbrakes
Indication on
the F/CTL SD
page
27-07-11A C 10 0 (O) One or more may be inoperative provided that the
deflection of the affected surface is visually checked
before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic System
with:
- A Ground cart, or with- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW ELEC
PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2
PUMP pb-sw in the following procedure.
- If surface 1 indication is inoperative:
CAUTION
The aircraft must be stopped during the
check.
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- SPEEDBRAKES lever . . . . . . . . . . . . . . . . . . FULL
- Visually check that surface 1 slightly extends
(approximately 6°).
(Cont’d on next page)
01.27.10FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-11 Spoilers/
Speedbrakes
Indication on
the F/CTL SD
page
27-07-11A (Cont’d) OPERATING PROCEDURES(Cont’d)
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . Off
- If surface 3 indication is inoperative:
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON
- Move the stick from left stop to right stop.
- Visually check the correct movement of surface 3.
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off
- If surface 2, 4, or 5 indication is inoperative:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- Move the stick from left stop to right stop andvisually check the correct movement of surfaces 2,4 and 5.
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
27-07-12 Spoilers/
Speedbrakes
Indication on the
WHEEL SD page
27-07-12A C 10 0 (O) One or more may be inoperative provided that thedeflection of the affected surface is visually checked
before each flight.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.27.11
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-12 Spoilers/
Speedbrakes
Indication on the
WHEEL SD page
27-07-12A (Cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic System
with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW ELEC
PUMP pb-sw by a similar action on theGround Cart or on the YELLOW ENG 2
PUMP pb-sw in the following procedure.
- If surface 1 indication is inoperative:
CAUTION
The aircraft must be stopped during the
check.
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- SPEEDBRAKES lever . . . . . . . . . . . . . . . . . . FULL
- Visually check that surface 1 slightly extends
(approximately 6°).
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off
(Cont’d on next page)
01.27.12FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-07 Indications on SD
pages
27-07-12 Spoilers/
Speedbrakes
Indication on the
WHEEL SD page
27-07-12A (Cont’d) OPERATING PROCEDURES(Cont’d)
- If surface 3 indication is inoperative:
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON
- Move the stick from left stop to right stop.
- Visually check the correct movement of surface 3.
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off
- If surface 2, 4, or 5 indication is inoperative:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- Move the stick from left stop to right stop andvisually check the correct movement of surfaces 2,4 and 5.
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
27-08 Indications on the
EWD
27-08-01 Flap Position
Indication on the
EWD
27-08-01A 1 1 Must be operative.
27-08-02 Slat Position
Indication on the
EWD
27-08-02A 1 1 Must be operative.
12 FEB 12MEL
A320/321MEL/CDL 01.27.13
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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27 FLIGHT CONTROLS
27-14 Aileron and Hydraulic
Actuation
27-14-01 Left Aileron Blue
Servo-Control
(Controlled by
ELAC 1)
27-14-01A A 1 0 (O)(M) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulicallysupplied (damping function is not affected), and
3) The left aileron green servo-control (controlled byELAC 2) is operative, and
4) The right aileron blue servo-control (controlled byELAC 2) is operative, and
5) All roll spoilers are operative, and
6) The TR 1 and TR 2 are operative, and
7) The DC TIE contactor 1PC1 is checked closed, and
8) Repaire with in three flight days.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check that DC TIE contactor 1 is closed:
- Supply the electrical network from the APU or theexternal power.
- On the ELEC SD page, check the link between theDC BUS 1 and the DC BAT BUS.
MAINTENANCE PROCEDURE
Refer to AMM 27-14-00-040-001
01.27.14FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-14 Aileron and
Hydraulic
Actuation
27-14-02 Left Aileron
Green Servo-
Control
(Controlled by
ELAC 2)
27-14-02A C 1 0 (M) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulicallysupplied (damping function is not affected), and
3) All roll spoilers are operative.
MAINTENANCE PROCEDURE
Refer to AMM 27-14-00-040-001
27-14-03 Right Aileron
Green Servo-
Control
(Controlled by
ELAC 1)
27-14-03A A 1 0 (O)(M) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulicallysupplied (damping function is not affected), and
3) The right aileron blue servo-control (controlled byELAC 2) is operative, and
4) The left aileron green servo-control (controlled by
ELAC 2) is operative, and
5) All roll spoilers are operative, and
6) The TR 1 and TR 2 are operative, and
7) The DC TIE contactor 1PC1 is checked closed, and
8) Repaire with in three flight days.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.27.15
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-14 Aileron and Hydraulic
Actuation
27-14-03 Right Aileron
Green Servo-
Control
(Controlled by
ELAC 1)
27-14-03A (Cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check that DC TIE contactor 1 is closed:
- Supply the electrical network from the APU or theexternal power.
- On the ELEC SD page, check the link between the DCBUS 1 and the DC BAT BUS.
MAINTENANCE PROCEDURE
Refer to AMM 27-14-00-040-001
27-14-04 Right Aileron
Blue Servo-
Control
(Controlled by
ELAC 2)
27-14-04A C 1 0 (M) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulicallysupplied (damping function is not affected), and
3) All roll spoilers are operative.
MAINTENANCE PROCEDURE
Refer to AMM 27-14-00-040-001
01.27.16FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-21 Rudder
Mechanical
Control
27-21-01 Rudder Pedal
Adjustment
System
27-21-01A C 2 1 (O) One may be inoperative provided that:
1) The rudder pedals can be secured in a position whichmeets individual pilot requirements, and
2) The full and unrestricted movement of the rudder pedals and brake pedals deflection is possible at bothpilot stations.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Simultaneously apply loads on both pedals (in rudder
control movement direction) to make sure that the secured
position is reached. For that purpose, the effort shall be
equivalent to a full rudder deflection.
27-22 Rudder Trim
Actuation
27-22-01 Rudder Trim
System
27-22-01A Rudder trim
system 1
inoperative
C 2 1 (O) Rudder Trim System 1 may be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
27-22-01B Rudder trim
system 2
inoperative
C 2 1 (O) Rudder Trim System 2 may be inoperative.
OPERATING PROCEDURES
Refer to MEL item 27-22-01A
12 FEB 12MEL
A320/321MEL/CDL 01.27.17
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-22 Rudder Trim
Actuation
27-22-02 Manual Rudder
Trim Reset
Function
27-22-02A C 1 0 May be inoperative provided that one rudder trim position
indication is operative.
27-22-03 Rudder Trim
Position
Indication on the
Center Pedestal
27-22-03A C 1 0 May be inoperative.
27-23 Artificial feel and
rudder travel limiting
actuation
27-23-01 Rudder Travel
Limiter System(Including
Rudder and
Pedals Travel
Limiter Units)
27-23-01A C 2 1 One may be inoperative.
27-34 Elevator and
Hydraulic Actuation
27-34-01 Elevator Servo-
Control
27-34-01A 4 4 All must be operative.
01.27.18FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-34 Elevator and
Hydraulic
Actuation
27-34-02 Elevator Servo-
Control Position
Transducer
27-34-02A C 4 2 (M) One transducer per servo-control must be operative.
MAINTENANCE PROCEDURE
Refer to AMM 27-34-00-040-001
27-40 Trimmable
Horizontal
Stabilizer (THS)
27-40-01 Stabilizer
Mechanical
Control
27-40-01A 1 1 Must be operative.
27-40-02 Stabilizer
Actuator Electric
Motor
27-40-02A Electric motor 3
inoperative
C 3 2 The stabilizer actuator electrical motor 3 may be
inoperative.
27-40-02-B Electric motor 2
inoperative
C 3 2 The stabilizer actuator electric motor 2 may be inoperative
provided that ELAC 1 pitch channel is considered
inoperative.
Refer to Item 27-93-01 ELAC 1
12 FEB 12MEL
A320/321MEL/CDL 01.27.19
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27-51 Flaps Electrical
Control and
Monitoring
27-51-01 SFCC Flap
Channel
27-51-01A B 2 1 (O)(M) SFCC 2 flap channel may be inoperative provided that:
1) It is deactivated, and
2) The slats and flaps are checked operative on SFCC 1,and
3) The SFCC 1 flap WTB is checked operative beforeeach flight, and
4) All ELACs, SECs, LGCIUs, RAs, FACs and ADIRS areoperative, and
5) The minimum idle on ground is considered inoperative.
Refer to Item 73-20-05 Minimum Idle on Ground
OPERATING PROCEDURES
GENERAL INFORMATION
ENG 2 APPR IDLE ONLY message is displayed onthe STATUS SD page.
FLAPS SLOW message is displayed on the STATUSSD page.
DURING COCKPIT PREPARATION
Disregard and clear the F/CTL FLAP SYS 2 FAULTalert displayed on the EWD.
MAINTENANCE PROCEDURE
Refer to AMM 27-51-00-040-001
01.27.20FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-51 Flaps Electrical
Control and
Monitoring
27-51-02 SFCC Slat
Channel
27-51-02A B 2 1 (O)(M) SFCC 2 slap channel may be inoperative provided that:
1) It is deactivated, and
2) The slats and flaps are checked operative on SFCC 1,and
3) The SFCC 1 slat WTB is checked operative beforeeach flight, and
4) All ELACs, SECs, LGCIUs, RAs, FACs and ADIRS areoperative, and
5) Takeoff is not performed in CONF 1+F.
OPERATING PROCEDURES
GENERAL INFORMATION
SLATS SLOW message is displayed on the STATUS
SD page.
DURING COCKPIT PREPARATION
Disregard and clear the F/CTL SLAT SYS 2 FAULTalert displayed on the EWD.
MAINTENANCE PROCEDUR
Refer to AMM 27-51-00-040-005
27-51-03 Flap Wing Tip
Brakes Solenoid
27-51-03A B 4 2 (M) One or two solenoids associated with the SFCC 2 may beinoperative provided that the SFCC 1 flap WTB is checked
operative before each flight.
MAINTENANCE PROCEDURE
Refer to AMM 27-51-00-040-004
12 FEB 12MEL
A320/321MEL/CDL 01.27.21
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-54 Flaps Hydraulic
Actuation and Power
Transmission
27-54-01 Flap Hydraulic
Motor
27-54-01A Green motor
inoperative
C 2 1 Green motor may be inoperative.
27-54-01B Yellow motor
inoperative
C 2 1 Yellow motor may be inoperative provided that the blue
slat motor is operative.
27-54-02 Flap PCU Valve
Block
27-54-02A B 2 1 The valve block associated with SFCC 2 may be
inoperative provided that the SFCC 2 flap channel is
considered inoperative.
Refer to Item 27-51-01 SFCC Flap Channel
27-54-03 Flap Pressure-
Off Brake
27-54-03A 2 2 Both must be operative.
01.27.22FLIGHT CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-64 Spoiler Hydraulic
Actuation
27-64-01 Spoiler 5
27-64-01A C 2 0 (O)(M) The pair of spoilers 5 may be inoperative provided that:
1) The affected spoiler is deactivated in the retractedposition, and
2) The pairs of spoilers 1, 2, 3, and 4 are operative.
OPERATING PROCEDURES
AFTER ENGINE START
On the HYD SD page, check the absence of amber data.
Note:
No performance penalty applies when
the pair of spoilers 5 is inoperative.
MAINTENANCE PROCEDURE
Refer to AMM 27-64-00-040-001
27-64-02 Spoiler 1 or 3
27-64-02A C 4 2 (O)(M)
(FD)
One pair of spoilers 1 or 3 may be inoperative provided
that:
1) The affected spoiler is deactivated in the retractedposition, and
2) The pairs of spoilers 2, 4, and 5 are operative, and
3) The Flight Manual performance penalties are applied.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
For performance calculations request Modified Tailored
Takeoff and Landing charts (MTTL) from FPE through
Flight Dispatch.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.23
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-64 Spoiler Hydraulic
Actuation
27-64-02 Spoiler 1 or 3
27-64-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
Landing performance computation:
Increase the landing distances by 10 %.
AFTER ENGINE START
On the HYD SD page, check the absence of amber data.
FOR TAKEOFF
Performed the takeoff using full thrust (TOGA).
MAINTENANCE PROCEDURE
Refer to AMM 27-64-00-040-001
01.27.24FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-64 Spoiler Hydraulic
Actuation
27-64-03 Spoiler 2 or 4
27-64-03A C 4 2 (O)(M)(FD)
One pair of spoilers 2 or 4 may be inoperative in theretracted position provided that:
1) The affected spoiler is deactivated in the retractedposition, and
2) The pairs of spoilers 1, 3, and 5 are operative, and
3) The SFCC 2 flap channel is operative, and
4) The Flight Manual performance penalties are applied.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to OperatingProcedures 27-64-02A Spoiler 1 or 3
AFTER ENGINE START
On the HYD SD page, check the absence of amber data.
MAINTENANCE PROCEDURE
Refer to AMM 27-64-00-040-001
30 JUN 12MEL
A320/321MEL/CDL 01.27.25
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-64 Spoiler Hydraulic
Actuation
27-64-04 Spoilers 1 and 2
27-64-04A B 4 0 (O)(M)
(FD)
The pairs of spoilers 1 and 2 may be inoperative in the
retracted position provided that:
1) The affected spoilers are deactivated in the retractedposition, and
2) The pairs of spoilers 3, 4, and 5 are operative, and
3) The SFCC 2 flap channel is operative, and
4) The Flight Manual performance penalties are applied.
OPERATING PROCEDURES (A321)
FLIGHT PREPARATION/LIMITATIONS
For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPEthrough Flight Dispatch.
Landing performance computation:
Increase the landing distances by 5 %.
DURING COCKPIT PREPARATION
- SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
(Cont’d on next page)
01.27.26FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-64 Spoiler Hydraulic
Actuation
27-64-04 Spoilers 1 and 2
27-64-04A (cont’d) OPERATING PROCEDURES (A321) cont’d
FOR TAKEOFF
Performed the takeoff using full thrust (TOGA).
IN FLIGHT
- In the case of further failure of SEC 1 and SEC 2:
- Autoland is not permitted.
- Disengage the AP at 500 ft RA before landing in
direct law. As soon as the AP is disengaged whenthe three SECs are failed, it cannot be engagedagain.
- Maximum landing capability is CAT I
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.27
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-64 Spoiler Hydraulic
Actuation
27-64-04 Spoilers 1 and 2
27-64-04A (cont’d) OPERATING PROCEDURES (A320)
FLIGHT PREPARATION/LIMITATIONS
For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPEthrough Flight Dispatch .
Landing performance computation:
Increase the landing distances by 10 %.
DURING COCKPIT PREPARATION
- SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B
· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
FOR TAKEOFF
Performed the takeoff using full thrust (TOGA).
IN FLIGHT
- In the case of further failure of SEC 1 and SEC 2:
- Autoland is not permitted.
- Disengage the AP at 500 ft RA before landing indirect law. As soon as the AP is disengaged whenthe three SECs are failed, it cannot be engagedagain.
- Maximum landing capability is CAT I
MAINTENANCE PROCEDURE
Refer to AMM 27-64-00-040-001
01.27.28FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27FLIGHT CONTROLS
27-64 Spoiler Hydraulic
Actuation
27-64-05 Spoilers 3 and 4
27-64-05A C 4 0 (O)(M)
(FD)
The pairs of spoilers 3 and 4 may be inoperative in the
retracted position provided that:
1) The affected spoilers are deactivated in the retractedposition, and
2) The pairs of spoilers 1, 2, and 5 are operative, and
3) The TR 1 and TR 2 are operative, and
4) The DC TIE contactor 1PC1 is checked closed, and
5) The SFCC 2 flap channel is operative, and
6) The Flight Manual performance penalties are applied.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
For performance penalties Refer to OperatingProcedures 27-64-04A Spoilers 1 and 2
DURING COCKPIT PREPARATION
Check that the DC TIE contactor 1 is closed:
- Supply the electrical network from the APU or theexternal power.
- On the ELEC SD page, check the link between theDC BUS 1 and the DC BAT BUS.
IN FLIGHT
Do not use the speedbrakes.
MAINTENANCE PROCEDURE
Refer to AMM 27-64-00-040-001
30 JUN 12MEL
A320/321MEL/CDL 01.27.29
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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.27 FLIGHT CONTROLS
27-81 Slats Electrical
Control and
Monitoring
27-81-01 Slat Wing Tip
Brakes
Solenoids
27-81-01A C 4 2 (M) One or two solenoids associated with the SFCC 2 may be
inoperative provided that the SFCC 1 slat WTB is checked
operative before each flight.
MAINTENANCE PROCEDURE
Refer to AMM 27-81-00-040-001
27-84 Slats Hydraulic
Actuation and Power
Transmission
27-84-01 Slats Hydraulic
Motor
27-84-01A C 2 1 One may be inoperative.
27-84-02 Slat PCU Valve
Block
27-84-02A C 2 1 The valve block associated with SFCC 2 may be
inoperative provided that the SFCC 2 slat channel is
considered inoperative.
Refer to MEL Item 27-51-02 SFCC Slat Channel
27-84-03 Slat Pressure-
Off Brake
27-84-03A 2 2 Both must be operative.
01.27.30FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-92 Electrical Flight
Control System
(EFCS) Control
Inputs and Power
Supply
27-92-01 Speedbrake
Control System
27-92-01B Speedbrake 2
or speedbrakes
3 and 4
inoperative
B 1 1 (O)(FD) Speedbrake 2 or speedbrakes 3 and 4 may be inoperative
provided that the Flight Manual performance penalties
associated with one or two pairs of spoilers inoperative are
applied.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
- If speedbrake n° 2 is inoperative: Apply performance penalties associated with the pair of spoilers 2 inoperative.Refer to Operating Procedures 27-64-03A Spoiler 2 or 4
- If speedbrakes n° 3 and n° 4 are inoperative: Apply performance penalties associated with two pairsof spoilers inoperative.Refer to Operating Procedures 27-64-04A Spoilers 1and 2
IN FLIGHT
- If speedbrakes n° 3 and n° 4 are inoperative:Do not use the speedbrakes.
30 JUN 12MEL
A320/321MEL/CDL 01.27.31
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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27 FLIGHT CONTROLS
27-92 Electrical Flight
Control System
(EFCS) Control Inputs
and Power Supply
27-92-02 Ground Spoiler
Control System
27-92-02A Ground spoiler
control system
inoperative
A 1 0 (O)(FD) May be inoperative provided that:
1) Both thrust reversers are not taken into account for performance computation, and
2) The autobrake function is not used, and
3) The Flight Manual performance penalties are applied,and
4) Repair must be made within three flight legs.
OPERATING PROCEDURES (A321)
GENERAL INFORMATION
The autobrake function is not available.
Refer to Operating Procedures 32-42-05A AUTO/BRK Function
CAUTION
One or both thrust reversers may not
deploy at landing. Consequently, for
performance determination, do not take
into account the credit of the thrust
reversers.
FLIGHT PREPARATION/LIMITATIONS
For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPE
through Flight Dispatch.
Landing performance computation:
Increase the landing distances by 20 %.
FOR TAKEOFF
Performed the takeoff using full thrust (TOGA).
(Cont’d on next page)
01.27.32FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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27 FLIGHT CONTROLS
27-92 Electrical Flight
Control System
(EFCS) Control
Inputs and Power
Supply
27-92-02 Ground Spoiler
Control System
27-92-02A (Cont’d) OPERATING PROCEDURES (A320)
GENERAL INFORMATION
The autobrake function is not available.
Refer to Operating Procedures 32-42-05A AUTO/BRK Function
CAUTION
One or both thrust reversers may not
deploy at landing. Consequently, for
performance determination, do not takeinto account the credit of the thrust
reversers.
FLIGHT PREPARATION/LIMITATIONS
For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPEthrough Flight Dispatch .
Landing performance computation:
Increase the landing distances by 35 %.
FOR TAKEOFF
Performed the takeoff using full thrust (TOGA).
30 JUN 12MEL
A320/321MEL/CDL 01.27.33
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-92 Electrical Flight
Control System
(EFCS) Control Inputs
and Power Supply
27-92-02 Ground Spoiler
Control System
27-92-02B Spoilers 5
inoperative
C 1 1 (O) The pair of spoilers 5 may be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to Operating Procedures
27-64-01A Spoiler 5
27-92-02C Spoilers 1 and
2, or spoilers 3
and 4
inoperative
C 1 1 (O) The pairs of spoilers 1 and 2 or the pairs of spoilers 3 and
4 may be inoperative provided that the Flight Manual
performance penalties are applied.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
- If the pairs of spoilers 1 and 2 are inoperative:
For performance penalties, Refer to OperatingProcedures 27-64-04A Spoilers 1 and 2
- If the pairs of spoilers 3 and 4 are inoperative:
For performance penalties, Refer to OperatingProcedures 27-64-05A Spoilers 3 and 4
27-92-03 SIDESTICK
PRIORITY light
27-92-03A 4 4 All must be operative.
01.27.34FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-92 Electrical Flight
Control System
(EFCS) Control
Inputs and Power
Supply
27-92-04 Sidestick Dual
Input Visual
Warnings
27-92-04A C 2 1 One may be inoperative.
27-92-05 Sidestick Dual
Input Aural
Warning
27-92-05A C 1 0 May be inoperative.
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A B 1 0 (O)(M)
(FD)
ELAC 1 or any ELAC 1 function may be inoperative
provided that:
1) All SECs, SFCCs, LGCIUs, RAs, ADIRS and FACsare operative, and
2) The pairs of spoilers 2, 3, 4, and 5 are operative, and
3) The TR 1 and the TR 2 are operative, and
4) Both accelerometers associated with the ELAC 2 arechecked operative before each flight, and
5) All sidesticks transducers associated with the ELAC 2
and the three SECs are checked operative beforeeach flight, and
6) The DC TIE contactor 1PC1 is checked closed, beforeeach flight, and
7) The elevators and roll spoilers control is checkedoperative through the SECs before each flight.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.35
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) Note:
F/O take-over pb cannot disengage
AP1.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
If the AP 1 is engaged for landing: Maximum landingcapability is CAT I.
If the AP 2 is engaged for landing: Landing capabilityis CAT II.
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic System
with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW ELEC
PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2
PUMP pb-sw in the following procedure.
- If the F/CTL ELAC 1 FAULT alert is displayed on the
EWD:
(Cont’d on next page)
01.27.36FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
Note:
i. After application of the maintenanceprocedure, the following ECAM
alerts remain displayed on the EWD:
- C/B TRIPPED R ELEC BAY
alert , and
- C/B TRIPPED ON OVHD PNL
alert, and
- F/CTL ELAC 1 FAULT alert.
ii. After first engine start, the F/CTL
ALTN LAW alert may be spuriously
displayed. It normally disappears
after second engine start.
Check of the elevator and the roll spoilers control throughthe SECs:
Put the aircraft in the test configuration:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
Note:
If the Yellow Electric Pump is not
available, pressurize the Yellow
Hydraulic System with a Ground Cart or
with the Yellow Engine 2 Pump with the
Engine 2 running.
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.37
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
- SEC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- SEC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- Wait 5 s
Check of the elevator control through the SEC 1 and the
spoilers control through the secretary 1 and the SEC 3:
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuit depressurization.
- On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
- Wait 5 s
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
(Cont’d on next page)
01.27.38FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
CAUTION
If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Check of the elevator control through the SEC 2 and of the
spoilers control through the SEC 2 and the SEC 3:
- ELAC 1 & 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Wait 5 s
- YELLOW ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuits depressurization.
- On the F/CTL SD page, check that the yellow and thegreen elevator actuators symbols become amber.
- Wait 5 s
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2 and 5 and the full travel of both elevators.
- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2 and 5 and the full travel of both elevators.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.39
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
CAUTION
If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Return to normal configuration:
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · OFF
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · OFF
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
Check that the DC TIE contactor 1 is closed:
- Supply the electrical network from the APU or theexternal power.
- On the ELEC SD page, check the link between theDC BUS 1 and the DC BAT BUS.
- If the F/CTL ELAC 1 PITCH FAULT alert is displayedon the EWD:
Note:
After first engine start:
- The F/CTL ALTN LAW alert may bespuriously displayed on the EWD. It
normally disappears after few seconds when
ELAC 2 auto test is accomplished.
(Cont’d on next page)
01.27.40FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
Check of the elevator and the roll spoilers control through
the SECs:
Put the aircraft in the test configuration:
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
- BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · AUTO
- BLUE PUMP OVRD pb · · · · · · · · · · · · · · · · · · · · · · ON
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On- SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Wait 5 s
Check of the elevator control through the SEC 1 and of the
spoilers control through the SEC 1 and the SEC 3:
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuit depressurization.
- On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
- Wait 5 sincerely- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.41
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
CAUTION
If an expected spoiler or elevator
movement does not occur, do not
attempt any reset.
Contact the maintenance.
Check of the elevator control through the SEC 2 and of the
spoilers control through the SEC 2 and the SEC 3:
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Wait 5 s
- YELLOW ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuits depressurization.
- On the F/CTL SD page, check that the yellow and thegreen elevator actuators symbols become amber.
- Wait 5 s
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
(Cont’d on next page)
01.27.42FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2 and 5 and the full travel of both elevators.
- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2 and 5 and the full travel of both elevators.
CAUTIONIf an expected spoiler or elevator
movement does not occur, do not
attempt any reset.
Contact the maintenance.
Return to normal configuration:
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.43
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-01 ELAC 1
27-93-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
Check that the DC TIE contactor 1 is closed:
- Supply the electrical network from the APU or theexternal power.
- On the ELEC SD page, check the link between the DCBUS 1 and the DC BAT BUS.
BEFORE ENGINE START
- AP 1 pb · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- CAPT take-over pb · · · · · · · · · · · · · · · · · · · · · · · Press
- Check that the AP OFF message is displayed on theEWD.
Note:
Due to the fact that the ELAC 1 is not
electrically supplied, the F/O take-over
pb cannot disengage the AP 1.
IN APPROACH
- If the AP 1 is used for the approach:
The captain must be the PF.
MAINTENANCE PROCEDURE
Refer to AMM 27-93-00-040-001
27-93-02 ELAC 2
27-93-02A 1 1 Must be operative.
01.27.44FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-93 ELAC System
(Elevator Aileron
Computer)
27-93-03 Pitch Normal
Law
27-93-03A 1 1 Must be operative.
27-94 SEC System
(Spoiler and
Elevator
Computer)
27-94-01 SEC 1
27-94-01A B 1 0 (O)(M)
(FD)
May be inoperative provided that:
1) It is deactivated, and
2) The SEC 2 and the SEC 3 are operative, and
3) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRSare operative, and
4) The SFCC 2 flap channel is operative, and
5) All aileron servo-controls associated with the operativeSECs are operative, and
6) The TR 1 and TR 2 are operative, and
7) The sidestick transducers associated with the ELACsand the operative SECs are checked operative beforeeach flight, and
8) The DC TIE contactor 1PC1 is checked closed, beforeeach flight, and
9) The elevators control through the SEC 2 and theELACs and the roll spoilers control through the
operative SECs are checked operative before eachflight, and
10) The Flight Manual performance penalties for the pairsof spoilers 3 and 4 inoperative are applied.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.45
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-94 SEC System (Spoiler
and Elevator
Computer)
27-94-01 SEC 1
27-94-01A (Cont’d) OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to OperatingProcedures 27-64-05A Spoilers 3 and 4
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic System
with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW ELEC
PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2
PUMP pb-sw in the following procedure.
Note:
After application of the maintenance
procedure, the C/B TRIPPED R ELEC
BAY and the C/B TRIPPED ON OVHD
PNL alerts are displayed on the EWD.
(Cont’d on next page)
01.27.46FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-94 SEC System
(Spoiler and
Elevator
Computer)
27-94-01 SEC 1
27-94-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
Check of the elevator control through the operative
computers:
Put the aircraft in the test configuration:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON
- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- SEC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- Wait 5 s
Check of the elevator control through the ELAC 1:
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuit depressurization.
- On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
- Wait 5 s
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- Move the CAPT stick from forward stop to aft stop.
- On the F/CTL SD page, check the full travel of bothelevators.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.47
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROLS
27-94 SEC System (Spoiler
and Elevator
Computer)
27-94-01 SEC 1
27-94-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
CAUTION
If an expected elevator movement doesnot occur, do not attempt any reset.
Contact the maintenance.
Check of the elevator control through the SEC 2:
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Wait 5 s
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuits depressurization.
- On the F/CTL SD page, check that the yellow and thegreen elevator actuators symbols become amber.
- Wait 5 s
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.Each stop must be applied during 3 s
- On the F/CTL SD page, check the correct movement
of the pairs of spoilers 2 and 5 and the full travel of both elevators.
- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.Each stop must be applied during 3 s
(Cont’d on next page)
01.27.48FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System
(Spoiler and
Elevator
Computer)
27-94-01 SEC 1
27-94-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
- On the F/CTL SD page, check the correct movement
of the pairs of spoilers 2 and 5 and the full travel of both elevators.
CAUTION
If an expected spoiler or elevator
movement does not occur, do not
attempt any reset.
Contact the maintenance.
Return to normal configuration:
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off
- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
Check that the DC TIE contactor 1 is closed:
- Supply the electrical network from the APU or theexternal power.
- On the ELEC SD page, check the link between the DCBUS 1 and the DC BAT BUS.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.49
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System (Spoiler
and Elevator
Computer)
27-94-01 SEC 1
27-94-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
IN FLIGHT
Do not use the speedbrakes.
- If the SEC 2 and the SEC 3 fail during the flight:
Autoland is not permitted.
Maximum landing capability is CAT I
Disengage the AP at 500 ft RA before landing in directlaw.
When the AP is disengaged with the three SECsfailed, it cannot be engaged again.
MAINTENANCE PROCEDURE
Refer to AMM 27-94-00-040-002
01.27.50FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System
(Spoiler and
Elevator
Computer)
27-94-02 SEC 2
27-94-02A B 1 0 (O)(M) May be inoperative provided that:
1) It is deactivated, and
2) The SEC 1 and the SEC 3 are operative, and
3) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRSare operative, and
4) All aileron servo-controls and roll spoilers associatedwith the operative SECs are operative, and
5) The sidestick transducers associated with the ELACsand the operative SECs are checked operative beforeeach flight, and
6) The elevators control through the SEC 1 and theELACs and the roll spoilers control through theoperative SECs are checked operative before each
flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic
System with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW
ELEC PUMP pb-sw by a similar
action on the Ground Cart or on the
YELLOW ENG 2 PUMP pb-sw in the
following procedure.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.51
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System (Spoiler
and Elevator
Computer)
27-94-02 SEC 2
27-94-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
Note:
After application of the maintenanceprocedure, the C/B TRIPPED REAR
PNL N-R alert is displayed on the EWD.
Check of the elevator control through the operative
computers:
Put the aircraft in the test configuration:
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb. . . . . . . . . . . . . . . . . . . ON
- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
- SEC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
- Wait 5 s
Check of the elevator control through the ELAC 1:
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuit depressurization.
- On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
- Wait 5 s
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
(Cont’d on next page)
01.27.52FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System
(Spoiler and
Elevator
Computer)
27-94-02 SEC 2
27-94-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- Move the CAPT stick from forward stop to aft stop.
- On the F/CTL SD page, check the full travel of bothelevators.
CAUTION
If an expected elevator movement does
not occur, do not attempt any reset.
Contact the maintenance.
Check of the elevator control through the SEC 1:
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- Wait 5 s
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
- Wait for hydraulic circuits depressurization.
- On the F/CTL SD page, check that the blue elevator actuator symbols becomes amber.
- Wait 5 s
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.Each stop must be applied during 3 s
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.53
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System (Spoiler
and Elevator
Computer)
27-94-02 SEC 2
27-94-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.
Each stop must be applied during 3 s
- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
CAUTION
If an expected spoiler or elevator
movement does not occur, do not
attempt any reset.
Contact the maintenance.
Return to normal configuration:
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
AFTER ENGINE START
Note:
The F/CTL ELEV SERVO FAULT alert
may be displayed on the EWD if the
PTU is inhibited and only one engine is
operating. This alert must disappear when the PTU or the second engine is
started.
(Cont’d on next page)
01.27.54FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System
(Spoiler and
Elevator
Computer)
27-94-02 SEC 2
27-94-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
IN FLIGHT
- If the SEC 1 and the SEC 3 fail during the flight:
Autoland is not permitted.
Maximum landing capability is CAT I
Disengage the AP at 500 ft RA before landing in direct law.
When the AP is disengaged with the three SECs failed, it
cannot be engaged again.
MAINTENANCE PROCEDURE
Refer to AMM 27-94-00-040-002
27-94-03 SEC 3
27-94-03A C 1 0 (O) May be inoperative provided that:
1) The SEC 1 and SEC 2 are operative, and
2) The SFCC 2 flap channel is operative, and
3) All aileron servo-controls and roll spoilers associatedwith the operative SECs are operative, and
4) The Flight Manual performance penalties for the pairsof spoilers 1 and 2 inoperative are applied.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.27.55
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System (Spoiler
and Elevator
Computer)
27-94-03 SEC 3
27-94-03A (cont’d) OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to OperatingProcedures 27-64-04A Spoilers 1 and 2
DURING COCKPIT PREPARATION
Deactivation of the SEC 3:
- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- FLIGHT CONTROLS/SEC 3/SPLY (121VU Q19)C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
IN FLIGHT
- If the SEC 1 and the SEC 2 fail during the flight:
Autoland is not permitted.
Maximum landing capability is CAT I
Disengage the AP at 500 ft RA before landing in directlaw.
When the AP is disengaged with the three SECsfailed, it cannot be engaged again.
01.27.56FLIGHT CONTROLS
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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27 FLIGHT CONTROLS
27-94 SEC System
(Spoiler and
Elevator
Computer)
27-95-01 FCDC 1
27-95-01A 1 1 Must be operative.
27-95-02 FCDC 2
27-95-02A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
FLIGHT CONTROLS/FCDC2/SPLY (121VU Q20) C/B· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
* * *
30 JUN 12MEL
A320/321MEL/CDL 01.27.57
FLIGHT CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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01.27.58FLIGHT CONTROLS
A320/321MEL/CDL
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-00 MAINTENANCE
Message on the
STATUS SD page
28-00-01 FUEL
MAINTENANCE
Message
28-00-01A C 1 - FUEL MAINTENANCE message may be displayed on the
STATUS SD page.
28-01 Overhead Panels
28-01-01 FUEL Overhead
Panel
28-01-01-01 Wing TK PUMP
pb-sw FAULT
light
28-01-01-01A C 4 0 One or more may be inoperative provided that the
corresponding pump is set to OFF when the associated
tank is empty.
28-01-01-02 Wing TK PUMP
pb-sw OFF light
28-01-01-02A C 4 0 One or more may be inoperative provided that the
corresponding pump indication is operative on the FUEL
SD page.
28-01-01-03 X FEED pb-sw
ON light
28-01-01-03A C 1 0 May be inoperative provided that the X FEED indication is
operative on the FUEL SD page.
28-01-01-04 X FEED pb-sw
OPEN light
28-01-01-04A C 1 0 May be inoperative provided that the X FEED indication is
operative on the FUEL SD page.
12 FEB 12MEL
A320/321MEL/CDL 01.28.01
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-01 Overhead Panels
28-01-01 FUEL Overhead
Panel
28-01-01-05 CTR TK PUMP
pb-sw FAULT
light
(A320)
28-01-01-05A C 2 0 One or both may be inoperative provided that the
corresponding pump is set to OFF when there is no fuel in
the center tank.
28-01-01-05 CTR TK XFR pb-
sw FAULT light
(A321)
28-01-01-05A C 2 0 One or both may be inoperative provided that the
corresponding transfer valve is set to OFF when there is
no fuel in the center tank.
28-01-01-06 CTR TK PUMPpb-sw OFF light
(A320)
28-01-01-06A C 2 0 One or both may be inoperative provided that the
corresponding pump indication is operative on the FUEL
SD page.
28-01-01-06 CTR TK XFR pb-
sw OFF light
(A321)
28-01-01-06A C 2 0 One or both may be inoperative provided that the
corresponding transfer valve indication is operative on theFUEL SD page.
01.28.02FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-01 Overhead Panels
28-01-01 FUEL Overhead
Panel
28-01-01-07 FUEL MODE
SEL pb-sw
FAULT light
(A320)
28-01-01-07A C 1 0 (O) May be inoperative provided that all tank pumps
indications are operative on the FUEL SD page.
OPERATING PROCEDURES
AFTER ENGINE START
- If there is fuel in the center tank and with the slatsretracted:On the FUEL SD page, check that the center tankpumps indications are in line.
- With the slats extended:
On the FUEL SD page, check that the center tank
pumps indications are cross line.
AFTER TAKEOFF
- If there is fuel in the center tank and with the slatsretracted:On the FUEL SD page, check that the center tankpumps indications are in line.
28-01-01-07 FUEL MODE
SEL pb-sw
FAULT light
(A321)
28-01-01-07B C 1 0 May be inoperative provided that all wing tank pumps and
center tank transfer valves indications are operative on the
FUEL SD page.
12 FEB 12MEL
A320/321MEL/CDL 01.28.03
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-01 Overhead Panels
28-01-01 FUEL Overhead
Panel
28-01-01-08 ACT pb-sw
FAULT light
(A320) (ACTs)
28-01-01-08A C 1 0 (O) May be inoperative provided that the fuel quantity
indications of the ACT(s) and of the center tank are
operative on the FUEL SD page.
OPERATING PROCEDURES
IN FLIGHT
- If a manual transfer from the ACT to the CTR tankis necessary:
- Refer to FCOM/PRO-ABN-28 ACT XFR FAULT PROC .
- On the FUEL SD page, monitor the fuel transfer.
28-01-01-09 ACT pb-sw FWD
light (A320)
(ACTs)
28-01-01-09A C 1 0 May be inoperative.
01.28.04FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-01 Fuel On Board
(FOB) Indication
on the FUEL SD
page
28-07-01-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
AFTER ENGINE START
Check that /FF is selected on the MCDU FUEL PREDpage.
- If /FF is not selected on the MCDU FUEL PREDpage:
Insert the FOB.
The FOB may be calculated either using theindications on the refuel control panel (if available)or by using the Manual Magnetic Indicators(MMIs):Refer to FCOM/LOD-FUL-FUEL-C USE OF MANUAL MAGNETIC INDICATIOR (MMI)
12 FEB 12MEL
A320/321MEL/CDL 01.28.05
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-02 Fuel Quantity
Indication (FQI)
in Degraded
Mode on the
FUEL SD page
28-07-01-02A (A320 ACTs)
(A320)
(A321)
C
C
C
6
5
3
0
0
0
(O) One or more FQI may be in the degraded mode (with
dashes on the two last digits) provided that the loss of
accuracy is taken into account for the fuel planning for
each affected tank.
Note:
The Fuel On Board indication is also in
the degraded mode.
OPERATING PROCEDURES (A320)
ON GROUND
The FQI is in degraded mode when the FOB indication is
displayed with two dashes across the two last digits on the
EWD.
- When the FQI is in degraded mode:
On the FUEL SD page, determine which tank isaffected.The resulting loss of accuracy must be taken into
account by using the two following parameters:
1. Fq : The extra fuel quantity to be loaded.
2. W: The weight to be added to the total fuel weightfor TOW calculation only.
Fq and W parameters are given as follows :
(Cont’d on next page)
01.28.06FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-02 Fuel Quantity
Indication (FQI)
in Degraded
Mode on the
FUEL SD page
28-07-01-02A (Cont’d) OPERATING PROCEDURES(Cont’d)
Applicable to (A320)
LOSS OF ACCURACY DUE TO THE FUEL QUANTITYINDICATION IN DEGRADED MODE
(Values in kg)
Fq(kg) W (kg)
OUTER TANK 20 200
INNER TANK 110 110
CENTER TANK 130 130
ALL TANKS 390 750
- When the auto refuel stops:
- Preselect the fuel quantity required for the mission :Fm
- Enter the table and determine Fq and W values for the affected tank.
- Start again the auto refuel with the new preselectedquantity which corresponds to the total FOB :Fm+Fq
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.28.07
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-02 Fuel Quantity
Indication (FQI)
in Degraded
Mode on the
FUEL SD page
28-07-01-02A (Cont’d) OPERATING PROCEDURES (A320)
Note:
If all tanks reach high level before
having loaded the complete Fq value,
this shows that all tanks are
volumetrically full but the necessary fuel
mass for the mission is not guaranteed
since the fuel quantity indication varieswith the fuel density. Therefore the
mission or the aircraft load must be
amended to match the minimum fuel
quantity known to be onboard.
- When the auto refuel stops again:
The FOB value to be considered for TOW calculationis: FOB = Fm+Fq+W
- If all tanks reach high level before havingloaded Fq value:- The extra fuel quantity known to be onboard is
Fq* with: Fq* < Fq
- The FOB value to be considered for TOWcalculation is: FOB = Fm+Fq *+W
- If the resulting TOW is higher than the MTOW:
The aircraft load must be reduced.
(Cont’d on next page)
01.28.08FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-02 Fuel Quantity
Indication (FQI)
in Degraded
Mode on the
FUEL SD page
28-07-01-02A (Cont’d) OPERATING PROCEDURES (A321)
ON GROUND
The FQI is in degraded mode when the FOB indication is
displayed with two dashes across the two last digits on the
EWD.
- When the FQI is in degraded mode:
On the FUEL SD page, determine which tank isaffected.The resulting loss of accuracy must be taken intoaccount by using the two following parameters:
1. Fq : The extra fuel quantity to be loaded.
2. W: The weight to be added to the total fuel weightfor TOW calculation only.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.28.09
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-02 Fuel Quantity
Indication (FQI)
in Degraded
Mode on the
FUEL SD page
28-07-01-02A (Cont’d) OPERATING PROCEDURES (A321) (Cont’d)
Fq and W parameters are given as follows :
LOSS OF ACCURACY DUE TO THE FUEL QUANTITYINDICATION IN DEGRADED MODE
(Values in kg)
Fq(kg) W (kg)
WING TANK 130 310
CENTER TANK 130 130
ALL TANKS 390 750
- When the auto refuel stops:
- Preselect the fuel quantity required for the mission: Fm
- Enter the table and determine Fq and W values for the affected tank.
- Start again the auto refuel with the newpreselected quantity which corresponds to the
total FOB : Fm+Fq
(Cont’d on next page)
01.28.10FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-02 Fuel Quantity
Indication (FQI)
in Degraded
Mode on the
FUEL SD page
28-07-01-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
Applicable to (A321)
Note:
If all tanks reach high level before
having loaded the complete Fq value,
this shows that all tanks are
volumetrically full but the necessary fuel
mass for the mission is not guaranteedsince the fuel quantity indication varies
with the fuel density. Therefore the
mission or the aircraft load must be
amended to match the minimum fuel
quantity known to be onboard.
- When the auto refuel stops again:
The FOB value to be considered for TOW calculationis: FOB = Fm+Fq+W
- If all tanks reach high level before having loaded Fqvalue:
- The extra fuel quantity known to be onboard isFq* with: Fq* < Fq
- The FOB value to be considered for TOW
calculation is: FOB = Fm+Fq *+W
- If the resulting TOW is higher than the MTOW:
The aircraft load must be reduced.
12 FEB 12MEL
A320/321MEL/CDL 01.28.11
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-03 Outer Tank Fuel
Quantity
Indication on the
FUEL SD page
(A320)
28-07-01-03A Check of fuel
quantity in the
associated tank
after refueling
C 2 1 (O)(M) One may be inoperative provided that:
1) The fuel quantity in the associated tank is checkedafter each refueling by the corresponding fuel quantityindicator on the refuel/defuel control panel, and
2) The associated fuel used indication is operative, and
3) The associated inner tank indication is operative.
OPERATING PROCEDURES
AFTER REFUELING
To check the fuel quantity in the associated tank:Refer to FCOM/PER-LOD-FUL-FUEL-A. GENERALINFORMATION.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-003
28-07-01-03B High level fuel
detection
system checkedoperative
before refueling
and associated
inner tank
indication
operative
C 2 1 (M) One may be inoperative provided that:
1) The high level fuel detection system is checked
operative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative, and
4) The associated inner tank indication is operative.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-003
01.28.12FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-03 Outer Tank Fuel
Quantity
Indication on the
FUEL SD page
(A320)
28-07-01-03C Check of fuel
quantity in the
associated wing
after refueling/
defueling
B 2 1 (O)(M) One may be inoperative provided that:
1) The fuel quantity in the associated wing (inner andouter tanks) is checked after each refueling/defuelingby the corresponding fuel quantity indicator on therefuel/defuel control panel, and
2) The associated fuel used indication is operative.
OPERATING PROCEDURES
Refer to MEL item 28-07-01-03A
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-003
28-07-01-03D High level fuel
detection
system checked
operative
before refueling
B 2 1 (M) One may be inoperative provided that:
1) The high level fuel detection system is checkedoperative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-003
12 FEB 12MEL
A320/321MEL/CDL 01.28.13
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-04 Inner Tank Fuel
Quantity
Indication on the
FUEL SD page
(A320)
28-07-01-04A Check of fuel
quantity in the
associated tank
after refueling
C 2 1 (O)(M) One may be inoperative provided that:
1) The fuel quantity in the associated tank is checkedafter each refueling by the corresponding fuel quantityindicator on the refuel/defuel control panel, and
2) The associated fuel used indication is operative.
OPERATING PROCEDURES
AFTER ENGINE START
Check that /FF is selected on the MCDU FUEL PREDpage.
- If /FF is not selected on the MCDU FUEL PREDpage:
Insert the FOB.
The FOB may be calculated either using theindications on the refuel control panel (if available)or by using the Manual Magnetic Indicators(MMIs): Refer to FCOM/PER-LOD-FUL-FUEL-C.MANUAL MAGNETIC INDICATOR (MMI)
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-005
01.28.14FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-04 Inner Tank Fuel
Quantity
Indication on the
FUEL SD page
(A320)
28-07-01-04B High level fuel
detection
system checked
operative
before refueling
C 2 1 (M) One may be inoperative provided that:
1) The high level fuel detection system is checkedoperative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-005
12 FEB 12MEL
A320/321MEL/CDL 01.28.15
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-04 Wing Tank Fuel
Quantity
Indication on the
FUEL SD page
(A321)
28-07-01-04A Check of fuel
quantity in the
associated tank
after refueling
C 2 1 (O)(M) One may be inoperative provided that:
1) The fuel quantity in the associated tank is checkedafter each refueling by the manual magnetic indicatorsor by the corresponding fuel quantity indicator on therefuel/defuel control panel, and
2) The associated fuel used indication is operative.
OPERATING PROCEDURES
AFTER ENGINE START
Check that /FF is selected on the MCDU FUEL PREDpage.
- IIf /FF is not selected on the MCDU FUEL PREDpage:
Insert the FOB.
The FOB may be calculated either using theindications on the refuel control panel (if available) or by using the Manual Magnetic Indicators (MMIs): Refer to FCOM/PER-LOD-FUL-FUEL-C.
MANUAL MAGNETIC INDICATOR (MMI).MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-005
01.28.16FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-05 Center Tank
Fuel Quantity
Indication on the
FUEL SD page
(A320)
28-07-01-05A Check of fuel
quantity after
refueling
C 1 0 (O)(M) May be inoperative provided that:
1) The fuel quantity in the center tank is checked after each refueling by the manual magnetic indicators or bythe corresponding fuel quantity indicator on therefuel/defuel control panel, and
2) All wing tanks fuel quantity indications are operative,and
3) Both fuel used indications are operative.
OPERATING PROCEDURES
AFTER REFUELING
To check the fuel quantity in the associated tank:Refer to FCOM/PER-LOD-FUL-FUEL-C.MANUAL MAGNETIC INDICATOR (MMI).
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-006
28-07-01-05B Fuel in the
center tank not
usable
C 1 0 May be inoperative provided that there is no fuel in the
center tank or the fuel in this tank is considered as not
usable and as part of the ZFW and is taken into account
for CG determination.
12 FEB 12MEL
A320/321MEL/CDL 01.28.17
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-05 Center Tank
Fuel Quantity
Indication on the
FUEL SD page
(A320) (ACTs)
Note:
This failure will result in the display of the FUEL ACT XFR FAULT alert while
the automatic transfer is still operative.
Refer to Item 28-09-03 FUEL ACT XFR
FAULT Alert
28-07-01-05A Check of fuel
quantity after
refueling
C 1 0 (O)(M)
(FD)
May be inoperative provided that:
1) The fuel quantity in the center tank is checked after each refueling by the manual magnetic indicators or bythe corresponding fuel quantity indicator on therefuel/defuel control panel, and
2) All wing tanks and ACT(s) fuel quantity indications areoperative, and
3) Both fuel used indications are operative, and
4) The forward transfer from ACT(s) to the center tank ismonitored during the flight.
OPERATING PROCEDURES
AFTER REFUELING
To check the fuel quantity in the associated tank: Refer to
FCOM/PER-LOD-FUL-FUEL-A.GENERAL
INFORMATION.
(Cont’d on next page)
01.28.18FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-05 Center Tank
Fuel Quantity
Indication on the
FUEL SD page
(A320) (ACTs)
28-07-01-05A (Cont’d) OPERATING PROCEDURES (Cont’d)
AT TOP OF CLIMB
- Check on the FUEL SD page that the fuel istransferred from one additional center tank (from ACT2 if ACT 2 is installed and not empty) to the center tank.
- Check that the fuel quantity in one additional center tank has decreased (from ACT 2 if ACT 2 is installedand not empty).
- If the automatic transfer has not started:
- After 30 minutes of flight:
- ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD
- If necessary perform a descent to FL 270.
- When ACT (both ACTs if two ACTs installed)empty:
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-006
28-07-01-05B Fuel in the
center tank not
usable
C 1 0 May be inoperative provided there is no fuel in the center
tank or the fuel in this tank is considered as not usable and
as part of the ZFW and is taken into account for CG
determination.
12 FEB 12MEL
A320/321MEL/CDL 01.28.19
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-06 ACT Fuel
Quantity
Indication on the
FUEL SD page
(A320) (ACTs)
Note:
This failure will result in the inhibition of the FUEL ACT XFR FAULT alert.
Refer to Item 28-09-03 FUEL ACT XFR
FAULT Alert
28-07-01-06B Fuel in the ACT C 1 0 (O)(FD) One fuel quantity indication may be inoperative provided
that:
1) All wing tanks and center tank and the other ACT fuelquantity indications are operative, and
2) Both fuel used indications are operative, and
3) The forward transfer from ACT(s) to the center tank ismonitored during the flight.
OPERATING PROCEDURES
AT TOP OF CLIMB
Check of the fuel transfer from one additional center tank
(from ACT 2 if ACT 2 is installed and not empty) to the
center tank:
On the FUEL SD page, check that the transfer indication
(arrow) is displayed or check that the total fuel indicated is
above the actual fuel indicated after refuel minus FU.
- If the automatic transfer has not started:
- After 30 minutes of flight:- ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD
- If necessary perform a descent to FL 270.
(Cont’d on next page)
01.28.20FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-01 Fuel Quantity
Indications on
the FUEL SD
page
28-07-01-06 ACT Fuel
Quantity
Indication on the
FUEL SD page
(A320) (ACTs)
28-07-01-06B (Cont’d) OPERATING PROCEDURES (Cont’d)
- When ACT (both ACTs if two ACTs installed) isempty:
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
28-70-01-06C ACT empty C 1 0 One may be inoperative provided that there is no fuel in
any ACT.
12 FEB 12MEL
A320/321MEL/CDL 01.28.21
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-02 Fuel
Temperature
Indications on
the FUEL SD
page
28-07-02-01 Fuel
Temperature
Indication on the
FUEL SD page
(A320)
28-07-02-01A C 4 2 One in each wing or both in one wing may be inoperative.
28-07-02-01 Fuel
Temperature
Indication on the
FUEL SD page
(A321)
28-07-02-01A C 2 1 One may be inoperative.
01.28.22FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-03 Tank Pump
Indications on
the FUEL SD
page
28-07-03-01 Wing Tank
Pump Indication
on the FUEL SD
page
28-07-03-01A C 4 0 One or more may be inoperative.
28-07-03-02 Center Tank
Pump Indication
on the FUEL SD
page (A320)
28-07-03-02A C 2 0 One or both may be inoperative.
28-07-04 ValveIndications on
the FUEL SD
page
28-07-04-01 Engine LP Fuel
Valve Indication
on the FUEL SD
page
28-07-04-01A C 2 0 (M) One or both may be inoperative provided that the
associated LP valve is checked operative before each
flight.
MAINTENANCE PROCEDURE
Refer to AMM 28-24-00-040-001
12 FEB 12MEL
A320/321MEL/CDL 01.28.23
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-04 Valve
Indications on
the FUEL SD
page
28-07-04-02 APU LP Fuel
Valve Indication
on the FUEL SD
page
28-07-04-02A C 1 0 (M) May be inoperative provided that:
1) The APU LP valve is secured in the closed positionand,
2) The APU is not used.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-001
28-07-04-03 Crossfeed Valve
Indication on the
FUEL SD page
28-07-04-03A C 1 0 (M) May be inoperative provided that operation of the
crossfeed valve is checked before the first flight of each
day.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-002
01.28.24FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-04 Valve
Indications on
the FUEL SD
page
28-07-04-04 Wing Transfer
Valve Indication
on the FUEL SD
page
(A320)
28-07-04-04A C 2 0 (O)(M) One or both may be inoperative provided that:
1) The fuel quantity indications of the associated inner and outer tanks are operative, and
2) The transfer valve operation is checked before eachflight and when used in flight.
OPERATING PROCEDURES
IN FLIGHT
- When any inner tank fuel quantity reaches 750 kgof fuel:
On the FUEL SD page, check the associated outer tank transfer.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-004
12 FEB 12MEL
A320/321MEL/CDL 01.28.25
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-07 Indications on the
FUEL SD page
28-07-04 Valve
Indications on
the FUEL SD
page
28-07-04-05 Center Tank
Transfer Valve
Indication on the
FUEL SD page
(A321)
28-07-04-05A C 2 0 One or both may be inoperative.
28-07-04-06 ACT to CTR TK
Transfer (Arrow)
Indication on the
FUEL SD page
(A320) (ACTs)
28-07-04-06A C 1 0 May be inoperative provided that the fuel quantity
indications (both FQI if both ACTs installed) of the ACT(s)
and of the center tank are operative on the FUEL SD
page.
01.28.26FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-09 ECAM Alerts
28-09-01 FUEL L(R)
INNER(OUTER)
TK HI TEMP
Alert
(A320)
28-09-01A One or two
inoperative
C 4 2 (O) One in each wing or both in one wing may be displayed
provided that:
1) The fuel temperature indications of the non affectedtanks are operative on the FUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
On the FUEL SD page, monitor the fuel temperature
before takeoff and periodically during the flight.
Note:
For fuel temperature limits, Refer to
FCOM LIMITATION.
- If fuel temperature reaches limits:
- Before takeoff:
Delay takeoff and shut down the engine on theaffected side.
- In flight:- Increase the engine fuel flow on the affected
side.
- If necessary use the APU GEN and switch off
the IDG on the affected side (if the opposite
GEN is available).
12 FEB 12MEL
A320/321MEL/CDL 01.28.27
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-09 ECAM Alerts
28-09-01 FUEL L(R)
INNER(OUTER)
TK HI TEMP
Alert (A320)
28-09-01B One or more
inoperative
C 4 0 (O) One or more may be displayed provided that:
1) The fuel temperature indications are operative on theFUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
OPERATING PROCEDURES
Refer to MEL item 28-09-01A (A320)
28-09-01 FUEL L(R) WINGTK HI TEMP
Alert (A321)
28-09-01A One inoperative C 2 1 (O) One may be displayed provided that:
1) The fuel temperature indications of the opposite wingare operative on the FUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
(Cont’d on next page)
01.28.28FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-09 ECAM Alerts
28-09-01 FUEL L(R) WING
TK HI TEMP
Alert (A321)
28-09-01A (Cont’d) OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
On the FUEL SD page, monitor the fuel temperaturebefore takeoff and periodically during the flight.
Note:
For fuel temperature limits, Refer to
FCOM LIMITATION.
- If fuel temperature reaches limits:
- Before takeoff:
Delay takeoff and shut down the engine on theaffected side.
- In flight:
- Increase the engine fuel flow on the affectedside.
- If necessary use the APU GEN and switch off
the IDG on the affected side (if the opposite
GEN is available).
28-09-01B Two inoperative C 2 0 (O) One or both may be displayed provided that:
1) The fuel temperature indications are operative on theFUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
OPERATING PROCEDURES
Refer to MEL item 28-09-01A (A321)
12 FEB 12MEL
A320/321MEL/CDL 01.28.29
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-09 ECAM Alerts
28-09-02 FUEL L(R)
INNER(OUTER)
TK LO TEMP
Alert
(A320)
28-09-02A One or two
inoperative
C 4 2 (O) One in each wing or both in one wing may be displayed
provided that:
1) The fuel temperature indications of the non affectedtanks are operative on the FUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
On the FUEL SD page, monitor the fuel temperature
before takeoff and periodically during the flight.
Note:
For fuel temperature limits, Refer to
FCOM LIMITATION.
- If fuel temperature reaches limits:
- Before takeoff:
Delay takeoff.
- In flight:
Consider descending to a lower altitude and/or increasing the mach to increase the TAT.
01.28.30FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-09 ECAM Alerts
28-09-02 FUEL L(R)
INNER(OUTER)
TK LO TEMP
Alert
(A320)
28-09-02B One or more
inoperative
C 4 0 (O) One or more may be displayed provided that:
1) The fuel temperature indications are operative on theFUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
OPERATING PROCEDURES
Refer to MEL item 28-09-02A (A320)
28-09-02 FUEL L(R) WINGTK LO TEMP
Alert
(A321)
28-09-02A One inoperative C 2 1 (O) One may be displayed provided that:
1) The fuel temperature indications of the opposite wingare operative on the FUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.28.31
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-09 ECAM Alerts
28-09-02 FUEL L(R) WING
TK LO TEMP
Alert
(A321)
28-09-02A (Cont’d) OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
On the FUEL SD page, monitor the fuel temperature
before takeoff and periodically during the flight.
Note:
For fuel temperature limits, Refer to
FCOM LIMITATION.
- If fuel temperature reaches limits:
- Before takeoff:
Delay takeoff.
- In flight:
Consider descending to a lower altitude and/or increasing the mach to increase the TAT.
28-09-02B Both
inoperative
C 2 0 (O) One or both may be displayed provided that:
1) The fuel temperature indications are operative on theFUEL SD page, and
2) The fuel temperature is monitored before takeoff andduring the flight.
Note:
For fuel temperature limitations, Refer toFCOM LIMITATION.
OPERATING PROCEDURES
Refer to MEL item 28-09-02A (A321)
01.28.32FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-09 ECAM Alerts
28-09-03 FUEL ACT XFR
FAULT Alert
(A320) (ACTs)
28-09-03A ACT empty C 1 0 May be displayed provided that there is no fuel in any
ACT.
28-09-03B ACT fuel
transfer
monitored
C 1 0 (O) May be displayed provided that the forward transfer from
the ACT(s) to the center tank is monitored during the flight.
OPERATING PROCEDURES
Refer to Operating Procedures 28-07-01-05A Center Tank
Fuel Quantity Indication on the FUEL SD page
28-12 Tank Venting
System
28-12-01 Overpressure
Protector
between theInner and the
Outer Tank
(A320)
28-12-01A Inner tank
temperature
monitored
C 2 0 (O) One or both may be broken or missing provided that the
fuel temperature of the inner tank is monitored.
OPERATING PROCEDURES
GENERAL INFORMATION
The dispatch condition results in an unusual distribution of the fuel quantity: the outer tank of the affected wing will be
partially empty with the transfer valves normally closed.
FLIGHT PREPARATION/LIMITATIONS
Fuel management should be performed with care.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.28.33
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-12 Tank Venting System
28-12-01 Overpressure
Protector
between Inner
and Outer Tank
(A320)
28-12-01A (Cont’d) OPERATING PROCEDURES(Cont’d)
ON GROUND AND IN FLIGHT
- After a long taxi or if the outside air temperature ishigh, with the outer tank of the affected wingempty:The FUEL L(R) OUTER TK HI TEMP alert may bedisplayed on the EWD.
- If the FUEL L(R) OUTER TK HI TEMP alert isdisplayed on the EWD:- Disregard the FUEL L(R) OUTER TK HI TEMP
alert.
- Monitor the inner tank fuel temperature during
taxi and in flight to ensure that it decreases and
remains within the temperature limitations.
Note:
For fuel temperature limitations, Refer to
FCOM LIMITATION.
- If the inner tank fuel temperature exceeds the
temperature limitations, apply the FUEL L(R)
INNER TK HI TEMP procedure:
Refer to Operating Procedres 28-09-01A(B)
FUEL L(R) INNER(OUTER)/WING TK HI
TEMP Alert.
28-12-01B Transfer valvessecured open C 2 0 (O)(M) One or both may be broken or missing provided that theassociated transfer valves are secured in the open position
after each refueling.
(Cont’d on next page)
01.28.34FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-12 Tank Venting
System
28-12-01 Overpressure
Protector
between Inner
and Outer Tank
(A320)
28-12-01B (Cont’d) OPERATING PROCEDURES
GENERAL INFORMATION
The dispatch condition results in an unusual distribution of
the fuel quantity: the fuel in the outer tank on the affected
side will transfer to the inner tank even when the inner tank
is not empty.
ON GROUND
Do not re-select the refuel power or open the refuel door.
Note:
The transfer valve latch circuit will sendorder to de-latch them and the valves
will close again (they will then operate
normally and open at low level).
MAINTENANCE PROCEDURE
Refer to AMM 28-12-00-040-003
12 FEB 12MEL
A320/321MEL/CDL 01.28.35
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-12 Tank Venting System
28-12-02 Overpressure
Protector in the
Vent Surge Tank
28-12-02A C 2 1 (O) One may be broken or missing.
OPERATING PROCEDURES
ON GROUND AND IN FLIGHT
- Avoid lateral accelerations in order to reduce thepossibility of fuel spill during taxi and climb out.
- In cruise check that no fuel spillage occurred.
- Check that the FOB is sufficient to reach thedestination with the adequate reserve.
28-12-03 Overpressure
Protector in the
Inner Tank
(A320)
28-12-03A 2 2 Both must be operative.
28-12-03 Overpressure
Protector in the
Wing Tank
(A321)
28-12-03A 2 2 Both must be operative.
01.28.36FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-12 Tank Venting
System
28-12-04 Overpressure
Protector
between the
Center and the
Inner Tank
(A320)
28-12-04A 1 1 Must be operative.
28-12-04 Overpressure
Protector
between the
Center and the
Wing Tank
(A321)
28-12-04A 1 1 Must be operative.
28-12-05 Overpressure
Protector in the
ACT (A320)
(ACTs)
28-12-05A C 1 0 May be broken or missing provided that the ACT auto
transfer system is considered inoperative.
Refer to Item 28-28-01 ACT Auto Transfer System
12 FEB 12MEL
A320/321MEL/CDL 01.28.37
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-15 Intercell Transfer
System
28-15-01 LH Wing
Transfer Valve
(A320)
28-15-01A One or both
inoperative
open
C 2 0 (O) One or both may be inoperative in the open position.
OPERATING PROCEDURES
GENERAL INFORMATION
The dispatch condition results in an unusual distribution of
the fuel quantity: the fuel in the outer tank on the affected
side will transfer to the inner tank even when the inner tank
is not empty.
25-15-01C One inoperative
closed
C 2 1 (O)(M) One may be inoperative in the closed position provided
that the remaining LH wing transfer valve is secured in the
open position after each refueling.
OPERATING PROCEDURES
Refer to MEL item 28-15-01A.
MAINTENANCE PROCEDURE
Refer to AMM 28-15-00-040-001
01.28.38FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-15 Intercell Transfer
System
28-15-02 RH Wing
Transfer Valve
(A320)
28-15-02A One or both
inoperative
open
C 2 0 (O)(FD) One or both may be inoperative in the open position.
OPERATING PROCEDURES
GENERAL INFORMATION
The dispatch condition results in an unusual distribution of
the fuel quantity: the fuel in the outer tank on the affected
side will transfer to the inner tank even when the inner tank
is not empty.
28-15-02C One inoperative
closed
C 2 1 (O)(M) One may be inoperative in the closed position provided
that the remaining RH wing transfer valve is secured in the
open position after each refueling.
OPERATING PROCEDURES
Refer to MEL item 28-15-02A
MAINTENANCE PROCEDURE
Refer to AMM 28-15-00-040-002
12 FEB 12MEL
A320/321MEL/CDL 01.28.39
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-20 Distribution
28-20-01 Automatic Fuel
Feed System
(A320)
28-20-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
ON GROUND
- If the center tank is empty for the flight :
- MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . MAN
- CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF
- If the center tank is not empty for the flight:
- Before engine start:
MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . MAN
- 3 min after engine start :
CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF
- After slats retraction and when the fuel in onewing is less than 5 000 kg:CTR TK PUMP 1 and 2 pb-sw. . . . . . . . . . . . . . On
- When the FUEL CTR TK PUMPS LO PR alert isdisplayed on the EWD:CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF
28-21 Main Fuel Pump
System
28-21-01 Wing Tank
Pump
28-21-01A JP4/JET B notused
C 4 3 One pump may be inoperative provided that JP4/JET B isnot used.
01.28.40FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-21 Main Fuel Pump
System
28-21-01 Wing Tank
Pump
28-21-01B Use of JP4/
JET B
C 4 3 (M) Pump 2 LH or pump 2 RH may be inoperative when
JP4/JET B is used provided that:
1) The fuel return valve is checked operative before each
flight, and2) The fuel temperature is less than 30 °C.
MAINTENANCE PROCEDURE
Refer to AMM 28-21-00-040-001
28-21-02 Center Tank
Pump
(A320) (ACTs)
28-21-02A One inoperative C 2 1 (O)(FD) One may be inoperative provided that the flight routespermit a landing at a suitable airport if the remaining center
tank pump fails with fuel in the center tank and in any
ACT(s).
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
In the case of dispatch with fuel in the center tank, the
remaining center tank pump failure must be considered for
the flight planning. Operator has to ensure that, from any
point of the first part of the route where the center tank is
not empty the aircraft may reach a suitable airportconsidering the fuel quantity (FQ) contained in the center
tank as definitely not usable for the flight planning (as a
consequence of the failure of the remaining center tank
pump).
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.28.41
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-21 Main Fuel Pump
System
28-21-02 Center Tank
Pump
(A320) (ACTs)
28-21-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
DURING COCKPIT PREPARATION
- X FEED pb-sw · · · · · · · · · · · · · · · · · · · · · · CHECK Off
- Affected CTR TK PUMP pb-sw · · · · · · · · · · · · · · · OFF
< If the fuel quantity in the center tank is less than
200 kg:
- Operative CTR TK PUMP pb-sw · · · · · · · · · · · · · · OFF
< If the fuel quantity in the center tank is more than
200 kg:
- Operative CTR TK PUMP pb-sw · · · · · · · · · · · · · · · On
IN FLIGHT
< If the fuel quantity in the center tank is less than
200 kg:
- Operative CTR TK PUMP pb-sw· · · · · · · Maintain OFF
< If the fuel quantity in the center tank is more than
200 kg:
The fuel in the center tank can be completely used if the
operative center tank pump does not fail before the center
tank is empty. If the operative center tank pump fails
before the center tank is empty, consider the fuel quantityremaining and the time to destination to decide either to
continue the flight or to divert.
(Cont’d on next page)
01.28.42FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-21 Main Fuel Pump
System
28-21-02 Center Tank
Pump
(A320) (ACTs)
28-21-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
· When the fuel quantity in the first wing inner tank is
less than 4 500 kg:
Operative CTR TK PUMP pb-sw . . . . . . . . . . . . . . . . . OFF
X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
· When the fuel quantity in the first wing inner tank
increases above 5 500 kg:
X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
Operative CTR TK PUMP pb-sw . . . . . . . . . . . . . . . . . OFF
· When the fuel quantity in the center tank is less
than 250 kg:
X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
12 FEB 12MEL
A320/321MEL/CDL 01.28.43
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-21 Main Fuel Pump
System
28-21-02 Center Tank
Pump
(A320)
28-21-02A One inoperative C 2 1 (O)(FD) One may be inoperative in the closed position provided
that the flight routes permit a landing at a suitable airport if
the remaining center tank transfer valve fails with fuel in
the center tank.
OPERATING PROCEDURES
IN FLIGHT
- Disregard the FUEL L(R) XFR VALVE FAULT alertdisplayed on the EWD.
- MODE SEL pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · Auto
- Operative CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · On
- Affected CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · OFF
- When differences between fuel quantities in twowings is above 1 500 kg:Monitor the fuel imbalance.
Note:
Apply the FUEL IMBALANCE FCOM
procedure as required provided that no
fuel leak is suspected.
- Until the fuel is balanced:
L(R) TK PUMPS (on the lighter side) pb-sw . . OFF
28-21-03 Wing Tank
Pump Sequence
Valve
(A320)
28-21-03A C 4 3 One may be inoperative provided that the associated
pump is set to OFF when the center tank is feeding.
01.28.44FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-22 APU Fuel Pump
System
28-22-01 APU Fuel Pump
28-22-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
FOR APU START OPERATION
Pressurize the LH fuel manifold with at least one fuel tank
pump.
28-22-01B A 1 0 (O)(FD) May be inoperative for four flights.
OPERATING PROCEDURES
Refer to MEL item 28-22-01A
28-23 Crossfeed System
28-23-01 Crossfeed Valve
28-23-01A 1 1 Must be operative.
12 FEB 12MEL
A320/321MEL/CDL 01.28.45
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-24 Engine LP Fuel
Shutoff
28-24-01 Engine LP Fuel
Valve Electrical
Motor
28-24-01A C 4 3 (M) One may be inoperative on one engine provided that:
1) The affected motor is deactivated, and
2) The remaining motor is checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 28-24-00-040-002
28-25 Refuel/Defuel System
28-25-01 Fuel Quantity
Preselector
28-25-01A C 1 0 May be inoperative.
28-25-02 Fuel Quantity onthe
Refuel/Defuel
Control Panel
28-25-02A (A320 ACTs)
(A320)
(A321)
C
C
C
8
7
5
0
0
0
One or more indications may be inoperative provided that
the fuel quantity is continuously monitored on the FUEL
SD page during refueling and defueling.
28-25-03 Refuel Valve
28-25-03A Manual
refueling
C 3 0 (M) One or more may be inoperative provided that the aircraft
is manually refueled.
MAINTENANCE PROCEDURE
Refer to AMM 28-25-00-040-005
01.28.46FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-25 Refuel/Defuel
System
28-25-03 Refuel Valve
28-25-03B Gravity
refueling
C 3 0 One or more may be inoperative provided that overwing
gravity refueling is performed.
Refer to FCOM/PER-LOD-FUL OVERWING GRAVITY
REFUELING
28-25-04 Transfer Defuel
Valve
28-25-04A C 1 0 (M) May be inoperative provided that the valve is secured in
the closed position.
MAINTENANCE PROCEDURE
Refer to AMM 28-25-00-040-004
28-25-05 Exterior
Refuel/Defuel
Control Panel
(A320)
28-25-05A Cockpit Fuel
Quantity pre-
selector
operative
C 1 0 (M) May be inoperative provided that the cockpit fuel quantity
pre-selector is operative.
MAINTENANCE PROCEDURE
Refer to AMM 28-25-00-040-008
28-25-05 Exterior
Refuel/Defuel
Control Panel
(A321)
28-25-05A C 1 0 (M) May be inoperative provided that the aircraft is manually
refueled.
MAINTENANCE PROCEDURE
Refer to AMM 28-25-00-040-008
12 FEB 12MEL
A320/321MEL/CDL 01.28.47
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-26 Main Transfer System
28-26-01 Center Tank
Transfer Valve
(A321)
28-26-01B One Inoperative
Closed
C 2 1 (O) One may be inoperative in the closed position provided
that the flight routes permit a landing at a suitable airport if
the remaining center tank valve fails with fuel in the center
tank.
OPERATING PROCEDURES
IN FLIGHT
- Disregard the FUEL L(R) XFR VALVE FAULT alertdisplayed on the EWD.
- MODE SEL pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · Auto
- Operative CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · On
- Affected CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · OFF
· When differences between fuel quantities in two
wings is above 1 500 kg:
Monitor the fuel imbalance.
Note:
Apply the FUEL IMBALANCE FCOM
procedure as required provided that no
fuel leak is suspected.
Refer to FCOM/PRO-ABN-28 FUEL
IMBALANCE.
· Until the fuel is balanced:
L(R) TK PUMPS (on the lighter side) pb-sw . . . . . . . . OFF
01.28.48FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer
System
28-28-01 ACT Auto
Transfer System
(A320) (ACTs)
28-28-01A ACT empty C 1 0 (FD) May be inoperative provided that there is no fuel in any
ACT.
28-28-01B Manual fuel
transfer
operative
C 1 0 (O)(FD) May be inoperative provided that:
1) The manual transfer from the ACT(s) to the center tank is operative, and
2) The fuel quantity indications of the ACT(s) and of thecenter tank are operative on the FUEL SD page.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
1. The refuel panel door must be open to check theoperation of the manual transfer on the ground usingthe FUEL SD page. Establish ground communicationsand ensure that the refuel panel door is open duringfollowing check and closed after the check is done.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.28.49
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer System
(A320) (ACTs)
28-28-01 ACT Auto
Transfer System
28-28-01B (Cont’d) OPERATING PROCEDURES (Cont’d)
2. The manual transfer may be performed only if the
center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor maybe overridden by keeping pressed in the HI LVL pbtest of the refuel panel. When the high level sensor isoverridden, take care to not overfill the center tank.Otherwise, fuel may spill out from the surge tanks.
- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD
- On the FUEL SD page, check that the fuel istransferred from one ACT (from ACT 2 if ACT 2 isinstalled and not empty) to the center tank.
- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
30 MIN AFTER TAKEOFF
- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD
- On the FUEL SD page, check that the fuel istransferred from the ACTs to the center tank.
- If necessary perform a descent to FL 270.
- When ACT (both ACTs if two ACTs installed) isempty:
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
28-28-01C ACT fuel not
usable
C 1 0 (O)(M)
(FD)
May be inoperative provided that:
1) The fuel in the ACT(s) is considered as not usable and
as part of the ZFW and is taken into account for CGdetermination, and
2) The ACT transfer valve is secured in the closedposition.
(Cont’d on next page)
01.28.50FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer
System (A320)
(ACTs)
28-28-01 ACT Auto
Transfer System
28-28-01C (Cont’d) OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
When there is less than 3 000 kg of fuel in thecenter tank:Disregard and clear the FUEL ACT XFR FAULT alertdisplayed on the EWD.
MAINTENANCE PROCEDURE
Refer to AMM 28-28-00-040-009
28-28-02 ACT Transfer
Valve
28-28-02A Valve closed
with the ACT
empty
C 1 0 (FD) May be inoperative in the closed position provided that
there is no fuel in any ACT.
28-28-02C Valve closed
with the ACT
fuel not usable
C 1 0 (O)(M)
(FD)
May be inoperative provided that:
1) It is secured in the closed position, and
2) The fuel in the ACT(s) is considered as not usable andas part of the ZFW and is taken into account for CGdetermination.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- When there is less than 3 000 kg of fuel in thecenter tank:Disregard and clear the FUEL ACT XFR FAULT alertdisplayed on the EWD.
MAINTENANCE PROCEDURE
Refer to AMM 28-28-00-040-010
12 FEB 12MEL
A320/321MEL/CDL 01.28.51
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer System
(A320) (ACTs)
28-28-03 ACT Transfer
Pump
28-28-03A C 1 0 May be inoperative.
28-28-04 ACT Air Shutoff
Valve
28-28-04A C 1 0 (FD) May be inoperative provided that the ACT auto transfer
system is considered inoperative.
Refer to Item 28-28-01 ACT Auto Transfer System
28-28-05 ACT Inward
Pressure Relief
Valve
28-28-05A Valve open with
fuel in the ACT
C 1 0 (O)(FD) May be inoperative in the open position provided that:
1) The manual transfer from the ACT(s) to the center tank is operative, and
2) The fuel quantity indications of the ACT(s) and of thecenter tank are operative on the FUEL SD page.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
1. The refuel panel door must be open to check theoperation of the manual transfer on the ground usingthe FUEL SD page. Establish ground communicationsand ensure that the refuel panel door is open duringfollowing check and closed after the check is done.
(Cont’d on next page)
01.28.52FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer
System (A320)
(ACTs)
28-28-05 ACT Inward
Pressure Relief
Valve
28-28-05A Valve open with
fuel in the
ACT(Cont’d)
OPERATING PROCEDURES (Cont’d)
2. The manual transfer may be performed only if thecenter tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor maybe overridden by keeping pressed in the HI LVL pbtest of the refuel panel. When the high level sensor isoverridden, take care to not overfill the center tank.Otherwise, fuel may spill out from the surge tanks.
- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD
- On the FUEL SD page, check that the fuel istransferred from one ACT (from the ACT 2 if the ACT 2is installed and not empty) to the center tank.
- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
AT TOP OF CLIMB
Check that the fuel is transferred from the ACTs to the
center tank.
- If the automatic transfer has not started:
- After 30 min of flight:
- ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD
- If necessary perform a descent to FL 270.
- When ACT (both ACTs if two ACTs installed) isempty:
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
28-28-05B ACT empty C 1 0 (FD) May be inoperative provided that there is no fuel in any
ACT.
12 FEB 12MEL
A320/321MEL/CDL 01.28.53
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer System
(A320) (ACTs)
28-28-06 ACT Vent Valve
28-28-06A Use of ACT fuel C 1 0 (O)(M) May be inoperative in the open position provided that:
1) The manual transfer from the ACT(s) to the center tank is operative, and
2) The fuel quantity indications of the ACT(s) and of thecenter tank are operative on the FUEL SD page.
OPERATING PROCEDURES
Refer to Operating Procedures 28-28-01B ACT Auto
Transfer System (Manual transfer from the ACT(s) to the
center tank operative)
MAINTENANCE PROCEDURE
Refer to AMM 28-28-00-040-003
28-28-06B ACT fuel notusable C 1 0 (O)(M)(FD) May be inoperative provided that:1) The fuel in the ACT(s) is considered as not usable and
as part of the ZFW and is taken into account for CGdetermination, and
2) The ACT transfer valve is secured in the closedposition.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- When there is less than 3 000 kg of fuel in thecenter tank:Disregard and clear the FUEL ACT XFR FAULT alertdisplayed on the EWD.
MAINTENANCE PROCEDURE
Refer to AMM 28-28-00-040-011
01.28.54FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer
System (A320)
(ACTs)
28-28-06 ACT Vent Valve
28-28-06E ACT empty C 1 0 (FD) May be inoperative provided that there is no fuel in any
ACT.
28-28-07 ACT Refuel
Valve
28-28-07A C 1 0 May be inoperative.
Note:
If the refuel valve is inoperative in the
closed position, the ACT cannot be
refuelled.
28-28-08 ACT IntegratedImpact Wall
28-28-08A Heat shield not
damaged
C 1 1 (M) The protection cover of the ACT integrated impact wall
may be damaged provided that the heat shield is not
damaged.
MAINTENANCE PROCEDURE
Refer to AMM 28-28-00-040-006
12 FEB 12MEL
A320/321MEL/CDL 01.28.55
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer System
(A320) (ACTs)
28-28-09 ACT 1 Inlet
Valve
28-28-09B All ACTs empty C 1 0 (FD) May be inoperative in the closed position provided that
there is no fuel in the ACT.
28-28-09C ACTs fuel not
usable
C 1 0 (O)(M)
(FD)
May be inoperative in the closed position provided that:
1) The fuel in the ACT is considered as not usable and aspart of the ZFW and is taken into account for CGdetermination, and
2) The ACT transfer valve is secured in the closedposition.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- When there is less than 3 000 kg of fuel in thecenter tank:Disregard and clear the FUEL ACT XFR FAULT alertdisplayed on the EWD.
MAINTENANCE PROCEDURE
Refer to AMM 28-28-00-040-008
01.28.56FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer
System (A320)
(ACTs)
28-28-09 ACT 1 Inlet
Valve
28-28-09D Use of ACT fuel C 1 0 (M) May be inoperative in the open position provided that the
ACT transfer valve is checked operative before each flight
when the ACT is used.
MAINTENANCE PROCEDURE
Refer to AMM 28-28-00-040-004
28-29 APU LP Fuel Shutoff
28-29-01 APU LP Fuel
Valve
28-29-01A Checked closedon FUEL SD
page
C 1 0 (O) May be inoperative provided that:
1) It is checked closed on the FUEL SD page, and
2) The APU is not used.
OPERATING PROCEDURES
BEFORE ENGINE START
The APU is not available.
APU MASTER SW pb-sw . . . . . . . . . . . . . . . . . . . . . . . . Off
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.28.57
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-28 Additional Center
Tank Transfer System
28-29 APU LP Fuel Shutoff
28-29-01 APU LP Fuel
Valve
28-29-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
Note:
i. No APU bleed air will be available for the
Main Engine Start (MES) or the air
conditioning.
ii. No electrical power will be available from the
APU generator.
On the FUEL SD page, check that the APU LP valve is
indicated closed:
Refer to FCOM/DSC-28-20 ECAM FUEL PAGE.
28-29-01B Secured closed C 1 0 (M) May be inoperative provided that:
1) It is secured in the closed position, and
2) The APU is not used.
MAINTENANCE PROCEDURE
Refer to AMM 28-29-00-040-002
01.28.58FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-43 Manual Magnetic
Indicators
28-43-01 Manual Magnetic
Indicators
(A320)
28-43-01A Associated fuel
quantity
indication
operative on the
FUEL SD page
C 9 0 One or more may be inoperative provided that the
associated fuel quantity indication is operative on the
FUEL SD page.
28-43-01B High level fuel
detection and
fuel used
indication
operative
C 9 0 (M) One or more may be inoperative provided that:
1) The high level fuel detection system is checkedoperative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-012
28-43-01 Manual Magnetic
Indicators
(A321)
28-43-01A Associated fuel
quantity
indication
operative on the
FUEL SD page
C 7 0 One or more may be inoperative provided that the
associated fuel quantity indication is operative on the
FUEL SD page.
28-43-01B High level fuel
detection andfuel used
indication
operative
C 7 0 (M) One or more may be inoperative provided that:
1) The high level fuel detection system is checkedoperative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative.
MAINTENANCE PROCEDURE
Refer to AMM 28-40-00-040-012
12 FEB 12MEL
A320/321MEL/CDL 01.28.59
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-46 Tank Level Sensing
28-46-01 High Level
Detection
System in the
Inner Tank
(A320)
28-46-01A C 2 0 One or both may be inoperative provided that the fuel
quantity is continuously monitored during refueling.
28-46-01 High Level
Detection
System in the
Wing Tank
(A321)
28-46-01A C 2 0 One or both may be inoperative provided that the fuel
quantity is continuously monitored during refueling.
28-46-02 High Level
Detection
System in the
Center Tank
28-46-02A C 1 0 May be inoperative provided that the fuel quantity is
continuously monitored during refueling.
01.28.60FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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28 FUEL
28-46 Tank Level Sensing
28-46-02 High Level
Detection
System in the
Center Tank
(A320) (ACTs)
28-46-02A C 1 0 May be inoperative provided that:
1) The fuel quantity is continuously monitored duringrefueling, and
2) The ACT auto transfer system is consideredinoperative.
Refer to Item 28-28-01 ACT Auto Transfer System
28-46-03 High Level
Detection
System in the
ACT (A320)
(ACTs)
28-64-03A C 1 0 May be inoperative provided that the fuel quantity iscontinuously monitored during refueling.
28-46-04 Low Level
Detection
System in the
Inner Tank
(A320)
28-64-04A C 2 1 One may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.28.61
FUEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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28 FUEL
28-46 Tank Level Sensing
28-46-04 Low Level
Detection
System in the
Wing Tank
(A321)
28-46-04A C 2 1 One may be inoperative.
28-46-05 Low Level
Detection
System in the
ACT
(A320) (ACTs)
28-46-05A C 1 0 May be inoperative provided that the ACT auto transfer
system is considered inoperative.
Refer to Item 28-28-01 ACT Auto Transfer System
28-50 Fuel Management
28-50-01 Fuel Quantity
Indicating
Computer (FQIC)
Channel
28-51-01A A 2 1 (O) One may be inoperative for 10 calendar days.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
1. Ensure that correct weights are entered in the FMGCassociated with the affected FQIC channel.
2. In the case of failure in-flight of the remaining FQICchannel, all fuel quantities indications on the EWD arelost.
* * *
01.28.62FUEL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-01 Overhead Panels
29-01-01 HYD Overhead
Panel
29-01-01-01 B(Y) ELEC PUMP
pb-sw FAULT light
29-01-01-01A C 2 0 One or both may be inoperative provided that the
associated reservoir quantity indication is operative on the
HYD SD page.
Note:
Simultaneous illumination of the BLUE
ELEC PUMP pb-sw FAULT light and the
ENG 1(2) PUMP pb-sw FAULT light with
engines off may be due to a failed
engine oil low pressure switch. In this
case, the ENG 1(2) OIL LO PR alert is
inoperative.
Refer to Item 79-09-01 ENG 1(2) OIL
LO PR Alert
29-01-01-02 B ELEC PUMP pb-
sw OFF light
29-01-01-02A C 1 0 May be inoperative.
29-01-01-03 Y ELEC PUMP pb-
sw ON light
29-01-01-03A C 1 0 May be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.29.01
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-01 Overhead Panels
29-01-01 HYD Overhead
Panel
29-01-01-04 G(Y) ENG 1(2)
PUMP pb-sw
FAULT light
29-01-01-04A C 2 0 One or both may be inoperative provided that the
associated reservoir quantity indication is operative on the
HYD SD page.
Note:
Simultaneous illumination of the BLUE
ELEC PUMP pb-sw FAULT light and the
ENG 1(2) PUMP pb-sw FAULT light with
engines off may be due to a failed
engine oil low pressure switch. In this
case, the ENG 1(2) OIL LO PR alert is
inoperative.
Refer to Item 79-09-01 ENG 1(2) OIL
LO PR Alert
29-01-01-05 G(Y) ENG 1(2)
PUMP pb-sw
OFF light
29-01-01-05A C 2 0 One or both may be inoperative.
29-01-01-06 PTU pb-sw
FAULT light
29-01-01-06A C 1 0 May be inoperative provided that the quantity indications of
the yellow and green reservoir are operative on the HYDSD page.
29-01-01-07 PTU pb-sw OFF
light
29-01-01-07A C 1 0 May be inoperative.
01.29.02HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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29 HYDRAULIC POWER
29-01 Overhead Panels
29-01-02 Maintenance HYD
Overhead Panel
29-01-02-01 G(B)(Y) LEAK
MEASUREMENT
VALVES pb-sw
OFF light
29-01-02-01A C 3 0 One or more may be inoperative.
29-07 Indications on the
HYD SD page
29-07-01 Yellow ELEC
Pump Indication
on the HYD SD
page
29-07-01A C 1 0 May be inoperative.
29-07-02 Pump Indicationon the HYD SD
page
29-07-02A C 3 0 One or more may be inoperative.
29-07-03 Fire Valve
Indication on the
HYD SD page
29-07-03A C 2 0 One or both may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.29.03
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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29 HYDRAULIC POWER
29-07 Indications on the
HYD SD page
29-07-04 PTU Indication
on the HYD SD
page
29-07-04A C 1 0 May be inoperative.
29-07-05 Reservoir
Quantity
Indication on the
HYD SD page
29-07-05A C 3 2 (M) One may be inoperative provided that:
1) The associated HYD B(G)(Y) RSVR LO LVL alert ischecked operative, and
2) The associated reservoir quantity is checked beforeeach flight.
MAINTENANCE PROCEDURE
Refer to AMM task
29-07-06 RAT Indication
on the HYD SD
page
29-07-06A C 1 0 May be inoperative provided that the RAT is visually
checked to be stowed before each flight.
29-07-07 System Label
Indication on the
HYD SD page
29-07-07A C 3 0 (O) One or more may be inoperative provided that theassociated system pressure is checked available before
each flight.
(Cont’d on next page)
01.29.04HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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29 HYDRAULIC POWER
29-07 Indications on the
HYD SD page
29-07-07 System Label
Indication on the
HYD SD page
29-07-07A (Cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic
System with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW
ELEC PUMP pb-sw by a similar
action on the Ground Cart or on the
YELLOW ENG 2 PUMP pb-sw in the
following procedure.
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · AUTO
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
- Move the CAPT stick left or right.
- On the F/CTL SD page, check the pairs of spoilersmovement.
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off - BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · OFF
12 FEB 12MEL
A320/321MEL/CDL 01.29.05
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-07 Indications on the
HYD SD page
29-07-08 System
Pressure
Indication on the
HYD SD page
29-07-08A C 3 2 (O) One may be inoperative provided that the associated
system label indication is checked operative before each
flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic System
with:
- A Ground cart, or with
- The Yellow Engine 2 Pump withthe Engine 2 running.
- Replace any action on the YELLOW ELEC
PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2
PUMP pb-sw in the following procedure.
- If the blue system pressure indication isinoperative:Check of the system label:
- On the HYD SD page, check that the BLUE systemlabel is amber.
- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON
- On the HYD SD page, check that the BLUE systemlabel is white and that the arrow is green.
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off
(Cont’d on next page)
01.29.06HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-07 Indications on the
HYD SD page
29-07-08 System Pressure
Indication on the
HYD SD page
29-07-08A (Cont’d) OPERATING PROCEDURES (Cont’d)
- If the yellow system pressure indication is
inoperative:Check of the system label:
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
- On the HYD SD page, check that the YELLOWsystem label is amber.
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- On the HYD SD page, check that the YELLOWsystem label is white and that the arrow is green.
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
- If the green system pressure indication is
inoperative:Check of the system label:
- On the HYD SD page, check that the GREENsystem label is amber.
- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
- On the HYD SD page, check that the GREENsystem label is white and that the arrow is green.
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
12 FEB 12MEL
A320/321MEL/CDL 01.29.07
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-09 ECAM Alerts
29-09-01 HYD B(Y) ELEC
PUMP LO PR
Alert
29-09-01A C 2 0 One or both may be displayed provided that the
associated system pressure indication is operative.
29-09-02 HYD B(Y) ELEC
PUMP OVHT
Alert
29-09-02A C 2 0 One or both may be displayed.
29-09-03 HYD G(Y) ENG
1(2) PUMP LO
PR Alert
29-09-03A C 2 0 (O) One or both may be displayed provided that:
1) The associated system pressure indications areoperative, and
2) The engine pumps are checked operative before eachflight.
OPERATING PROCEDURES
AFTER ENGINE START
Check of the engines pumps:
- PTU pb-sw· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
- On the HYD SD page, check that the green and theyellow hydraulic systems pressures are correct.
A correct pressure is 3 000 PSI ( ± 200 PSI).
- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
(Cont’d on next page)
01.29.08HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-09 ECAM Alerts
29-09-03 HYD G(Y) ENG
1(2) PUMP LO PR
Alert
29-09-03A (Cont’d)) OPERATING PROCEDURES (Cont’d)
Note:
On the HYD SD page, the PTU remainsindicated running .
TAXI
Note:
Due to a false HYD G(Y) ENG 1(2)
PUMP LO PR alert displayed on the
EWD, the “T.O CONFIG NORMAL” line
will not replace the “T.O CONFIG . .
TEST” line in the T.O MEMO.
Consider normal configuration for
takeoff provided that no alert wasdisplayed during the T.O CONFIG TEST
except a false HYD G(Y) ENG 1(2)
PUMP LO PR alert.
CAUTION:
The T.O CONFIG TEST pb must be
maintained pressed to check that there
is no alert except a false HYD G(Y)
ENG 1(2) PUMP LO PR alert.
12 FEB 12MEL
A320/321MEL/CDL 01.29.09
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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29 HYDRAULIC POWER
29-09 ECAM Alerts
29-09-04 HYD G(B)(Y)
RSVR LO AIR
PR Alert
29-09-04A C 3 2 (M) One may be inoperative provided that the air pressure is
checked on the associated reservoir before each flight.
MAINTENANCE PROCEDURE
Refer to AMM task
29-09-05 HYD G(B)(Y)
RSVR LO LVL
Alert
29-09-05A C 3 2 One may be displayed provided that the associated
reservoir quantity is checked on the HYD SD page before
each flight.
Note:
i. When the alert is displayed on the EWD, theassociated PUMP pb-sw FAULT light and
the PTU pb-sw FAULT light (if the green or
the yellow system is affected) may
simultaneously come on.
Refer to Item 29-01-01-01 B(Y) ELEC
PUMP pb-sw FAULT light, and
Refer to Item 29-01-01-04 G(Y) ENG 1(2)
PUMP pb-sw FAULT light, and
Refer to Item 29-01-01-06 PTU pb-sw
FAULT light
ii. If the blue reservoir is affected, EMER GEN
may appear in the INOP SYS column on theSTATUS SD page before engine start.
01.29.10HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-09 ECAM Alerts
29-09-06 HYD G(B)(Y) RSVR
OVHT Alert
29-09-06A C 3 2 The HYD G RSVR OVHT alert or the HYD Y RSVR OVHT
alert may be displayed.
29-09-07 HYD PTU FAULT
Alert
29-09-07A C 1 0 (O) May be displayed provided that the PTU is checked
operative before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic
System with:- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW
ELEC PUMP pb-sw by a similar
action on the Ground Cart or on the
YELLOW ENG 2 PUMP pb-sw in the
following procedure.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.29.11
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-09 ECAM Alerts
29-09-07 HYD PTU FAULT
Alert
29-09-07A (Cont’d) OPERATING PROCEDURES (Cont’d)
Check of the PTU:
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
- On the HYD SD page, check that the green hydraulicsystem pressure indication is green.If the green hydraulic system pressure indication is notavailable, check on the HYD SD page that the GREENsystem label is white and the arrow is green.
- YELLOW ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · Off
29-09-08 HYD RAT FAULT
Alert
29-09-08A C 1 0 (M) May be displayed provided that the RAT integrity is
checked before each flight.
MAINTENANCE PROCEDURE
Refer to AMM task
29-09-09 HYD
G(B)(Y)(B+G)(G+
Y)(B+Y) SYS LO
PR Alert
29-09-09A C 3 0 (O) One or more may be displayed provided that the
associated system pressure is checked available before
each flight.
(Cont’d on next page)
01.29.12HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-09 ECAM Alerts
29-09-09 HYD
G(B)(Y)(B+G)(G+Y)
(B+Y) SYS LO PR
Alert
29-09-09A (Cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Note:
If the Yellow Electric Pump is not
available:
- Pressurize the Yellow Hydraulic
System with:
- A Ground cart, or with
- The Yellow Engine 2 Pump with
the Engine 2 running.
- Replace any action on the YELLOW
ELEC PUMP pb-sw by a similar
action on the Ground Cart or on the
YELLOW ENG 2 PUMP pb-sw in the
following procedure.
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
- BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · AUTO
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
- On the CAPT or the F/O side, move the stick left or right.
- On the F/CTL SD page, check the pairs of spoilersmovement.
- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
12 FEB 12MEL
A320/321MEL/CDL 01.29.13
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-10 Main Hydraulic Power
29-10-01 Engine Driven
Pump
29-10-01A 2 2 Both must be operative.
29-10-02 Engine Driven
Pump
Depressurizatio
n Function
29-10-02A C 2 1 One may be inoperative.
29-10-03 Blue System
Electric Pump
29-10-03A C 1 1 (O) The automatic control may be inoperative provided that the
pump is manually operated.
OPERATING PROCEDURES
DURING PRELIMINARY COCKPIT PREPARATION
- If the blue electric pump continuously runs:
At electrical power supply application:BLUE ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · · · OFF
AFTER ENGINE START
BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . . . . . AUTO
- If the blue electric pump does not automaticallystart:
- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON
- On the HYD SD page, check that the blue hydrauliccircuit pressure is available.
AFTER ENGINE SHUTDOWN
BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . . . . . OFF
01.29.14HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-10 Main Hydraulic
Power
29-10-04 Hydraulic System
Accumulator
29-10-04A No hydraulic
fluid leakage
C 3 0 (M) One or more may be inoperative provided that it is
checked that there is no hydraulic fluid leakage in the
accumulator nitrogen charging circuit.
MAINTENANCE PROCEDURE
Refer to AMM 29-10-00-040-007
29-10-04B Accumulator
deactivated
C 3 0 (M) One or more may be inoperative provided that the
affected accumulator is deactivated.
MAINTENANCE PROCEDURE
Refer to AMM task
29-10-05 Yellow Brake
Accumulator
29-10-05A 1 1 Must be operative.
29-10-07 Engine Pump Fire
Valve
29-10-07A 2 2 Both must be operative.
29-10-08 Hydraulic System
Filter
29-10-08A One LP filter
inoperative
C 8 7 One LP filter may be inoperative.
29-10-08B Reservoir filling
filter inoperative
C 8 7 The reservoir filling filter may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.29.15
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-10 Main Hydraulic Power
29-10-09 Hydraulic Case
Drain Filter
29-10-09A C 3 2 (M) One may be inoperative provided that it is removed.
MAINTENANCE PROCEDURE
Refer to AMM task
29-22 Blue Auxiliary
Hydraulic Power
29-22-01 Ram Air Turbine
29-22-01A 1 1 Must be operative.
29-23 Power Transfer
29-23-01 Power Transfer
Unit (PTU)
29-23-01A C 1 1 (O) PTU may continuously run when set to AUTO provided
that the operation of the PTU in both directions is checked
before the first flight of each day.
(Cont’d on next page)
01.29.16HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-23 Power Transfer
29-23-01 Power Transfer
Unit (PTU)
29-23-01A (cont’d) OPERATING PROCEDURES
AFTER ENGINE START
Check of the PTU operation:
- GREEN ENG 1 PUMP pb-sw . . . . . . . . . . . . . . OFF
- On the HYD SD page, check that the green systempressure is correct.
A correct pressure is 3 000 PSI ( ± 200 PSI).
- Check the PTU arrow indication.
- GREEN ENG 1 PUMP pb-sw . . . . . . . . . . . . . . . On
- PTU pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- YELLOW ENG 2 PUMP pb-sw . . . . . . . . . . . . . OFF
- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
- Let the pressure in the yellow hydraulic systemdecrease to 200 PSI or less.
- If the pressure is not below 200 PSI, the indicationson the HYD SD page will not be displayed.
- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.29.17
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-23 Power Transfer
29-23-01 Power Transfer
Unit (PTU)
29-23-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
- On the HYD SD page, check that the yellow systempressure is correct.
A correct pressure is 3 000 PSI (± 200 PSI).
- Check the PTU arrow indication.
- YELLOW ENG 2 PUMP pb-sw · · · · · · · · · · · · · · · · On
Note:
i. The PTU pressurizes the system to a
nominal value of 3 000 PSI PSI (± 200 PSI),
but if no consumers are operated the
pressure is not constant. The PTU operates
in a cycle which keeps the pressure in the
hydraulic systems between 2 100 PSI and 3
200 PSI.
ii. For passengers comfort, the PTU may beset to OFF during the taxi after landing
provided that both engines hydraulic pumps
are operative and running. The PTU must be
set back to AUTO before leaving the aircraft.
29-24 Yellow Auxiliary
Hydraulic Power
29-24-01 Yellow System
Electric Pump
29-24-01A C 1 0 (O) May be inoperative provided that the associated pb-sw is
set to off.
(Cont’d on next page)
01.29.18HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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29 HYDRAULIC POWER
29-24 Yellow Auxiliary
Hydraulic Power
29-24-01 Yellow System
Electric Pump
29-24-01A (Cont’d) OPERATING PROCEDURES
ON GROUND
- If the pump continuously runs and does not stopwhen set to off:DOORS/CARGO (T12 on 122 VU) C/B · · · · · · · · · Pull
- If unsuccessful:
- Y HYD/ELEC PUMP/NORM (AB 03 on 123 VU) C/B. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
- Y HYD/ELEC/PUMP (AB 06 on 123 VU) C/B. . . Pull
Note:
i. If the pump continuously runs on the
ground, there is a potential overheat
situation.ii. The reset of the C/Bs must be limited
to the time required to open or close
the cargo doors.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.29.19
HYDRAULIC POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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01.29.20HYDRAULIC POWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-00 MAINTENANCE
Message on the
STATUS SD page
30-00-01 ICE DETECT
MAINTENANCE
Message
30-00-01A One inoperative C 1 - ICE DETECT MAINTENANCE message may be displayed
on the STATUS SD page.
30-01 Overhead Panels
30-01-01 ANTI ICE
Overhead Panel
30-01-01-01 ANTI ICE ENG
1(2) pb-sw
FAULT light
30-01-01-01A One inoperative C 2 1 (FD) One may be inoperative provided that the associated
engine anti-ice valve is considered inoperative in the
closed position.
Refer to Item 30-21-01A Engine Anti-Ice Valve
30-01-01-01B One or both
inoperative
C 2 0 (FD) One or both may be inoperative provided that the
associated engine anti-ice valve is considered inoperative
in the open position.
Refer to Item 30-21-01 Engine Anti-Ice Valve
30-01-01-02 ANTI ICE ENG
1(2) pb-sw ON
light
30-01-01-02A C 2 0 One or both may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL
01.30.01ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-01 Overhead Panels
30-01-01 ANTI ICE
Overhead Panel
30-01-01-03 ANTI ICE WING
pb-sw FAULT
light
30-01-01-03A C 1 0 (O) May be inoperative provided that the anti-ice “arrow”
symbols are operative on the BLEED SD page .
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check of the anti-ice "arrow" symbol:
- Make sure that the engine bleed air supply systemis available.
- ANTI ICE WING pb-sw . . . . . . . . . . . . . . . . . . . . ON
- On the BLEED SD page, check that the anti-ice"arrow" symbols are displayed amber anddisappear after 30 s.
- ANTI ICE WING pb-sw . . . . . . . . . . . . . . . . . . . . Off
30-01-01-03B C 1 0 (M)(FD) May be inoperative provided that the wing anti-ice control
valves are deactivated in the closed position and
considered inoperative.
Refer to Item 30-11-01 Wing Anti-Ice Control Valve
MAINTENANCE PROCEDURE
Refer to AMM 30-11-00-040-002
30-01-01-04 ANTI ICE WING
pb-sw ON light
30-01-01-04A C 1 0 May be inoperative.
01.30.02ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-01 Overhead Panels
30-01-02 WIPER
Overhead Panel
30-01-02-01 Wiper High
Speed Function
(FAST Position)
30-01-02-01A C 2 0 One or both may be inoperative provided that the
associated low speed function is operative.
30-01-02-02 Wiper Low
Speed Function
(SLOW Position)
30-01-02-02A C 2 0 One or both may be inoperative.
30-07 Indications on the
BLEED SD page
30-07-01 ANTI ICE
Indication on the
BLEED SD page
30-07-01A C 2 0 One or both may be inoperative.
30-07-02 Arrow Indication
on the BLEED
SD page
30-07-02A C 2 0 One or both may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL
01.30.03ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-11 Wing Ice Protection
30-11-01 Wing Anti-Ice
Control Valve
30-11-01A Inoperative in
the open
position
C 2 1 (O)(M)
(FD)
The RH valve may be inoperative in the open position
provided that the associated ECAM procedure is applied.
OPERATING PROCEDURES (A321)
FLIGHT PREPARATION/LIMITATIONS
Flight planning:
Increase fuel consumption by:
Zp(ft) 5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000
Fuel penalties 4.5% 4.0% 5.0% 4.0% 4.0% 3.5% 3.0% 2.5%
Single engine cruise:
Decrease drift down ceilings by:
600 ft when OAT £ ISA2 300 ft when OAT > ISA
Approach climb performance:
- When the engine bleed air supply system isclosed:No penalty.
- When the engine bleed air supply system isopen:Decrease maximum climb limiting weight by:1 100 kg when OAT £ ISA + 5° C4 500 kg when OAT > ISA + 5° C
DURING COCKPIT PREPARATION
- After application of the maintenance procedure:
On the BLEED SD page, check that the anti-ice arrowsymbol is displayed.The anti-ice arrow symbol may be displayed amber or green.The WING ANTI ICE L(R) HI PR alert must not bedisplayed on the EWD.
(Cont’d on next page)
01.30.04ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-11 Wing Ice
Protection
30-11-01 Wing Anti-Ice
Control Valve
30-11-01A (Cont’d) OPERATING PROCEDURES (A321) (Cont’d)
BEFORE ENGINE START
- Maintain the X BLEED selector at SHUT before enginestart when the APU bleed is used.
- Start the engine 1.
- Maintain the X BLEED selector at SHUT during thestart of engine 1.
- Use the CROSS BLEED ENGINE START (Refer toFCOM/PRO-SLP-70 Cross Bleed Engine Start)
- Apply the procedure associated with the WING ANTIICE R VALVE OPEN alert displayed on the EWD.
AFTER TAKEOFF
- When above 1 500 ft: Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.
IN FLIGHT
- In the case of failure of a Bleed Air Supply System:
PACK (affected side) pb-sw· · · · · · · · · · · · · · · · · · OFF
AFTER LANDING
- Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.
12 FEB 12MEL
A320/321MEL/CDL
01.30.05ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-11 Wing Ice Protection
30-11-01 Wing Anti-Ice
Control Valve
30-11-01A (cont’d) OPERATING PROCEDURES (A320)
FLIGHT PREPARATION/LIMITATIONS
Flight planning:
Increase fuel consumption by:
Zp(ft) 5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000
Fuel penalties 4.5% 4.5% 6.0% 4.5% 3.5% 2.5% 2.5% 2.5%
Single engine cruise:
Decrease drift down ceilings by:
1100 ft when OAT £ ISA4500 ft when OAT > ISA
Approach climb performance:
- When the engine bleed air supply system isclosed:No penalty.
- When the engine bleed air supply system isopen:Decrease maximum climb limiting weight by:800 kg when OAT £ ISA + 5° C4 900 kg when OAT > ISA + 5° C
DURING COCKPIT PREPARATION
- After application of the maintenance procedure:
On the BLEED SD page, check that the anti-ice arrowsymbol is displayed.
The anti-ice arrow symbol may be displayed amber or green.The WING ANTI ICE L(R) HI PR alert must not bedisplayed on the EWD.
(Cont’d on next page)
01.30.06ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-11 Wing Ice
Protection
30-11-01 Wing Anti-Ice
Control Valve
30-11-01A (cont’d) OPERATING PROCEDURES (A320) (cont’d)
BEFORE ENGINE START
- Maintain the X BLEED selector at SHUT before enginestart when the APU bleed is used.
- Start the engine 1.
- Maintain the X BLEED selector at SHUT during thestart of engine 1.
- Use the CROSS BLEED ENGINE START (Refer toFCOM/PRO-SLP-70 Cross Bleed Engine Start)
- Apply the procedure associated with the WING ANTIICE R VALVE OPEN alert displayed on the EWD.
AFTER TAKEOFF
- When above 1 500 ft: Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.
IN FLIGHT
- In the case of failure of a Bleed Air Supply System:
PACK (affected side) pb-sw· · · · · · · · · · · · · · · · · · OFF
AFTER LANDING
- Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.
MAINTENANCE PROCEDURE
Refer to AMM 30-11-00-040-004
12 FEB 12MEL
A320/321MEL/CDL
01.30.07ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-11 Wing Ice Protection
30-11-01 Wing Anti-Ice
Control Valve
30-11-01B Inoperative in
the closed
position
C 2 0 (M)(FD)One or both may be inoperative in the closed position
provided tha the aircraft is not operated in known or
forecast icing conditions.
MAINTENANCE PROCEDURE
Refer to AMM 30-11-00-040-001
30-21 Engine Air Intake Ice
Protection
30-21-01 Engine Anti-Ice
Valve
30-21-01A Inoperative inthe closed
position
C 2 1 (M)(FD)One may be inoperative in the closed position providedthat the aircraft is not operated in known or forecast icing
conditions.
MAINTENANCE PROCEDURE
Refer to AMM 30-21-00-040-001
01.30.08ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-21 Engine Air Intake
Ice Protection
30-21-01 Engine Anti-Ice
Valve
30-21-01B Inoperative in
the open
position
C 2 0 (O)(M)
(FD)
One or both may be inoperative in the open position
provided that the Flight Manual performance penalties are
applied.
OPERATING PROCEDURES (A321)
GENERAL INFORMATION
An higher idle speed is set on both engines when an
engine anti-ice valve is inoperative in the open position.
FLIGHT PREPARATION/LIMITATIONS
Note:
i. For performance calculations
request Modified Tailored Takeoff
and Landing charts (MTTL) from
FPE through Flight Dispatch or usethe following penalties for takeoff
and landing performance
determination if MTTL charts are not
available.
ii. Performance penalties apply
whatever one or both valves are
inoperative.
Takeoff performance:
Perform the takeoff using full thrust (TOGA).
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL
01.30.09ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-21 Engine Air Intake Ice
Protection
30-21-01 Engine Anti-Ice
Valve
30-21-01B (Cont’d) OPERATING PROCEDURES (A321) (Cont’d)
Apply the following reductions on the MTOW and the
speeds :
OAT(°C) £ISA+10°C >ISA+10°C
Weight decrement (kg) 900 5100
V1, VR and V2 decrement (kg) 1 5
Flight planning:
Increase fuel consumption by:
Zp (ft) 2 Valves blocked OPEN 1 Valve blocked OPEN
5 000 7.0% 3.5%
10 000 5.0% 2.5%
15 000 5.5% 3.0%
20 000 4.0% 2.0%
25 000 4.0% 2.0%
30 000 3.5% 2.0%
35 000 3.5% 2.0%
40 000 3.5% 2.0%
Single engine cruise:
Decrease drift down ceilings by:
300 ft when OAT£ ISA + 5°C
2 400 ft when OAT > ISA + 5°C
(Cont’d on next page)
01.30.10ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-21 Engine Air Intake
Ice Protection
30-21-01 Engine Anti-Ice
Valve
30-21-01B (Cont’d) OPERATING PROCEDURES (A321) (Cont’d)
Approach climb performance:
Decrease maximum climb limiting weight by:700 kg when OAT £ ISA + 10 °C
5 900 kg when OAT > ISA + 10°C
DURING COCKPIT PREPARATION
ANTI ICE ENG (affected) pb-sw. . . . . . . . . . . . . . . ON
AFTER ENGINE START
The FADEC commands the continuous ignition on the
affected engine.
OPERATING PROCEDURES (A320)
GENERAL INFORMATION
An higher idle speed is set on both engines when an
engine anti-ice valve is inoperative in the open position.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL
01.30.11ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-21 Engine Air Intake Ice
Protection
30-21-01 Engine Anti-Ice
Valve
30-21-01B (Cont’d) OPERATING PROCEDURES (A320) (Cont’d)
FLIGHT PREPARATION/LIMITATIONS
Note:
i. For performance calculations request
Modified Tailored Takeoff and Landing
charts (MTTL) from FPE through Flight
Dispatch or use the following penalties for
takeoff and landing performance
determination if MTTL charts are not
available.
ii. Performance penalties apply whatever oneor both valves are inoperative.
Takeoff performance:
Perform the takeoff using full thrust (TOGA).
Apply the following reductions on the MTOW and the
speeds :
OAT(°C) £ISA+10°C ISA+10°C< OAT£ ISA+20°C >ISA+20°C
Weight
decrement
(kg)
1100 2000 3200
V1, VR and
V2
decrement
(kg)
1 1 2
(Cont’d on next page)
01.30.12ICE AND RAINPROTECTION
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-21 Engine Air Intake
Ice Protection
30-21-01 Engine Anti-Ice
Valve
30-21-01B (Cont’d) OPERATING PROCEDURES (A320) (Cont’d)
Flight planning:
Increase fuel consumption by:
Zp (ft) 2 Valves blocked OPEN 1 Valve blocked OPEN
5 000 5.5% 3.0%
10 000 4.5% 2.5%
15 000 4.0% 2.0%
20 000 3.0% 1.5%
25 000 3.0% 1.5%
30 000 2.0% 1.0%
35 000 2.0% 1.0%
40 000 2.0% 1.0%
Single engine cruise:
Decrease drift down ceilings by:
400 ft when OAT£ ISA + 5°C
3 700 ft when OAT > ISA + 5°C
Approach climb performance:
Decrease maximum climb limiting weight by:
300 kg when OAT £ ISA + 10 °C
4 400 kg when OAT > ISA + 10°C
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL
01.30.13ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-21 Engine Air Intake Ice
Protection
30-21-01 Engine Anti-Ice
Valve
30-21-01B (Cont’d) OPERATING PROCEDURES (A320) (Cont’d)
DURING COCKPIT PREPARATION
ANTI ICE ENG (affected) pb-sw. . . . . . . . . . . . . . . ON
AFTER ENGINE START
The FADEC commands the continuous ignition on the
affected engine.
MAINTENANCE PROCEDURE
Refer to AMM 30-21-00-040-002
30-31 Probe Ice Protection
30-31-01 Probe Heat
Computer (PHC)
30-31-01A Associated
probe heating
operative
C 3 2 (M) One may be inoperative provided that the associated
probe heating is checked operative before each flight.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-001
01.30.14ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-31 Probe Ice
Protection
30-31-01 Probe Heat
Computer (PHC)
30-31-01B F/O PHC
inoperative
B 3 2 (O)(M) The F/O PHC may be inoperative provided that the ADRs,
heaters and failure alerts associated with the operative
computers are checked operative every day.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
AIR DATA selector· · · · · · · · · · · · · · · · · · · · · · · · F/O 3
IN FLIGHT
- If icing conditions are encountered:
ADR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
CAUTION
When ADR 2 is set to OFF, takeoff in
CONF 1+F is not permitted.
The ADR 2 pb-sw must remain set to OFF for the
remainder of the flight.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-005
12 FEB 12MEL
A320/321MEL/CDL
01.30.15ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-31 Probe Ice Protection
30-31-01 Probe Heat
Computer (PHC)
30-31-01C STBY PHC
inoperative
C 3 2 (M)(FD)The STBY PHC may be inoperative provided that:
1) The ADRs, heaters and failure alerts associated withthe operative computers are checked operative everyday, and
2) The aircraft is not operated in visible moisture or inknown or forecast icing conditions, and
3) The OAT at the departure airport is above 5 °C whenthe taxiway or the runway are contaminated with water or slush.
MAINTENANCE PROCEDURE
AMM 30-31-00-040-005
30-31-02 Pitot Heater
30-31-02A F/O pitot heater
inoperative
B 3 2 (O)(M)
(FD)
The F/O pitot heater may be inoperative provided that the
ADRs, heaters and failure alerts associated with the CAPTand the STBY probes (pitot, static, AOA, TAT) are
checked operative every day.
OPERATING PROCEDURES
Refer to Operations Procedures 30-31-01B Probe Heat
Computer
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-002
01.30.16ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-31 Probe Ice
Protection
30-31-02 Pitot Heater
30-31-02B CAPT pitot
heater
inoperative
B 3 2 (M)(FD)The CAPT pitot heater may be inoperative provided that:
1) The ADRs, heaters and failure alerts associated withthe F/O and the STBY probes (pitot, static, AOA, TAT)are checked operative every day, and
2) The aircraft is not operated in visible moisture or inknown or forecast icing conditions.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-002
30-31-02C STBY pitot
heater
inoperative
B 3 2 (M)(FD)The STBY pitot heater may be inoperative provided that:
1) The ADRs, heaters and failure alerts associated with
the CAPT and the F/O probes (pitot, static, AOA, TAT)are checked operative every day, and
2) The aircraft is not operated in visible moisture or inknown or forecast icing conditions.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-002
12 FEB 12MEL
A320/321MEL/CDL
01.30.17ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-31 Probe Ice Protection
30-31-03 Static Ports
Heater
30-31-03A One STBY
static port
heater
inoperative
C 6 5 One STBY static ports heater may be inoperative.
30-31-03B Both STBY
static port
heater
inoperative
C 6 4 (M)(FD)Both STBY static ports heaters may be inoperative
provided that:
1) The ADRs, heaters and failure alerts associated withthe CAPT and the F/O probes (pitot, static, AOA, TAT)are checked operative every day, and
2) The OAT at the departure airport is above 5 °C whenthe runway is contaminated with water or slush.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-003
30-31-03C One or bothF/O static port
heater
inoperative
C 6 5 (O) One F/O static port heaters may be inoperative providedthat the ADRs, heaters and failure alerts associated with
the CAPT and the STBY probes (pitot, static, AOA, TAT)
are checked operative every day.
OPERATING PROCEDURES
Refer to Operations Procedures 30-31-01B Probe Heat
Computer
30-31-03D One or both
CAPT static
port heater
inoperative
C 6 5 (M)(FD)One CAPT static port heaters may be inoperative provided
that:
1) The ADRs, heaters and failure alerts associated with
the F/O and the STBY probes (pitot, static, AOA, TAT)are checked operative every day, and
2) The OAT at the departure airport is above 5 °C whenthe runway is contaminated with water or slush.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-003
01.30.18ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-31 Probe Ice
Protection
30-31-04 Angle of Attack
(AOA) Probes
Heating
30-31-04A F/O AOA
inoperative
C 3 2 (O)(M)
(FD)
The F/O AOA probes heating may be inoperative provided
that the ADRs, heaters and failure alerts associated with
the CAPT and the STBY probes (pitot, static, AOA, TAT)
are checked operative every day.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability CAT II, if icing conditions areencountered during the flight.
RVSM operation are not permitted.
DURING COCKPIT PREPARATION
AIR DATA selector· · · · · · · · · · · · · · · · · · · · · · · · F/O 3
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-004
30-31-04B STBY AOA
inoperative
C 3 2 (O)(M) The STBY AOA probes heating may be inoperative
provided that the ADRs, heaters and failure alerts
associated with the CAPT and the F/O probes (pitot, static,
AOA, TAT) are checked operative every day
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-004
12 FEB 12MEL
A320/321MEL/CDL
01.30.19ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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30 ICE AND RAIN PROTECTION
30-31 Probe Ice Protection
30-31-04 Angle of Attack
(AOA) Probes
Heating
30-31-04C CAPT AOA
inoperative
C 3 2 (O)(M)
(FD)
The CAPT AOA probes heating may be inoperative
provided that:
1) The ADRs, heaters and failure alerts associated with
the F/O and the STBY probes (pitot, static, AOA, TAT)are checked operative every day, and
2) The aircraft is not operated in visible moisture or inknown or forecast icing conditions.
OPERATING PROCEDURES
Landing capability is CAT II.
MAINTENANCE PROCEDURE
Refer to AMM 30-31-00-040-004
30-31-05 TAT Probes
Heating
30-31-05A One inoperative C 2 1 One may be inoperative.
30-31-05B Both
inoperative
C 2 0 (FD) Both may be inoperative provided that the aircraft is not
operated in visible moisture or in known or forecast icing
conditions.
01.30.20ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-42 Windshield Anti-
Icing and
Defogging
30-42-01 Window Heat
Computer
30-42-01A C 2 1 (O)(M)
(FD)
One may be inoperative provided that:
1) The aircraft is not operated in known or forecast icing
conditions, and2) All heaters and failure alerts on the front and sliding
windows associated with the operative computer arechecked operative every day.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I when the PF sideis inoperative.
Landing capability is CAT II when the PNF side isinoperative.
MAINTENANCE PROCEDURE
Refer to AMM 30-42-00-040-001
12 FEB 12MEL
A320/321MEL/CDL
01.30.21ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-42 Windshield Anti-Icing
and Defogging
30-42-02 Fixed Lateral
Window and
Sliding Window
Heating
30-42-02A C 4 0 One or more may be inoperative.
30-42-03 Windshield
Heating
30-42-03A C 2 1 (O)(FD) One may be inoperative provided that the aircraft is not
operated in known or forecast icing conditions.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I when the PF sideis inoperative.
Landing capability is CAT II when the PNF side is
inoperative.
30-42-04 PROBES/
WINDOW HEAT
pb-sw AUTO
Control
30-42-04A C 1 0 Automatic control may be inoperative provided that the
PROBES/WINDOW HEAT system is manually selected.
30-42-05 PROBES/
WINDOW HEAT
pb-sw ON light
30-42-05A C 1 0 May be inoperative provided that PROBES/WINDOW
HEATautomatic system is operative.
01.30.22ICE AND RAINPROTECTION
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-45 Windshield Rain
Protection
30-45-01 Windshield
Wiper
30-45-01A One inoperative
on the PNF side
A 2 1 One may be inoperative on the PNF side for three flights.
30-45-01B One inoperative
on the PNF side
C 2 0 (O)(FD) One or both may be inoperative provided that:
1) The aircraft is not operated in precipitation withindeparture and arrival areas, and
2) The approach minima do not require their use.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 1 when the wiper and
the rain repellent are inoperative or deactivated on the PF
side.
30-45-01C Rain repellentsystem
operative
B 2 1 One may be inoperative provided that the associated rainrepellent system is installed and operative.
30-45-02 Windshield
Wiper PARK
Function
30-45-02A One or both
inoperative
C 2 0 One or both may be inoperative provided that the
associated wipers can be positioned in a location that will
not obstruct forward vision.
30-45-02B One or both
inoperative andremoved
2 0 (M) One or both may be inoperative provided that the
associated wipers are removed.
Refer to Item 30-45-01 Windshield Wiper
MAINTENANCE PROCEDURE
Refer to AMM 30-45-00-040-003
12 FEB 12MEL
A320/321MEL/CDL
01.30.23ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-45 Windshield Rain
Protection
30-45-03 Rain Repellent
System
30-45-03A C 2 0 One or both may be inoperative.
Note:
No entry in the logbook is required whenit is installed but intentionally
deactivated.
30-71 Waste Water Ice
Protection
30-71-01 Waste Water
Drain Mast
Heating System
30-71-01A C 2 0 (M)(FD) One or both may be inoperative provided that:
1) The associated galleys and lavatories are not used,and
2) The associated lavatory water supplies are closed.
MAINTENANCE PROCEDURE
Refer to AMM 30-71-00-040-001
30-71-02 Waste Water
Drain Line Ice
Protection
System
30-71-02A C 1 0 May be inoperative.
01.30.24ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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30 ICE AND RAIN PROTECTION
30-81 Ice Detection
30-81-01 Ice Detection
System
30-81-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
IN FLIGHT
The presence of ice in the vicinity of the windshield and on
the wipers is periodically checked.
30-81-02 External Visual
Icing Indicator
30-81-02A C 1 0 The presence of ice in the vicinity of the winsheild and on
the wipers is periodically checked.
30-81-03 Lighting of
External Visual
Icing Indicator
30-81-03A C 1 0 (O)(FD) May be inoperative.
IN FLIGHT
- If icing conditions are expected during nightoperations:Refer to FCOM limitation for Icing Conditions
* * *
12 FEB 12MEL
A320/321MEL/CDL
01.30.25ICE AND RAIN
PROTECTION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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01.30.26ICE AND RAINPROTECTION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDIG
SYSTEMS
31-00 MAINTENANCE
Message on the
STATUS SD page
31-00-01 QAR
MAINTENANCE
Message
31-00-01A C 1 - QAR MAINTENANCE message may be displayed on the
STATUS SD page.
31-00-02 ACMS
MAINTENANCE
Message
31-00-02A C 1 - ACMS MAINTENANCE message may be displayed on the
STATUS SD page.
31-00-03 DAR
MAINTENANCE
Message
31-00-03A C 1 - DAR MAINTENANCE message may be displayed on the
STATUS SD page.
31-00-04 CFDIU
MAINTENANCE
Message
31-00-04 C 1 - CFDIU MAINTENANCE message may be displayed on the
STATUS SD page.
31-00-05 DMC 1/3
MAINTENANCE
Message
31-00-05A C 2 - DMC 1/3 MAINTENANCE message may be displayed on
the STATUS SD page provided that the DMC 2/3
MAINTENANCE message is not displayed on the STATUS
SD page.
12 FEB 12MEL
A320/321MEL/CDL
01.31.01INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-00 MAINTENANCE
Message on the
STATUS SD page
31-00-06 DMC 2/3
MAINTENANCE
Message
31-00-06A C 2 - DMC 2/3 MAINTENANCE message may be displayed on
the STATUS SD page.
31-05 Indications on the
Primary Flight Display
(PFD)
31-05-01 AP Related
Indications on the
FMA
31-05-01A Refer to MEL Item 22-05-01 AP Related Indications on theFMA.
31-05-02 A/THR Related
Indications on the
FMA
31-05-03A Refer to MEL Item 22-05-03 Approach and Landing
Capabilities on the FMA.
31-05-04 Special Messages
on the FMA
31-05-04A Refer to MEL Item 22-05-04 Special Messages on theFMA.
01.31.02INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-05 Indications on the
Primary Flight
Display (PFD)
31-05-05 Actual Airspeed
Reference Line
and Scale
Indications on the
PFD
31-05-05A Refer to MEL Item 34-05-01 Actual Airspeed Reference
Line and Scale Indication on the PFD
31-05-06 Mach Number
Indication on the
PFD
31-05-06a Refer to MEL Item 34-05-02 Mach Number Indication on
the PFD.
31-05-07 VMO/MMO
CharacteristicSpeed Indication
on the PFD
31-05-07A Refer to MEL Item 34-05-03 VMO/MMO Characteristic
Speed Indication on the PFD.
31-05-08 Altitude Indication
on the PFD
31-05-08A Refer to MEL Item 34-05-04 Altitude Indication on the
PFD.
31-05-09 Vertical SpeedIndication on the
PFD
31-05-09A Refer to MEL Item 34-05-06 Vertical Speed in Inertial
Mode Indication on the PFD
12 FEB 12MEL
A320/321MEL/CDL
01.31.03INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-05 Indications on the
Primary Flight Display
(PFD)
31-05-10 Other Air Data
Related
Indications on the
PFD
31-05-10A Refer to MEL Item 34-05-07 Other Air Data Related
Indications on the PFD.
31-05-11 Attitude Indication
on the PFD
31-05-11A Refer to MEL Item 34-05-08 Attitude Indication on the
PFD.
31-05-12 Heading Indication
on the PFD
31-05-12A Refer to MEL Item 34-05-09 Heading Indication on thePFD.
31-06 Indications on the
Navigation Display
(ND)
31-06-01 Ground Speed
Indication on the
ND
31-06-01A Refer to MEL Item 34-06-01 Ground Speed Indication on
the ND.
31-06-02 True Air Speed
Indication on the
ND
31-06-02A Refer to MEL Item 34-06-02 True Air Speed Indication on
the ND.
01.31.04INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-06 Indications on the
Navigation Display
(ND)
31-06-04 Heading Indication
on the ND
31-06-04A Refer to MEL Item 34-06-04 Heading Indication on the ND.
31-06-05 Position (Aircraft
Symbol) Indication
on the ND
31-06-05A Refer to MEL Item 34-06-05 Position (Aircraft Symbol)
Indication on the ND.
31-06-06 Navigation Station
Information on the
ND
31-06-06A Refer to MEL Item 34-06-06 Radio Navaids Indications on
the ND.
31-06-07 Chrono Indication
on the ND
31-06-07A Refer to MEL Item 34-06-07 Chrono Indication on the ND.
31-07 Indications on the
System Display
(SD)
31-07-01 Indications on the
System Display
pages
31-07-01A Refer to corresponding item in the associated ATA
chapter.
12 FEB 12MEL
A320/321MEL/CDL
01.31.05INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-07 Indications on the
System Display (SD)
31-07-02 Permanent Data
(TAT, SAT, ISA,
GLOAD - ALT SEL,
UTC, GW)
Indications on the
SD
31-07-02A C 7 1 (O) TAT indication must be available.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check that the TAT value is operative on the SD
permanent data.
- If the TAT value is not operative:
Check that the TAT value is available through the ADR3.
Note:
Use the AIR DATA SWITCHING
selector to display temporarily the TAT
value on the SD.
IN FLIGHT
- If needed:
The TAT value may be displayed through the sameaction on the AIR DATA SWITCHING selector.
31-08 Indications on the
Engine Warning
Display (EWD)
31-08-01 Engine Parameter
Indications on the
EWD
31-08-01A Refer to MEL item 77-08
01.31.06INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-08 Indications on the
Engine Warning
Display (EWD)
31-08-02 Fuel On Board
(FOB) Indication
on the EWD
31-08-02A Refer to MEL Item 28-07-01-01 Fuel On Board (FOB)
Indication on the FUEL SD page.
31-08-03 MEMO Messages
on the EWD
31-08-03A C 7 0 One or more may be inoperative.
31-08-04 Slats/Flaps
Position
Indications on the
EWD
31-08-04A Refer to MEL Item 27-08-01 Flap Position Indication on theEWD.
Refer to MEL Item 27-08-02 Slat Position Indication on the
EWD.
Note:
Apply both MEL Items.
31-20 Independent
Instruments
31-20-01 Electrical Clock
Indicator
31-20-01A C 1 0 (O) May be inoperative provided that:
1) The UTC indication from the CFDIU is operative on thepermanent data of the SD, and
2) A chrono indication is operative on at least one ND.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL
01.31.07INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-20 Independent
Instruments
31-20-01 Electrical Clock
Indicator
31-20-01A (Cont’d) OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- After any electrical power interruption resulting inthe loss of the UTC on the SD:Initialize the UTC and the date using the MCDU: Refer to FCOM /DSC-45-20-GMT/Date Initialization.
31-30 Centralized Fault
Display System
(CFDS) and Data
Recording System
31-30-01 Centralized Fault
Display System
(CFDS)
31-30-01A C 1 0 May be inoperative.
31-30-02 Digital AIDS
Recorder (DAR)
31-30-02A Refer to MEL Item 31-00-03 DAR MAINTENANCE
Message
Note:
Failure of DAR is indicated by a
MAINTENANCE message on the
STATUS SD page.
01.31.08INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-30 Centralized Fault
Display System
(CFDS) and Data
Recording System
31-30-03 Digital Flight Data
Recorder (DFDR)
31-30-03A A 1 0 May be inoperative provided:
1) Cockpit voice Recorder (VCR) is operative,
2) Airplane is not dispatched from JED, RUH, DMM,MED, and
3) Repair are made within 3 flight days.
31-30-04 Data Management
Unit (DMU) part of
Flight Data
Interface and
Management
Unit(FDIMU)
31-30-04 C 1 0 May be inoperative.
31-30-05 Flight Data
Interface Unit
(FDIU)
31-30-05A A 1 0 Note:
If FDIU is inoperative the DFDR and the
QAR are inoperative.
Refer to Item 31-30-03 Digital Flight
Data Recorder (DFDR), and
Refer to Item 31-30-06 Quick AccessRecorder (QAR)
12 FEB 12MEL
A320/321MEL/CDL
01.31.09INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-30 Centralized Fault
Display System
(CFDS) and Data
Recording System
31-30-06 Quick Access
Recorder (QAR)
31-30-06A Refer to Item 31-00-01 QAR MAINTENANCE Message
Note:
Failure of QAR is indicated by a
MAINTENANCE message on the
STATUS SD page.
31-30-07 Printer
31-30-07A C 1 0 May be inoperative.
31-38 Up and Down DataLoading System
Acquisition/Interface
and Equipment
31-38-01 DATA LOADING
selector
31-38-01A C 1 0 May be inoperative.
31-38-02 Data Loading
Routing Box
(DLRB)
31-38-02A C 1 0 May be inoperative.
01.31.10INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-38 Up and Down Data
Loading System
Acquisition/Interfa
ce and Equipment
31-38-03 Multipurpose Disk
Drive Unit (MDDU)
31-38-03A C 1 0 May be inoperative.
31-53 Flight Warning
Computer (FWC)
31-53-01 Flight Warning
Computer (FWC)
31-53-01A C 2 1 (O) FWC 2 may be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
31-53-02 MASTER CAUT
Cancel Function
31-53-02A C 2 1 One may be inoperative.
31-53-03 MASTER WARN
Cancel Function
31-53-03A C 2 1 One may be inoperative.
31-53-04 MASTER CAUT
light
31-53-04A C 2 1 One may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL
01.31.11INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-53-05 MASTER WARN
light
31-53-05A C 2 1 One may be inoperative.
31-53-06 Altitude Alert
31-53-06A B 2 1 (O) One altitude alert function May be ioperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
- When both altitude alert functions are inoperative:
RVSM operations are not permitted.
31-53-06B A 2 0 (O)(FD) B oth altitude alert functions may be inoperative provided:
1) Autopilot with altitude hold is operative,
2) Flight is not conducted within RVSM airspace,
3) Enroute operations do not require its use, and
4) Repairs are made within one flight days.
OPERATING PROCEDURES:
1. Flight crew must be aware that the usual alerts for altitude deviations will not occur.
2. PM should call out approaching and departingassigned altitudes.
3. RVSM operations are not allowed.
01.31.12INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-55 System Data
Acquisition
Concentrator
(SDAC)
31-55-01 System Data
Acquisition
Concentrator
(SDAC)
31-55-01A C 2 1 SDAC 2 may be inoperative.
31-56 ECAM Control
Panel (ECP)
31-56-01 System Page
Manual Call pb on
the ECP
31-56-01A C 11 0 One or more may be inoperative.
31-56-02 ALL pb on the
ECP
31-56-02A 1 1 Must be operative.
12 FEB 12MEL
A320/321MEL/CDL
01.31.13INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-56 ECAM Control Panel
(ECP)
31-56-03 CLR pb on the
ECP
31-56-03A C 2 1 One may be inoperative.
31-56-04 EMER CANC pb
on the ECP
31-56-04A 1 1 Must be operative.
31-56-05 RCL pb on the
ECP
31-56-05A 1 1 Must be operative.
31-56-06 STS pb on the
ECP
31-56-06A C 1 0 Must be operative.
31-56-07 T.O CONFIG pb on
the ECP
31-56-07A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
BEFORE TAKEOFF
Check that the aircraft is in the correct takeoff
configuration:
- FLAPS/SLATS· · · · · · · · · · · · · · · · · · · · · · · · · CHECK
(Cont’d on next page)
01.31.14INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-56 ECAM Control
Panel (ECP)
31-56-07 T.O CONFIG pb on
the ECP
31-56-07A (Cont’d) OPERATING PROCEDURES (Cont’d)
- On EWD, check that the FLAPS position corresponds
to the position inserted in the MCDU PERF TAKE OFFPage.
- PITCH TRIM· · · · · · · · · · · · · · · · · · · · · · · · · · · CHECK
- Check that the selected pitch trim is in the green bandof the pitch trim wheel and corresponds to the valueinserted in the MCDU PERF TAKE OFF Page.
- RUDDER TRIM · · · · · · · · · · · · · · · · · · · CHECK ZERO
- SPEED BRAKE leve · · · · · · · · · · · · · · · · CHECK RET
- SIDESTICK PRIORITY light · · · · · · · CHECK NO RED
- On the WHEEL SD page, check that the brakes
temperature is below 300 °C.
- DOORS · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · CHECK
- On the DOOR/OXY SD page, check that all doors areindicated closed.
- Deselect the DOOR/OXY SD page after the check.
12 FEB 12MEL
A320/321MEL/CDL
01.31.15INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-62 Display Management
Computer (DMC)
31-62-01 DMC 1
31-62-01B C 1 0 (O) May be inoperative provided that:
1) The DMC 2 and DMC 3 are operative, and
2) The ISIS airspeed function is operative, and
3) The ISIS altitude indication is operative, and
4) The ISIS attitude function is operative, and
5) The standby compass is operative, and
6) The EIS DMC SWITCHING selector is set to CAPT 3.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- In the case of multiple undue ECAM alerts concerningENG 1(2) N1(N2) (EGT)(FF) OVER LIMITOr
ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCYOr NAV ATT(ALT1)(HDG) DISCREPANCYOr NAV FM/GPS POS DISAGREEOr FUEL F.USED/FOB DISAGREEOr MINIMUM or HUNDRED ABOVE callouts, possiblyassociated with EFIS red flags, apply the belowprocedure:
- Crosscheck the affected parameters on the EWD,PFD, ND, or on the related SD page to confirm that
the alerts are undue.- EIS DMC SWITCHING selector . . . . . . . . . . NORM
(Cont’d on next page)
01.31.16INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-62 Display
Management
Computer (DMC)
31-62-01 DMC 1
31-62-01B (Cont’d) OPERATING PROCEDURES (Cont’d)
Note:
CAPT PFD and ND ae lost when EIS
DMC SWITCHING selector is set to
NORM.
- If the undue ECAM alerts stop:
- Pull EIS/DMC3/SPLY (121 VU Q09) C/B andEIS/DMC3/STBY/SPLY (49 VU E10) C/B for morethan 5 s and push them back.
- EIS DMC SWITCHINGselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . CAPT 3
- If the undue ECAM alerts continue:
- EIS DMC SWITCHING selector. . . . . . . . . . CAPT 3
- Wait for CAPT PFD and ND recovery.
- Pull EIS/DMC2/SPLY (121 VU Q08) C/B for morethan 5 s and push it back.
12 FEB 12MEL
A320/321MEL/CDL
01.31.17INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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31 INDICATING/RECORDING
SYSTEMS
31-62 Display Management
Computer (DMC)
31-62-02 DMC 2
31-62-02A C 1 0 (O)(M) May be inoperative provided that:
1) The DMC 1 and DMC 3 are operative, and
2) The ISIS airspeed function is operative, and
3) The ISIS altitude indication is operative, and
4) The ISIS attitude function is operative, and
5) The standby compass is operative, and
6) The EIS DMC SWITCHING selector is set to F/O 3,and
7) The AC ESS FEED control is checked operative everyday, and
8) The AC ESS FEED pb-sw FAULT light is checkedoperative every day.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- In the case of multiple undue ECAM alerts concerningENG 1(2) N1(N2) (EGT)(FF) OVER LIMITOr ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCYOr NAV ATT(ALT1)(HDG) DISCREPANCYOr NAV FM/GPS POS DISAGREEOr FUEL F.USED/FOB DISAGREEOr MINIMUM or HUNDRED ABOVE callouts, possiblyassociated with EFIS red flags, apply the belowprocedure:
- Crosscheck the affected parameters on the EWD,PFD, ND, or on the related SD page to confirm thatthe alerts are undue.
- EIS DMC SWITCHING selector . . . . . . . . . . NORM
(Cont’d on next page)
01.31.18INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-62 Display
Management
Computer (DMC)
31-62-02 DMC 2
31-62-02A OPERATING PROCEDURES (Cont’d)
Note:
CAPT PFD and ND ae lost when EIS
DMC SWITCHING selector is set to
NORM.
- If the undue ECAM alerts stop:
- Pull EIS/DMC3/SPLY (121 VU Q09) C/B andEIS/DMC3/STBY/SPLY (49 VU E10) C/B for morethan 5 s and push them back.
- EIS DMC SWITCHINGselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F/O 3
- If the undue ECAM alerts continue:
- EIS DMC SWITCHING selector . . . . . . . . . . . F/O 3
- Wait for CAPT PFD and ND recovery.
- Pull EIS/DMC2/SPLY (49 VU E11) C/B for morethan 5 s and push it back.
MAINTENANCE PROCEDURE
Refer to AMM 31-68-00-040-005
31-62-03 DMC 3
31-62-03B C 1 0 (O) May be inoperative provided that:
1) The DMC 1 and DMC 2 are operative, and
2) The ISIS airspeed function is operative, and
3) The ISIS altitude indication is operative, and
4) The ISIS attitude indication is operative, and
5) The standby compass is operative.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL
01.31.19INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-62 Display Management
Computer (DMC)
31-62-03 DMC 3
31-62-03B (cont’d) OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
- In the case of multiple undue ECAM alerts concerningENG 1(2) N1(N2) (EGT)(FF) OVERLIMITOr ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCYOr NAV ATT(ALT1)(HDG) DISCREPANCYOr NAV FM/GPS POS DISAGREEOr FUEL F.USED/FOB DISAGREEOr MINIMUM or HUNDRED ABOVE callouts, possiblyassociated with EFIS red flags, apply the belowprocedure:
- Crosscheck the affected parameters on the EWD,PFD, ND, or on the related SD page to confirm thatthe alerts are undue.
-EIS DMC SWITCHING selector . . . . . . . . . . . . . . CAPT 3
(Cont’d on next page)
01.31.20INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-62 Display
Management
Computer (DMC)
31-62-03 DMC 3
31-62-03B (Cont’d) OPERATING PROCEDURES (Cont’d)
Note:
CAPT PFD and ND ae lost when EIS
DMC SWITCHING selector is set to
CAPT 3.
- If the undue ECAM alerts stop:
- Pull EIS/DMC1/SPLY (49 VU E11) C/B a for morethan 5 s and push it back.
- EIS DMC SWITCHINGselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
- If the undue ECAM alerts continue:
- EIS DMC SWITCHING selector . . . . . . . . . . NORM
- Wait for CAPT PFD and ND recovery.
- Pull EIS/DMC2/SPLY (121 VU Q08) C/B for morethan 5 s and push it back.
12 FEB 12MEL
A320/321MEL/CDL
01.31.21INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-63 Display Unit (DU)
31-63-01 PFDU 1
31-63-01A 1 1 Must be operative.
31-63-02 PFDU 2
31-63-02A C 1 0 (O) May be inoperative provided that PFDU 1, NDU 1, NDU 2,
EWDU and SDU are operative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I.
ON GROUND OR IN FLIGHT
PFDU 2 knob · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
31-63-03 NDU 1
31-63-03A C 1 0 (O) May be inoperative provided that PFDU 1, PFDU 2, NDU
2, EWDU and SDU are operative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I.
ON GROUND OR IN FLIGHT
NDU 1 knob · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
01.31.22INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-63 Display Unit (DU)
31-63-04 NDU 2
31-63-04A C 1 0 (O) May be inoperative provided that PFDU 1, PFDU 2, NDU
1, EWDU and SDU are operative.
31-63-05 SDU
31-63-05A A 1 0 (O)(M) May be inoperative for three flight days provided that:
1) The PFDU 1, PFDU 2, NDU 1, NDU 2 and EWDU areoperative, and
2) The AC ESS FEED control is checked operative everyday, and
3) The AC ESS FEED pb-sw FAULT light is checkedoperative every day.
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
SDU knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- In the case of alerts being displayed on the EWD:
Use the ECAM/ND SWITCHING selector to display thesystem page on the selected NDU.
- In the case of failure of the AC BUS 1:
All the Display Units are lost.
Apply the ELEC AC ESS BUS FAULT alert procedure:Refer to FCOM/PRO-ABN-24-ELEC AC ESS FAULT.
Note:
The AC ESS BUS is recovered whenthe AC ESS FEED pb-sw is set to
ALTN.
MAINTENANCE PROCEDURE
Refer to AMM 31-68-00-040-006
30 JUN 12MEL
A320/321MEL/CDL
01.31.23INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-63 Display Unit (DU)
31-63-06 EWDU
31-63-06A 1 1 Must be operative.
31-68 Switching Panel
31-68-01 AIR DATA
SWITCHING
selector on the
Center Pedestal
31-68-01A C 1 0 May be inoperative provided that the AIR DATA
SWITCHING selector is set to NORM.
31-68-02 ATT HDG
SWITCHING
selector on the
Center Pedestal
31-68-02A C 1 0 May be inoperative provided that the ATT HDG
SWITCHING selector is set to NORM.
31-68-03 ECAM/ND XFR
SWITCHING
selector on the
Center Pedestal
31-68-03A C 1 0 May be inoperative provided that:
1) Both ECAM DU are operative, and
2) The ECAM/ND XFR SWITCHING selector is set toNORM.
01.31.24INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-68 Switching Panel
31-68-04 EIS DMC
SWITCHING
selector on the
Center Pedestal
31-68-04A C 1 0 May be inoperative provided that the EIS DMC
SWITCHING selector is set to NORM.
31-68-05 PFD/ND XFR pb
on the Lateral
Instrument Panel
31-68-05A C 2 0 (O) One or both may be inoperative provided that:
1) The PFD and ND units are operative, and
2) The PFD to ND automatic switching is checkedoperative on the PF side before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- On the side where the PFD/ND XFR pb isinoperative:
- PFD brightness control knob . . . . . . . . . . . . . . . OFF
- Check that the PFD image is automaticallydisplayed on the NDU.
- PFD brightness control knob . . . . . . . . . . . . . . . . On
- If the PFD image is not automatically displayedon the NDU:The affected side cannot be used by the PilotFlying.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL
01.31.25INDICATING/RECORDING
SYSTEMS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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31 INDICATING/RECORDING
SYSTEMS
31-68 Switching Panel
31-68-05 PFD/ND XFR pb
on the Lateral
Instrument Panel
31-68-05A (Cont’d) OPERATING PROCEDURES (Cont’d)
- On the side where the PFD to ND automaticswitching is inoperative:
- PFD brightness control knob . . . . . . . . . . . . . . . OFF
- EIS DMC SWITCHING selector (Affected side. . . . . . . . . . . . . . . . . . CAPT 3 (F/O 3)
- Check that the PFD image is displayed on theassociated NDU.
- PFD brightness control knob . . . . . . . . . . . . . . . . On
- EIS DMC SWITCHING knob(Affected side) . . . . . . . . . . . . . . . . . . . . . . . NORM
IN FLIGHT
- If a PFDU fails with no automatic transfer to theassociated NDU:
- PFD brightness control knob . . . . . . . . . . . . . . . OFF
- EIS DMC SWITCHING selector (Affected side) . . . . . . . . . . . . . . . . . CAPT 3 (F/O 3)
- Check that the PFD image is displayed on theassociated NDU.
* * *
01.31.26INDICATING/RECORDINGSYSTEMS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A C 4 0 (O) One or more may be inoperative provided that the ground
brake cooling time is applied.
OPERATING PROCEDURES (A320)
FLIGHT PREPARATION/LIMITATIONS
The brake energy graph and the brake cooling time table
given hereafter permit to determine the ground brake
cooling time.
BRAKE ENERGY GRAPH
- If MAX reverser thrust was selected for allreversers during the braking phase:Enter the brake energy graph: WITH THRUST
REVERSERS USE.
- If MAX reverser thrust was NOT selected for allreversers during the braking phase:Enter the brake energy graph: WITHOUT THRUSTREVERSERS USE.
Determination of the brake energy accumulated during a
REJECTED TAKEOFF (RTO) :
- Enter with the aircraft takeoff weight (TOW) and withthe rejected takeoff speed in kt IAS.
- Apply airport pressure altitude, temperature, wind andrunway slope corrections.
Determination of the brake energy accumulated during a
LANDING :
- Enter with the aircraft landing weight, and
- Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manualbraking speed in kt IAS in the other cases.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
12 FEB 12MEL
A320/321MEL/CDL 01.32.01
LANDING GEAR
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A320) (Cont’d)
- Apply airport pressure altitude, temperature, wind andrunway slope corrections.
- Correct for brake setting with a preselected autobrakesetting (LO, MED) or with MAX PEDAL braking in theother cases.
Note:
In the case of a dispatch with one brake
inoperative (Refer to Item 32-42-01
Main Wheel Brake or Refer to Item 32-
42-02 Green System Brake), the brake
energy accumulated is increased by
34%.
(Cont’d on next page)
01.32.02LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A320) (Cont’d)
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.03
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A320) (Cont’d)
(Cont’d on next page)
D
01.32.04LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A320)(Cont’d)
BRAKE COOLING TIME TABLE
Determination of the brake cooling time:
EXAMPLE:
55 152
46
153
46
154
46
155
46
155
47
==> TIME (min) WITHOUT BRAKE
COOLING FAN
==> TIME (min) WITH BRAKE
COOLING FAN
If the Energy and the OAT are not given in the table, use
the values given in the next adjacent column/row.
For Example, with Energy = 78 MJ, and OAT = 15°C,entering the next adjacent column/row (Energy = 80 MJ,
OAT = 20°C) gives the following results:
- Without brake cooling fan: 189 min
- With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to
determine the ground brake cooling time.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.05
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A320) (Cont’d)
(Cont’d on next page)
D
01.32.06LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A320)(Cont’d)
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.07
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A320)(Cont’d)
AFTER ENGINE START
- In the case of a false BRAKES HOT alert displayedon the EWD:EMER CANC pb · · · · · · · · · · · · · · · · · · · · · · · · · Press
Note:
In the case of a false BRAKES HOT
alert due to a faulty BTMU or a faulty
BSCU, the "T.O CONFIG NORMAL” line
will not replace the "T.O CONFIG . .
TEST" line in the T.O MEMO. Consider
normal configuration for takeoff provided
that no alert were displayed during theT.O CONFIG TEST.
CAUTION
The T.O CONFIG TEST pb must be
maintained pressed to check that
there is no alert.
OPERATING PROCEDURES (A321)
FLIGHT PREPARATION/LIMITATIONS
The brake energy graph and the brake cooling time table
given hereafter permit to determine the ground brake
cooling time.
(Cont’d on next page)
01.32.08LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
BRAKE ENERGY GRAPH
- If MAX reverser thrust was selected for allreversers during the braking phase:Enter the brake energy graph: WITH THRUSTREVERSERS USE.
- If MAX reverser thrust was NOT selected for allreversers during the braking phase:Enter the brake energy graph: WITHOUT THRUSTREVERSERS USE.
Determination of the brake energy accumulated during a
REJECTED TAKEOFF (RTO) :
- Enter with the aircraft takeoff weight (TOW) and withthe rejected takeoff speed in kt IAS.
- Apply airport pressure altitude, temperature, wind andrunway slope corrections.
Determination of the brake energy accumulated during a
LANDING :
- Enter with the aircraft landing weight, and
- Enter with touch down speed in kt IAS if the autobrakewas selected and applied or with the manual brakingspeed in kt IAS in the other cases.
- Apply airport pressure altitude, temperature, wind andrunway slope corrections.
- Correct for brake setting with a preselected autobrakesetting (LO, MED) or with MAX PEDAL braking in theother cases.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.09
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
Note:
In the case of a dispatch with one brake
inoperative (Refer to Item 32-42-01
Main Wheel Brake or Refer to Item 32-
42-02 Green System Brake), the brake
energy accumulated is increased by
34%.
(Cont’d on next page)
01.32.10LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.11
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
01.32.12LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
BRAKE COOLING TIME TABLE
Determination of the brake cooling time:
EXAMPLE:
55 152
46
153
46
154
46
155
46
155
47
==> TIME (min) WITHOUT BRAKE
COOLING FAN
==> TIME (min) WITH BRAKE
COOLING FAN
If the Energy and the OAT are not given in the table, use
the values given in the next adjacent column/row.
For Example, with Energy = 78 MJ, and OAT = 15°C,entering the next adjacent column/row (Energy = 80 MJ,
OAT = 20°C) gives the following results:
- Without brake cooling fan: 189 min
- With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to
determine the ground brake cooling time.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.13
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
01.32.14LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.15
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-01 Brakes
Temperature
Indication on the
WHEEL SD page
32-07-01A (Cont’d) OPERATING PROCEDURES (A321)(Cont’d)
AFTER ENGINE START
- In the case of a false BRAKES HOT alert displayedon the EWD:EMER CANC pb · · · · · · · · · · · · · · · · · · · · · · · · · Press
Note:
In the case of a false BRAKES HOT
alert due to a faulty BTMU or a faulty
BSCU, the "T.O CONFIG NORMAL” line
will not replace the "T.O CONFIG . .
TEST" line in the T.O MEMO. Consider
normal configuration for takeoff provided
that no alert were displayed during theT.O CONFIG TEST.
CAUTION
The T.O CONFIG TEST pb must be
maintained pressed to check that
there is no alert.
32-07-01B C 4 0 (O)(M) One or more may be inoperative provided that:
1) The associated sensor is deactivated if the BRAKESHOT alert is displayed on the EWD, and
2) The ground brake cooling time is applied.
OPERATING PROCEDURES
Refer to MEL item 32-07-01A
MAINTENANCE PROCEDURE
Refer to AMM 32-47-00-040-001
01.32.16LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-02 L/G Position
Indication on the
WHEEL SD page
32-07-02A C 6 0 One or more may be inoperative provided that the L/G
gear position indications are operative on the LDG GEAR
indicator panel.
32-07-03 L/G Doors
Position Indication
on the WHEEL SD
page
32-07-03A C 3 0 (O) One or more may be inoperative.
OPERATING PROCEDURES
IN FLIGHT
MAX SPEED . . . . . . . . . . . . . . . . . . . . . . . 250 kt or M 0.60
32-07-04 L/G CTL Indication
on the WHEEL SD
page
32-07-04A C 1 0 May be inoperative.
32-07-05 UP LOCK
Indication on the
WHEEL SD page
32-07-05A C 3 0 One or more may be inoperative.
32-07-06 [Y] N/W STEERINGIndication on the
WHEEL SD page
32-07-06A C 2 0 One or both may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.32.17
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-07 Tire Pressure
Indication on the
WHEEL SD page
32-07-07A C 6 0 One or more may be inoperative.
32-07-08 ANTI SKID, [1], [2]
Indication on the
WHEEL SD page
32-07-08A C 3 0 One or more may be inoperative.
32-07-09 AUTO BRK
Indication on the
WHEEL SD page
32-07-09A C 1 0 May be inoperative.
32-07-10 [G] NORM BRK
Indication on theWHEEL SD page
32-07-10A C 2 0 One or both may be inoperative.
32-07-11 Release Brake
Indication on the
WHEEL SD page
32-07-11A C 4 0 One or more may be inoperative.
01.32.18LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-07 Indications on the
WHEEL SD page
32-07-12 ACCU
PRESS/ACCU
ONLY Indication
on the WHEEL SD
page
32-07-12A C 1 0 May be inoperative.
32-07-13 [Y] ALTN BRK
Indication on the
WHEEL SD page
32-07-13A C 2 0 One or both may be inoperative.
32-09 ECAM Alerts
32-09-01 BRAKES-N/WS
MINOR FAULT
Alert
32-09-01A Fault on an
alternate
braking system
pressure
transducer
C 1 0 May be inoperative provided that:
1) The alert is confirmed to be caused by a fault on analternate braking system pressure transducer bytroubleshooting, and
2) The associated BRAKES pressure indicator isconsidered inoperative.
Refer to Item 32-44-03 BRAKES Pressure Indicator
12 FEB 12MEL
A320/321MEL/CDL 01.32.19
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-09 ECAM Alerts
32-09-01 BRAKES-N/WS
MINOR FAULT
Alert
32-09-01C Both BRAKES
pressure
indicators
operative
B 1 0 (O)(M) May be displayed provided that:
1) Both BRAKES pressure indicators are operative, and
2) The alternate braking system is checked operativebefore the first flight of each day, and
3) It is checked before each flight that the CFDS failuremessage related to the BRAKES-N/WS MINORFAULT alert do not report a fault on an alternatepressure transducer.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
The ACCU PRESS indication must be in the green band.
- If ACCU PRESS indication not in the green band:
Y ELEC PUMP pb-sw · · · · · · · · · · · · · · · ON then OFF
- CHOCKS · · · · · · · · · · · · · · · · · · · · CHECK IN PLACE
- PARKING BRAKE handle · · · · · · · · · · · · · · · · · · · OFF
- PARKING PEDALS · · · · · · · · · · · · · · · · · · · · · PRESS
Apply maximum pressure on both pedals.
- BRAKE PRESSURE(on BRAKES pressure indicators) · · · · · · · · · · CHECK
Pressure must increase without delay symmetricallyon left and right sides for the same applicationsimultaneously applied on left and right pedals. Withfull pedal deflection, the pressure must be between
900 and 1100 psi.
- BRAKES PEDALS · · · · · · · · · · · · · · · · · · · · RELEASE
Check that no residual pressure in the brakes remains.
- PARKING BRAKE handle · · · · · · · · · · · · · · · · · · · · ON
MAINTENANCE PROCEDURE
Refer to AMM 32-46-00-040-001
01.32.20LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-09 ECAM Alerts
32-09-02 WHEEL TYRE LO
PR Alert
32-09-02A Associated
monitoring
channel
deactivated
C 1 0 (M) May be displayed on one or more wheels provided that:
1) The alert is confirmed to be false by troubleshooting,and
2) The associated pressure monitoring channel is
deactivated, and
3) The tire pressure on the affected wheel is checked tobe within the limits before the first MEL dispatch andthen every three days.
MAINTENANCE PROCEDURE
Refer to AMM 32-49-00-040-001
32-09-02B TPIC
deactivated
C 1 0 (M) May be displayed on all wheels provided that:
1) The alert is confirmed to be false by troubleshooting,and
2) The Tire Pressure Indicating Computer (TPIC) isdeactivated, and
3) The tire pressure on each wheel is checked to bewithin the limits before the first MEL dispatch and thenevery three days.
MAINTENANCE PROCEDURE
Refer to AMM 32-49-00-040-002
01 MAY 12MEL
A320/321MEL/CDL 01.32.21
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-11 Main Gear
32-11-01 Main Gear Torque
Link Damper
32-11-01A A 2 0 (FD) One or both may be inoperative for 7 flights.
32-12 Main Gear Doors
32-12-01 Ground Opening
Cable
32-12-01A C 2 0 (M) One or both may be broken or missing.
MAINTENANCE PROCEDURE
Refer to AMM 32-12-00-040-006
01.32.22LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-31 Normal Extension
and Retraction
32-31-01 Landing Gear
Control and
Interface Unit
(LGCIU)
32-31-01A A 2 1 (O)(FD) The LGCIU 2 may be inoperative for one flight day
provided that:
1) All ELACs, SECs, SFCCs, RAs, FACs, and ADIRSsare operative,
2) Both air conditioning packs are operative,
3) The FLEX Takeoff Mode is not used,
4) The operation of avionics equipment is time limited onground,
5) Reverser number 2 considered inoperative,
6) Both radio altimeter systems are operative, and
7) Both FCU channels are operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
HYDRAULIC/LGCIU/SYS2
(121VU Q35) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
The following table gives the consequences on the
systems affected when the LGCIU 2 is inoperative and
above mentioned C/B is pulled.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.32.23
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-31 Normal Extension and
Retraction
32-31-01 Landing Gear
Control and
Interface Unit
(LGCIU)
32-31-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
(Cont’d on next page)
01.32.24LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-31 Normal Extension
and Retraction
32-31-01 Landing Gear
Control and
Interface Unit
(LGCIU)
32-31-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.32.25
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-31 Normal Extension and
Retraction
32-31-01 Landing Gear
Control and
Interface Unit
(LGCIU)
32-31-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
IN FLIGHT
- In the case of loss of the LGCIU 1:
AP and FD are lost.
Maximum landing capability is CAT I.
32-31-02 Landing Gear
Retracting System
32-31-02A C 1 0 (O) May be inoperative provided that the aircraft is operated in
accordance with the Flight Manual supplement for the
flight with landing gear down.
OPERATING PROCEDURES
Refer to FCOM/PRO-SPO-25 Flight With Gear Down.
32-32 Proximity Detector
System
32-32-01 LGCIU 1 Proximity
Detector
32-32-01A 16 16 All must be operative.
01.32.26LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-02 LGCIU 2 RH L/G
Shock Absorber
Proximity Detector
32-32-02A A 1 0 (O)(M)
(FD)
May be inoperative for one flight provided that:
1) Both radio altimeters are operative, and
2) The other proximity detectors are operative, and
3) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.32.27
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-02 LGCIU 2 RH L/G
Shock Absorber
Proximity Detector
32-32-02A (Cont’d) OPERATING PROCEDURES (Cont’d)
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
01.32.28LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-02 LGCIU 2 RH L/G
Shock Absorber
Proximity Detector
32-32-02B A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and InterfaceUnit (LGCIU)
32-32-03 LGCIU 2 LH L/G
Shock Absorber
Proximity Detector
32-32-03A A 1 0 (O)(M)
(FD)
May be inoperative for one flights provided that:
1) Both radio altimeters are operative, and
2) The other proximity detectors are operative, and
3) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.32.29
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32-03A (Cont’d) OPERATING PROCEDURES (Cont’d)
(Cont’d on next page)
01.32.30LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-03 LGCIU 2 LH L/G
Shock Absorber
Proximity Detector
32-32-03A (Cont’d) OPERATING PROCEDURES (Cont’d)
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-03B A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to MEL 32-31-01 Landing Gear Control and
Interface Unit (LGCIU)
30 JUN 12MEL
A320/321MEL/CDL 01.32.31
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-04 LGCIU 2 Nose L/G
Shock Absorber
Proximity Detector
32-32-04A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-04B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
01.32.32LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-05 LGCIU 2 RH L/G
Down Lock
Proximity Detector
32-32-05A Other proximity
detectors
operative
C 1 0 (O)(M) May be inoperative provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-05B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and InterfaceUnit (LGCIU)
30 JUN 12MEL
A320/321MEL/CDL 01.32.33
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-06 LGCIU 2 LH L/G
Down Lock
Proximity Detector
32-32-06A Other proximity
detectors
operative
C 1 0 (O)(M) May be inoperative provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-06B LGCIU 2considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
01.32.34LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-07 LGCIU 2 Nose L/G
Down Lock
Proximity Detector
32-32-07A Other proximity
detectors
operative
C 1 0 (O)(M) May be inoperative provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-07B LGCIU 2considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
30 JUN 12MEL
A320/321MEL/CDL 01.32.35
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-08 LGCIU 2 RH L/G
Up Lock Proximity
Detector
32-32-08A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-08B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
01.32.36LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-09 LGCIU 2 LH L/G
Up Lock Proximity
Detector
32-32-09A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-09B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
30 JUN 12MEL
A320/321MEL/CDL 01.32.37
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-10 LGCIU 2 Nose L/G
Up Lock Proximity
Detector
32-32-10A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
GENERAL INFORMATION
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-10B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
01.32.38LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-11 LGCIU 2 RH L/G
Doors Open
Proximity Detector
32-32-11A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
Refer to Operating Procedures 32-32-08A LGCIU 2 RH
L/G Up Lock Proximity Detector
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-11B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
32-32-12 LGCIU 2 LH L/G
Doors Open
Proximity Detector
32-32-12A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
Refer to Operating Procedures 32-32-09A LGCIU 2 LH
L/G Up Lock Proximity Detector
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
30 JUN 12MEL
A320/321MEL/CDL 01.32.39
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-12 LGCIU 2 LH L/G
Doors Open
Proximity Detector
32-32-12B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
32-32-13 LGCIU 2 Nose L/G
Doors Open
Proximity Detector
32-32-13A Other proximity
detectors
operative
A 2 0 (O)(M)
(FD)
One or both may be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
Refer to Operating Procedures 32-32-10A LGCIU 2 Nose
L/G Up Lock Proximity Detector
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-13B LGCIU 2considered
inoperative
A 2 0 (FD) One or both may be inoperative for one flight providedthat the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
01.32.40LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-14 LGCIU 2 RH L/G
Doors Closed
Proximity Detector
32-32-14A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative.
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
Refer to Operating Procedures 32-32-08A LGCIU 2 RH
L/G Up Lock Proximity Detector
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-14B LGCIU 2considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
30 JUN 12MEL
A320/321MEL/CDL 01.32.41
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-15 LGCIU 2 LH L/G
Doors Closed
Proximity Detector
32-32-15A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
Refer to Operating Procedures 32-32-09A LGCIU 2 LH
L/G Up Lock Proximity Detector
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-15B LGCIU 2considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
01.32.42LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-32 Proximity Detector
System
32-32-16 LGCIU 2 Nose L/G
Doors Closed
Proximity Detector
32-32-16A Other proximity
detectors
operative
A 1 0 (O)(M)
(FD)
May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
OPERATING PROCEDURES
Refer to Operating Procedures 32-32-10A LGCIU 2 Nose
L/G Up Lock Proximity Detector
MAINTENANCE PROCEDURE
Refer to AMM 32-31-00-040-003
32-32-16B LGCIU 2
considered
inoperative
A 1 0 (FD) May be inoperative for one flight provided that the LGCIU
2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface
Unit (LGCIU)
32-33 Free Fall Extension
32-33-01 Landing Gear
Gravity Extension
System
32-33-01A C 1 0 (O) May be inoperative provided that the aircraft is operated in
accordance with the Flight Manual supplement for the
flight with landing gear down.
OPERATING PROCEDURES
Refer to FCOM/SPO-25 Flight With Gear Down.
30 JUN 12MEL
A320/321MEL/CDL 01.32.43
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-41 Wheels
32-41-01 Nose Wheel Tie
Bolt
32-41-01A A 12 11 (M)(FD) One tie bolt on one wheel may be broken or missing for 15
flights provided that:
1) The affected wheel tie bolt is removed, and
2) The affected wheel and the associated brake arechecked for absence of damage.
MAINTENANCE PROCEDURE
Refer to AMM 32-41-00-040-002
32-41-02 Main Wheel Tie
Bolt
32-41-02A A 18 17 (M)(FD) One tie bolt on one wheel may be broken or missing for 15
flights provided that:
1) The affected wheel tie bolt is removed, and
2) The affected wheel and the associated brake arechecked for absence of damage.
MAINTENANCE PROCEDURE
Refer to AMM 32-41-00-040-003
01.32.44LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-42-01 Main Wheel Brake
32-42-01A C 4 3 (O)(M)
(FD)
One may be inoperative provided that:
1) The nose wheel steering is operative, and
2) Both thrust reversers are operative, and
3) The green and yellow systems are operative onoperative brakes, and
4) The affected brake is deactivated or removed, and
5) The runway width at departure and arrival airports is atleast 45 m, and
5) The Flight Manual performance penalties areapplied,and
6) Anti-skid system is operative and Wheel tachometers
are operative.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.32.45
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-42-01 Main Wheel Brake
32-42-01A (Cont’d) OPERATING PROCEDURES (A320)
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
For performance calculations request Modified TailoredTakeoff and Landing charts (MTTL) from FPE through
Flight Dispatch.
Landing performance computation:
Increase the landing distances by 20 %.
FOR TAKEOFF
The autobrake function, even if available, must not be
used.
Performed the takeoff using full thrust (TOGA).
-- In the case of engine failure at takeoff:Retract the landing gear when positive climb.
Vibrations may occur during 1 or 2 min after theretraction of the landing gear.
- If both engines are operative:
Keep the landing gear down for 1 min.
FOR LANDING
The autobrake function, even if available, must not be
used.
(Cont’d on next page)
01.32.46LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-42-01 Main Wheel Brake
32-42-01A (Cont’d) OPERATING PROCEDURES (A321)
For performance calculations request Modified Tailored
Takeoff and Landing charts (MTTL) from FPE through
Flight Dispatch.
Landing performance computation:
Increase the landing distances by 20 %.
FOR TAKEOFF
The autobrake function, even if available, must not be
used.
Performed the takeoff using full thrust (TOGA).
- In the case of engine failure at takeoff:
Retract the landing gear when positive climb.Vibrations may occur during 1 or 2 min after theretraction of the landing gear.
- If both engines are operative:
Keep the landing gear down for 1 min.
FOR LANDING
The autobrake function, even if available, must not beused.
MAINTENANCE PROCEDURE
Refer to AMM 32-42-00-040-003
30 JUN 12MEL
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SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-42-02 Green System
Brake
32-42-02A C 1 1 (O)(M)(FD)
Braking on one wheel may be inoperative provided that:1) The nose wheel steering is operative, and
2) Both thrust reversers are operative, and
3) The green hydraulic supply of affected brake isdeactivated, and
4) The runway width at departure and arrival airports is atleast 45 m, and
5) The Flight Manual performance penalties are applied.
OPERATING PROCEDURES
Refer to Operating Procedures 32-42-01A Main Wheel
Brake
MAINTENANCE PROCEDURE
Refer to AMM 32-42-00-040-002
01.32.48LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-42-03 Braking/Steering
Control Unit
(BSCU) System 1
32-42-03A C 1 0 (M) May be inoperative provided that:
1) The BSCU system 2 is operative, and
2) The affected system is deactivated, and
3) It is checked that the CFDS does not report a faultrelated to the L/G SYS DISAGREE alert before eachflight, and
4) The AUTO/BRK (LO, MED, MAX) pb-sw DECEL lightand the AUTO/BRK (LO, MED, MAX) pb-sw ON lightare considered inoperative, and
5) Brake pressure indicators is operative, and
6) Alternate brake system checked operative before eachdepature.
Refer to Item 32-42-08 AUTO/BRK (LO, MED, MAX) pb-sw DECEL light, and
Refer to Item 32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light
MAINTENANCE PROCEDURE
Refer to AMM 32-42-00-040-007
32-42-04 Braking/Steering
Control Unit
(BSCU) System 2
32-42-04A C 1 0 (M) May be inoperative provided that:
1) The affected system is deactivated, and
2) It is checked that the CFDS does not report a faultrelated to the L/G SYS DISAGREE alert before eachflight, and
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.32.49
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-42-04 Braking/Steering
Control Unit
(BSCU) System 2
32-42-04A (Cont’d) 3) Brake pressure indicators is operative, and
4) Alternate brake system checked operative before eachdepature.
MAINTENANCE PROCEDURE
Refer to AMM 32-42-00-040-007
32-42-05 AUTO/BRK
Function
32-42-05A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
BEFORE TAKEOFF
When T.O MEMO is displayed on the EWD, disregard the
line:
AUTO BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX (blue)
32-42-06 Tachometer
32-42-06B 4 4 Must be operative.
32-42-08 AUTO/BRK (LO,
MED, MAX) pb-sw
DECEL light
32-42-08A C 3 0 One or more may be inoperative.
01.32.50LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-42-09 AUTO/BRK (LO,
MED, MAX) pb-sw
ON light
32-42-09A AUTO/BRK
mode arming
displayed on
the WHEEL SD
page
C 3 0 One or more may be inoperative provided that, when
appropriate, the associated AUTO/BRK mode arming is
displayed on the WHEEL SD page.
32-42-09B AUTO/BRK
function
considered
inoperative
C 3 0 One or more may be inoperative provided that the
AUTO/BRK function is considered inoperative.
Refer to Item 32-42-05 AUTO/BRK Function
32-44 Alternate Braking
32-44-01 Yellow System
Brake
32-44-01A C 1 1 (M) Braking on one wheel may be inoperative provided that:
1) Both thrust reversers are operative, and
2) The yellow hydraulic supply of the affected brake isdeactivated.
MAINTENANCE PROCEDURE
Refer to AMM 32-43-00-040-001
30 JUN 12MEL
A320/321MEL/CDL 01.32.51
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-44 Alternate Braking
32-44-02 ACCU PRESS
Indicator
32-44-02A Brakes
pressure
indicator
operative
C 1 0 May be inoperative provided that:
1) Both brakes pressure indicators are operative, and
2) The pressure on both brakes pressure indicators ischecked with parking brake ON before each flight.
32-44-02B Checks on
WHEEL SD
page
C 1 0 May be inoperative provided that:
1) The ACCU PRESS/ACCU ONLY indication isoperative on the WHEEL SD page, and
2) The hydraulic pressure of the brake accumulator ischecked on the WHEEL SD page before each flight.
01.32.52LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-42 Normal Braking
32-44-03 BRAKES Pressure
Indicator
32-44-03A C 2 0 One or both may be inoperative provided that the BSCU
system 1 and the BSCU system 2 are operative.
32-44-04 Alternate Braking
Control Unit
(ABCU)
32-44-04A 1 1 Must be operative.
32-45 Parking/Ultimate
Emergency Braking
32-45-01 Parking Brake
Control Valve
Electrical Motor
32-45-01A C 2 1 (M) One may be inoperative provided that:
1) Both thrust reversers are operative, and
2) The aircraft is not towed if the STBY motor is affectedand when the batteries supply the aircraft.
MAINTENANCE PROCEDURE
Refer to AMM 32-45-00-040-001
30 JUN 12MEL
A320/321MEL/CDL 01.32.53
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-47 Brake Temperature
System
32-47-01 Brake
Temperature
Monitoring Unit
(BTMU)
32-47-01A C 2 0 (O) One or both may be inoperative provided that the ground
brake cooling time is applied.
OPERATING PROCEDURES
DURING PRELIMINARY COCKPIT PREPARATION
HYDRAULIC/BRK/TEMP/DET/UNIT
(121VU M26 or M37) C/B. . . . . . . . . . . . . . . . . . . . . . PULL
Determine brake cooling time (Refer to OpsProc 32-07-
01A(B) Brakes Temperature Indication on the WHEEL SD
page).
32-48 Brake Cooling
32-48-01 Brake Fan System
32-48-01A C 1 0 May be inoperative.
32-48-02 BRK FAN pb-sw
HOT light
32-48-02A C 1 0 May be inoperative.
32-48-03 BRK FAN pb-sw
ON light
32-48-03A C 1 0 May be inoperative.
Note:
Brake Fan operation may be checked through the brake
fan ECAM MEMO.
01.32.54LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-51 Steering
32-51-01 Nose Wheel
Steering Control
System
32-51-01A A 1 1 Must be operative.
32-51-02 Rudder PEDALS
DISC pb
32-51-02A C 2 0 (O) One or both may be inoperative (no disconnection is
possible).
OPERATING PROCEDURES
The purpose of the procedure is to explain how to perform
the flight control check with one or both PEDALS DISC pb
failed in the released position.
OPERATING PROCEDURES
GENERAL INFORMATION
- When the disconnection is not possible on oneside:The flight control check can be performed on theoperative side.
- When the disconnection is not possible on bothsides:The flight control check must be performed whileaircraft is stopped.
Note:
It is not necessary to set the A/SKID &N/W STRG sw to OFF.
30 JUN 12MEL
A320/321MEL/CDL 01.32.55
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-51 Steering
32-51-03 NWS Electrical
Deactivation Box
32-51-03A No towing
mode when
lever in the
TOWING
position
C 1 0 (O) May be inoperative.
Note:
The towing mode is not available when
the lever is in the TOWING position.
OPERATING PROCEDURES
BEFORE CONVENTIONAL OR TOWLESS PUSHBACK
A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . OFF
AFTER PUSHBACK
A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . . ON
32-51-03B NWS electrical
deactivation
box deactivated
C 1 0 (O)(M) May be inoperative provided that the NWS electrical
deactivation box is deactivated.
(Cont’d on next page)
01.32.56LANDING GEAR
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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32 LANDING GEAR
32-51 Steering
32-51-03 NWS Electrical
Deactivation Box
32-51-03B NWS electrical
deactivation
box deactivated
(Cont’d)
OPERATING PROCEDURES
BEFORE CONVENTIONAL OR TOWLESS PUSHBACK
A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . OFF
As a result of the NWS electrical box deactivation, the
parking brake light on that box will not be available.
The parking brake setting must be verbally confirmed
between the flight crew and the ground personnel before
pushback.
AFTER PUSHBACK
A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . . ON
MAINTENANCE PROCEDURE
Refer to AMM 32-51-00-040-002
30 JUN 12MEL
A320/321MEL/CDL 01.32.57
LANDING GEAR
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SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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32 LANDING GEAR
32-51 Steering
32-51-04 PARKING BRAKE
light on the NWS
Electrical
Deactivation Box
32-51-04A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
BEFORE PUSHBACK
The parking brake setting must be verbally confirmed
between the flight crew and the ground personnel.
32-61 Landing Gear Panel
on the Center
Instrument Panel
32-61-01 LDG GEAR
Indicator Panel
32-61-01A C 1 0 May be inoperative.
32-61-02 DOWN Red Arrow
light on the
Landing Gear
lever
32-61-02A C 1 0 (M) May be inoperative provided that the L/G GEAR NOT
DOWN alert and the L/G GEAR NOT DOWNLOCKED
alert are checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 32-61-00-040-001
* * *
01.32.58LANDING GEAR
A320/321MEL/CDL 30 JUN 12
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SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
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01.32.60LANDING GEAR
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SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
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SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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01.32.62LANDING GEAR
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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12 FEB 12MEL
A320/321MEL/CDL 01.32.63
LANDING GEAR
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
D
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01.32.64LANDING GEAR
A320/321MEL/CDL
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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33 LIGHTS
33-01 Overhead Panels
33-01-01 ANN LT
Overhead Panel
33-01-01-01 TEST Function
of ANN LT sw
33-01-01-01A C 1 0 May be inoperative.
33-01-01-02 DIM Function of
ANN LT sw
33-01-01-02A C 1 0 Dim lighting may be inoperative provided that the bright
lighting is operative.
33-01-01-03 BRT Function of
ANN LT sw
33-01-01-03A C 1 0 Bright lighting may be inoperative for night operation.
33-01-02-01 EMER EXIT LT
OFF light
33-01-02-01A C 1 0 (M) May be inoperative provided that the emergency lighting
system is checked operative every day.
MAINTENANCE PROCEDURE
Refer to AMM 33-51-00-040-002
12 FEB 12MEL
A320/321MEL/CDL 01.33.01
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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33 LIGHTS
33-01 Overhead Panels
33-01-01 ANN LT
Overhead Panel
33-01-02-02 AUTO Function
of SEAT BELT
SIGNS sw
33-01-02-02A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
SEAT BELTS selector · · · · · · · · · · · · · · · · · · · · · · · ON
AFTER TAKEOFF
SEAT BELTS selector · · · · · · · · · · · · · · · · As required
DURING APPROACH
SEAT BELTS selector · · · · · · · · · · · · · · · · · · · · · · · ON
33-01-02-03 AUTO Function
of NO SMOKING
SIGNS sw
33-01-02-03A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check that the passenger address function isoperative in the affected lavatory with the door closed.
01.33.02LIGHTS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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33 LIGHTS
33-10 Cockpit General
Illumination
33-10-01 Cockpit General
Illumination
(Center & Main
Instrument
Lighting,
Console and
Floor Lighting,
Dome lights and
Lighting Strips,
Instrument and
Panel Integral
Lighting, Map
Holder Lighting,
Center Pedestal
Lighting)
33-10-01A C 13 10 May be inoperative provided that:
1) The lighting is sufficient for all instruments andcontrols, and
2) The RH dome light is operative, and
3) The left section of the center main panel flood light isoperative.
NOTE: RH dome light is considered operative with a
minimum of three bulbs illuminated in each assembly. The
bulbs can be checked by selecting the DOME toggle
switch from DIM to BRT and ensure both functions
operate.
33-20 Cabin General
Illumination
33-20-01 Cabin General
Illumination
33-20-01A C 6 3 The lighting must be sufficient for cabin attendants to
perform their duties.
30 JUN 12MEL
A320/321MEL/CDL 01.33.03
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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33 LIGHTS
33-20 Cabin General
Illumination
33-20-02 Cabin Signs (No
Smoking/No
Electronic
Devices/Fasten
Seat Belt/Return
to Seat)
33-20-02A Passenger seat
occupied
C 30 0 One or more may be inoperative and the affected
passenger seat may be occupied provided that:
1) The passenger address system is operative, and canbe heard throughout the cabin during the flight, and
2) The passenger address system is used to alert thepassengers when return to seat is requested, seatbelts should be fastened and smoking is prohibited.
33-20-02B Passenger seat
not occupied
C 30 0 (M)(FD)One or more “No Smoking/Fasten Seat Belt” sign may be
inoperative provided that:
1) No passenger seat is occupied from which a
passenger cannot see a readily legible “Nosmoking/Fasten Seat Belt” sign, and
2) The affected seat is blocked and placardedinoperative.
MAINTENANCE PROCEDURE
Refer to AMM 33-20-00-040-001
01.33.04LIGHTS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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33 LIGHTS
33-20 Cabin General
Illumination
33-20-03 Lavatory Sign
(Return to seat)
33-20-03A C 3 0 (O)(FD) One or more may be inoperative and the affected lavatory
may be used provided that:
1) The passenger address system is checked operative
in the affected lavatory, and2) The passenger address system is used to alert the
occupant to return to his seat.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check that the passenger address function is operative in
the affected lavatory with the door closed.
12 FEB 12MEL
A320/321MEL/CDL 01.33.05
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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33 LIGHTS
33-30 Cargo and Service
Compartment Lighting
33-30-01 Cargo and
Service
Compartment
Lighting System
33-30-01A C 1 0 May be inoperative.
33-40 Exterior Lighting
33-40-01 Navigation light
System 1
33-40-01A Daylight
operations
C 3 0 (FD) One or more may be inoperative for daylight operations.
33-40-01B Navigation light
system 2
operative
C 3 0 One or more may be inoperative provided that the
Navigation light system 2 is operative.
33-40-02 Navigation lightSystem 2
33-40-02A C 3 0 One or more may be inoperative.
33-40-03 Landing light
33-40-03A Nose, taxi and
takeoff lights
operative
C 2 1 One may be inoperative provided that the nose, taxi and
takeoff lights are operative.
33-40-03B Daylight
operations
C 2 0 (FD) One or both may be inoperative for daylight operations.
01.33.06LIGHTS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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33 LIGHTS
33-40 Exterior Lighting
33-40-04 Landing light
Extension/
Retraction
System
33-40-04A Inoperative in
extended
position
C 2 0 (O)(FD) One or both may be inoperative in the extended position.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
The fuel consumption is increased by 1 % per landing light
extended.
33-40-04B Inoperative in
retracted
position
C 2 0 One or both may be inoperative in the retracted position
provided that the associated light is considered
inoperative.
Refer to MEL Item 33-40-03 Landing light
33-40-05 Runway Turnoff
lights
33-40-05A C 2 0 One or both may be inoperative.
33-40-06 Taxi and Takeoff
light
33-40-06A C 2 1 One may be inoperative.
33-40-07 Logo lights
33-40-07A D 2 0 One or both may be inoperative.
30 JUN 12MEL
A320/321MEL/CDL 01.33.07
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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33 LIGHTS
33-40 Exterior Lighting
33-40-08 Beacon light
33-40-08A Daylight
operations
C 2 0 (O)(FD) One or both may be inoperative for daylight operations.
OPERATING PROCEDURES
BEFORE ENGINE START
- If the bottom light is inoperative:
If this light is used to alert the ground crew of theengine start, the captain must brief the groundmechanic regarding beacon light.
33-40-08B Strobe lights
operative
C 2 0 (O) One or both may be inoperative provided that the Strobe
lights are operative.
OPERATING PROCEDURES
Refer to MEL item 33-40-08A
33-40-09 Wing Scan lights
33-40-09A Daylight
operations
C 2 0 (FD) One or both may be inoperative for daylight operations.
33-40-09B Night
operations
C 2 1 One may be inoperative for night operations.
33-40-10 Strobe light
33-40-10A C 3 0 One or more may be inoperative.
01.33.08LIGHTS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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33 LIGHTS
33-51 Cabin Emergency
Lighting
33-51-01 Exit Marking
Sign
(A320)
33-51-01B A maximum of
three non-
adjacent LEDs
inoperative
C 6 6 A maximum of three non-adjacent LEDs may be
inoperative in one or more signs.
33-51-01 Exit Marking
Sign
(A321)
33-51-01B A maximum of
three non-
adjacent LEDs
inoperative
C 8 8 A maximum of three non-adjacent LEDs may be
inoperative in one or more signs.
33-51-02 Exit Location
Sign in the MainAisle
33-51-02A C 18 15 A maximum of three non-adjacent LEDs may be
inoperative in one or more signs.
33-51-03 Overhead
Emergency
Lighting System
in the Main Aisle
33-51-03A C 22 19 A maximum of three non-adjacent overhead emergency
lights may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.33.09
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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33 LIGHTS
33-51 Cabin Emergency
Lighting
33-51-04 Overhead
Emergency
Lighting System
in the Door
Vicinity
(A320)
33-51-04A Refer to Item 52-10-01 Cabin Passenger Door, and
Refer to Item 52-10-02 Overwing Emergency Exit
33-51-04 Overhead
Emergency
Lighting System
in the Door
Vicinity
(A321)
33-51-04A Refer to MEL Item 52-10-01 Cabin Passenger Door
33-51-05 Floor Proximity
Emergency
Escape Path
Marking System
in the Main Aisle
33-51-05A
( M : meters )
C 80
M
79
M
Each of the photoluminescent strips of an aisle may be
inoperative or missing up to a length of 0,25 meter
(10 inches) provided the inoperative or missing parts are
not directly opposite each other and are not closer than 2,0
meter (78.74 inches). No more than four such inoperative
or missing parts are allowed provided:
1- All strips within 1 meter of an exit is operative, and
2- All strips marking right angle intersection includingcross aisles and overwing exits are operative.
01.33.10LIGHTS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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33 LIGHTS
33-51 Cabin Emergency
Lighting
33-51-07 Floor Proximity
Emergency
Escape Path
Marking System
Exit Marker
33-51-07A Refer to MEL Item 52-10-01 Cabin Passenger Door, and
Refer to MEL Item 52-10-02 Overwing Emergency Exit
33-51-08 Overwing
Emergency light
33-51-08A Daylight
operations
C 4 0 (FD) One or more may be inoperative for daylight operations.
33-51 Cabin Emergency
Lighting
33-51-09 Overwing ExitHandle light
33-51-09A C 4 0 One or more may be inoperative.
33-51-10 Escape Slide
Lighting
33-51-10A Daylight
operations
C 8 0 May be inoperative for daylight operations.
33-51-11 LavatoryAuxiliary light
33-51-11A C 4 0 One or more may be inoperative.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.33.11
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E MI T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.33.12LIGHTS
A320/321MEL/CDL 12 FEB 12
MEL
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34 NAVIGATION
34-00 MAINTENANCE
Messages on the
STATUS SD page
34-00-01 ADR (1)(2)(3)
MAINTENANCE
Message
34-00-01A C 3 - ADR (1)(2)(3) MAINTENANCE message may be displayed
on the STATUS SD page.
34-00-02 IR
MAINTENANCE
Message
34-00-02A C 3 - IR MAINTENANCE message may be displayed on the
STATUS SD page.
34-01 Overhead
Panels
34-01-01 ADIRS
Overhead Panel
34-01-01-01 ADR pb-sw
FAULT light
34-01-01-01A C 3 0 One or more may be inoperative.
34-01-01-02 ADR pb-sw OFF
light
34-01-01-02A C 3 0 One or more may be inoperative.
34-01-01-03 IR pb-sw FAULT
light
34-01-01-03A C 3 0 One or more may be inoperative.
34-01-01-04 IR pb-sw OFF
light
34-01-01-04A C 3 0 One or more may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.34.01
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-01 Overhead Panels
34-01-01 ADIRS Overhead
Panel
34-01-01-04 IR pb-sw OFF
light
34-01-01-04A C 3 0 One or more may be inoperative.
34-01-01-05 ON BAT light
34-01-01-05A C 1 0 May be inoperative.
34-01-01-31 ADR pb-sw
34-01-01-31A C 3 2 (O) ADR 2 or ADR 3 pb-sw may be inoperative provided that:
1) The associated mode selector is operative, and
2) The two ADRs and the two IRs associated with the twooperative ADRs pb-sw are operative.
OPERATING PROCEDURES
IN FLIGHT
If needed, the associated ADR can be set to OFF through
the associated mode selector.
Note:
- If the ADR is set to OFF:
The associated IR is also set to OFF.
The F/CTL MAINTENANCE message is
displayed on the STATUS SD page.
01.34.02NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-01 Overhead Panels
34-01-01 ADIRS Overhead
Panel
34-01-01-32 IR pb-sw
34-01-01-32A C 3 2 (O) IR 2 or IR 3 pb-sw may be inoperative provided that:
1) The associated mode selector is operative, and
2) The two ADRs and the two IRs associated with the twooperative IRs pb-sw are operative.
OPERATING PROCEDURES
FLIGHT
If needed, the associated IR can be set to OFF through the
associated mode selector.
Note:
- If the IR is set to OFF:
The associated ADR is also set to
OFF.
The F/CTL MAINTENANCE
message is displayed on the
STATUS SD page.
34-01-01-33 IR Mode selector
34-01-01-33A C 3 2 One may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.34.03
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-01 Overhead Panels
34-01-02 GPWS Overhead
Panel
34-01-02-01 GPWS SYS
FAULT light
34-01-02-01A C 1 0 May be inoperative provided GPWS is verified operative
before each departure.
34-05 Indications on the
Primary Flight Display
(PFD)
34-05-01 Actual Airspeed
Reference Line
and Scale
Indication on the
PFD
34-05-01A 2 2 Both must be operative.
34-05-02 Mach Number
Indication on the
PFD
34-05-02A One indication
inoperative
C 2 1 One may be inoperative.
34-05-02B Both indications
inoperative - FCU
operative
C 2 0 Both may be inoperative provided that the SPD/MACH
selection window on the FCU is operative.
34-05-02C Both indications
inoperative - FLlimitation
C 2 0 (FD) Both may be inoperative provided that the flight altitude is
limited to 25 000 ft.
34-05-02D Both indications
inoperative - ISIS
Mach Number
Function operative
C 2 0 Both may be inoperative provided that the ISIS Mach
Number indication is operative.
01.34.04NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-05 Indications on the
Primary Flight
Display (PFD)
34-05-03 VMO/MMO
Characteristic
Speed Indication
on the PFD
34-05-03A 2 2 Both must be operative.
34-05-04 Altitude
Indication on the
PFD
34-05-04A 2 2 Both must be operative.
34-05-05 Baro Reference
Indication on the
PFD
34-05-05A 2 2 Both must be inoperative.
34-05-06 Vertical Speed in
Inertial Mode
Indication on the
PFD
34-05-06A C 2 0 One or both may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.34.05
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-05 Indications on the
Primary Flight Display
(PFD)
34-05-07 Other Air Data
Related
Indications on the
PFD
34-05-07A C 2 0 (O) One or more may be inoperative.
OPERATING PROCEDURES
GENERAL INFORMATION
For F, S, Green Dot determination, refer to the QRH/FPE-
SPD speeds.
For VAPP determination, refer to QRH/FPE-IFL-VAPP
determination.
For VFE or VLE determination, refer to the corresponding
placard in the cockpit.
34-05-08 Attitude Indication
on the PFD
34-05-08A C 2 1 (O) One may be inoperative provided that the aircraft is
operated in day VMC conditions.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I.
34-05-09 Heading Indication
on the PFD
34-05-09A C 2 1 One may be inoperative.
01.34.06NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-06 Indications on the
Navigation Display
(ND)
34-06-01 Ground Speed
Indication on the
ND
34-06-01A C 2 0 One or both may be inoperative.
34-06-02 True Air Speed
Indication on the
ND
34-06-02A C 2 0 One or both may be inoperative.
34-06-03 Wind Indication
on the ND
34-06-03A C 2 0 One or both may be inoperative.
34-06-04 Heading
Indication on theND
34-06-04A C 2 1 One may be inoperative provided that the heading
indications are operative on both PFDs.
34-06-05 Position
(Aircraft
Symbol)
Indication on the
ND
34-06-05A C 2 0 One or both may be inoperative.
34-06-06 Radio Navaids
Indications on
the ND
34-06-06A C 2 0 One or more may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.34.07
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-06 Indications on the
Navigation Display
(ND)
34-06-07 Chrono Indication
on the ND
34-06-07A C 2 0 One or both may be inoperative.
34-10 Air Data/Inertial
Reference System
(ADIRS)
34-10-01 ADR 1
34-10-01A 1 1 Must be operative.
34-10-02 ADR 2
34-10-02B C 1 0 (O) May be inoperative provided that:
1) The IR 1, IR 3, ADR 1 and ADR 3 are operative, and
2) The takeoff is not performed in CONF 1+F.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING COCKPIT PREPARATION
- ADR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
The F/CTL MAINTENANCE message is displayed onthe STATUS SD page.
- AIR DATA SWITCHING selector · · · · · · · · · · · · · F/O 3
- ADIRS/ADIRU/2/26VAC AND AOA(location 121VU N08 or N09) C/B · · · · · · · · · · · · · Pull
(Cont’d on next page)
01.34.08NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-10 Air Data/Inertial
Reference System
(ADIRS)
34-10-02 ADR 2
34-10-02B (Cont’d) OPERATING PROCEDURES (Cont’d)
AFTER ENGINE START
- Use the RCL pb-sw on the ECAM control panel, inorder to recall the NAV ADR 2 FAULT alert.
- On the EWD, check that the ADR 2...OFF procedure isnot displayed.
FOR TAKEOFF
Takeoff in CONF 1+F is not permitted.
Note:
When the ADR 2 pb-sw is set to OFF,
and if the aircraft is in CONF 1+F, the
SFCS n°2 Flap channel is unable to
crosscheck the airspeed coming fromthe ADR 1 with the ADR 2 airspeed
coming from the SFCS n°2 Slat channel.
This may lead to an uncommanded flap
retraction during the takeoff. As a
consequence, takeoff in CONF 1+F is
not permitted when the ADR 2 pb-sw is
set to OFF.
12 FEB 12MEL
A320/321MEL/CDL 01.34.09
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-10 Air Data/Inertial
Reference System
(ADIRS)
34-10-03 ADR 3
34-10-03A C 1 0 (O) May be inoperative provided that the IR 1, IR 2, ADR 1
and ADR 2 are operative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING COCKPIT PREPARATION
- ADR 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
The F/CTL MAINTENANCE message is displayed onthe STATUS SD page.
- ADIRS/ADIRU/3/26VAC AND AOA(location 121VU N07 or N08) C/B· · · · · · · · · · · · · · Pull
AFTER ENGINE START
- Use the RCL pb-sw on the ECAM control panel, inorder to recall the NAV ADR 3 FAULT alert.
- On the EWD, check that the ADR 3...OFF procedure isnot displayed.
01.34.10NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-10 Air Data/Inertial
Reference System
(ADIRS)
34-10-04 IR 1
34-10-04B GPS 1
operative
B 1 1 (O)(FD) The NAV mode may be inoperative provided that:
1) The IR 1 is operated in ATT mode, and
2) The IR 2 and IR 3 are operative, and
3) The GPS 1 is operative, and
4) The terrain function of the TAWS is consideredinoperative.Refer to MEL Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS)
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING COCKPIT PREPARATION
- ATT HDG SWITCHING selector · · · · · · · · · · · CAPT 3
- IR 1 mode selector· · · · · · · · · · · · · · · · · · · · · · · · · ATT
- The heading must be entered through the MCDU for the IR 1 and has to be frequently reset(Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN
ATT MODE).
34-10-04C GPS 1
inoperative
B 1 1 (O)(FD) The NAV mode may be inoperative provided that:
1) The IR 1 is operated in ATT mode, and
2) The IR 2 and IR 3 are operative, and
3) The Flight remains within radio navaids coverage, and
4) The terrain function of the TAWS ñ– is consideredinoperative.Refer to MEL Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS)
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.34.11
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-10 Air Data/Inertial
Reference System
(ADIRS)
34-10-04 IR 1
34-10-04C GPS 1 inoperative
(Cont’d)
OPERATING PROCEDURES
Refer to MEL item 34-10-04B Operating Procedures
34-10-05 IR 2
34-10-05B IR 2 totally
inoperative
C 1 0 (O) May be inoperative provided that:
1) The IR 2 pb-sw is set to OFF, and
2) The IR 1, the IR 3, the ADR 1 and the two ADRs areoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING COCKPIT PREPARATION
- IR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
The F/CTL MAINTENANCE message is displayed onthe STATUS SD page.
- ATT HDG SWITCHING selector · · · · · · · · · · · · · F/O 3
- AIR DATA SWITCHING selector · · · · · · · · · · · · · F/O 3
34-10-05C Only NAV mode of
IR 2 inoperative
C 1 0 (O) The NAV mode may be inoperative provided that:
1) The IR 2 is operated in ATT mode, and
2) The IR 1 and the IR 3 are operative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
(Cont’d on next page)
01.34.12NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-10 Air Data/Inertial
Reference System
(ADIRS)
34-10-05 IR 2
34-10-05C Only NAV mode
of IR 2
inoperative
(Cont’d)
OPERATING PROCEDURES (Cont’d)
DURING COCKPIT PREPARATION
- ATT HDG SWITCHING selector · · · · · · · · · · · · · F/O 3
- IR 2 mode selector· · · · · · · · · · · · · · · · · · · · · · · · · ATT
- The heading must be entered through the MCDUkeyboard for the IR 2 and has to be frequently reset(Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN
ATT MODE).
34-10-07 IR 3
34-10-07A IR 3 mode
selector set to
OFF
B 1 0 (O) May be inoperative provided that:
1) The IR 3 pb-sw is set to OFF, and
2) The IR 1, the IR 2, the ADR 1, and the ADR 2 are
operative.
OPERATING PROCEDURES
GENERAL INFORMATION
For aircraft fitted with Honeywell 10 MCU ADIRU,
disregard the characteristic speeds (Vls, F, S, Green Dot)
displayed on the PFD. For characteristic speeds (Vls, F, S,
Green Dot) determination, refer to the QRH. The “CHECK
GW” (or “CHECK WEIGHT”) message may be displayed
on the MCDU.
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING COCKPIT PREPARATION
IR 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
The F/CTL MAINTENANCE message is displayed on the
STATUS SD page.
01 MAY 12MEL
A320/321MEL/CDL 01.34.13
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-10 Air Data/Inertial
Reference System
(ADIRS)
34-10-07 IR 3
34-10-07B IR 3 operated in
ATT mode
C 1 0 (O) The NAV mode may be inoperative provided that:
1) The IR 3 is operated in ATT mode, and
2) The IR 1 and the IR 2 are operative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Landing capability is CAT II.
DURING COCKPIT PREPARATION
- IR 3 mode selector· · · · · · · · · · · · · · · · · · · · · · · · · ATT
- The heading must be entered through the MCDU for the IR 3 and has to be frequently reset.(Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN
ATT MODE).
34-11 Sensors
34-11-01 Angle of Attack
(AOA) Sensor
34-11-01A C 3 2 The F/O or the STBY Angle Of Attack sensor may be
inoperative provided that the associated ADR is
considered inoperative.
Refer to MEL Item 34-10-02 ADR 2, or
Refer to MEL Item 34-10-03 ADR 3
01.34.14NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-11 Sensors
34-11-02 CAPT Total Air
Temperature
(TAT) Sensor
Element
Connected to
ADR1
34-11-02A C 1 0 (O) May be inoperative provided that:
1) The CAPT sensor element connected to the ADR 3 isoperative, and
2) The F/O sensor connected to the ADR 2 is operative,and
3) The ADR 2 and the ADR 3 are operative, and
4) The TAT indication on the SD is checked operative,and
5) The TAS indication on the ND 1 is consideredinoperative.Refer to MEL Item 34-06-02 True Air Speed Indicationon the ND
OPERATING PROCEDURES
Refer to Operating Procedures 31-07-02A Permanent
Data Indications on the SD
12 FEB 12MEL
A320/321MEL/CDL 01.34.15
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-11 Sensors
34-11-03 CAPT Total Air
Temperature (TAT)
Sensor Element
Connected to
ADR3
34-11-03A C 1 0 (O) May be inoperative provided that:
1) The CAPT sensor element connected to the ADR 1 isoperative, and
2) The F/O sensor connected to the ADR 2 is operative,and
3) The ADR 1 and the ADR 2 are operative, and
4) The TAT indication on the SD is checked operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check that the TAT is displayed on the SD permanent
data.
34-11-04 F/O Total Air
Temperature (TAT)
Sensor Element
Connected to
ADR2
34-11-04A C 1 0 (O) May be inoperative provided that:
1) Both CAPT TAT sensor elements are operative, and
2) The ADR 1 and the ADR 3 are operative, and
3) The TAT indication on the SD is checked operative,and
4) The TAS indications on the ND 2 is consideredinoperative.Refer to MEL Item 34-06-02 True Air Speed Indicationon the ND
(Cont’d on next page)
01.34.16NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-11 Sensors
34-11-04 F/O Total Air
Temperature
(TAT) Sensor
Element
Connected to
ADR2
34-11-04A (Cont’d) OPERATING PROCEDURES
Refer to Operating Procedures 31-07-02A Permanent
Data Indications on the SD
34-21 Altitude and
Airspeed Standby
Data
34-21-05 Standby ALT
Metric Indicator
34-21-05A C 1 0 May be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.34.17
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-22 Attitude and Heading
Standby Data
34-22-01 Standby Compass
Indicator
34-22-01A Applicable to
aircraft fitted with
NORTHROP
GRUMMAN
(LITTON) ADIRU
except P/N 465020-
0303-0316 or
subsequent, having
the shelf modified
(MOD 30650/SB
25-1248, or MOD
30872)
1 1 Must be operative.
34-22-01B Applicable to
aircraft fitted with
NORTHROP
GRUMMAN(LITTON) ADIRU
P/N 465020-0303-
0316 or
subsequent, having
the shelf modified
(MOD 30650/SB
25-1248, or MOD
30872) or
HONEYWELL
ADIRU
C 1 0 (O) May be inoperative provided that:
1) The three IRs are operative, and
2) The ATT/HDG SWITCHING selector, the EIS DMCSWITCHING selector and the PFD/ND XFR pb arechecked operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check of the ATT HDG, PFD/ND, and EIS DMCswitching:
- ATT HDG SWITCHING selector . . . . . . . . CAPT 3
- Check that the display is normal on the CAPT
PFD, the CAPT ND, and the RMI VOR.
- ATT HDG SWITCHING selector . . . . . . . . . . F/O 3
- Check that the display is normal on the F/O PFD
and the F/O ND.
- ATT HDG SWITCHING selector . . . . . . . . . NORM
- EIS DMC SWITCHING selector. . . . . . . . . CAPT 3
- Check that the display is normal on the CAPT PFD
and the CAPT ND.
(Cont’d on next page)
01.34.18NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-22 Attitude and
Heading Standby
Data
34-22-01 Standby
Compass
Indicator
34-22-01B Applicable to
aircraft fitted with
NORTHROP
GRUMMAN
(LITTON) ADIRU
P/N 465020-0303-
0316 or
subsequent, having
the shelf modified
(MOD 30650/SB
25-1248, or MOD
30872) or
HONEYWELL
ADIRU
OPERATING PROCEDURES (Cont’d)
- EIS DMC SWITCHING selector . . . . . . . . . . F/O 3
- Check that the display is normal on the F/O PFD
and the F/O ND.
- EIS DMC SWITCHING selector . . . . . . . . . NORM
- CAPT PFD/ND XFR pb . . . . . . . . . . . . . . . . . Press
- Check that the CAPT PFD and the CAPT ND
images are exchanged.
- CAPT PFD/ND XFR pb . . . . . . . . . . . . . . . . . Press
- F/O PFD/ND XFR pb. . . . . . . . . . . . . . . . . . . Press
- Check that the F/O PFD and the F/O ND images
are exchanged.
- F/O PFD/ND XFR pb. . . . . . . . . . . . . . . . . . . Press
34-22-02 Standby
Compass
Lighting
34-22-02A C 1 0 May be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.34.19
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-23 Integrated Standby
Instrument System
(ISIS)
34-23-01 ISIS Baro-Altitude
Indication
34-23-01A B 1 0 May be inoperative provided that the aircraft is operated in
day VMC conditions.
34-23-02 ISIS Airspeed
Indication
34-23-02A C 1 0 May be inoperative provided that:
1) The ISIS attitude indication is operative, and
2) The ADRs, DMCs and probe heat computers areoperative, and
3) The AIR DATA SWITCHING selector, the EIS DMCSWITCHING selector and the PFD/ND XFR pb areoperative.
34-23-03 ISIS BugsIndication
34-23-03A C 1 0 May be inoperative.
01.34.20NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-23 Integrated
Standby
Instrument
System (ISIS)
34-23-04 ISIS Attitude
Indication
34-23-04B B 1 0 (O)(FD) M ay be inoperative provided that the aircraft is operated in
day VMC conditions.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT I.
12 FEB 12MEL
A320/321MEL/CDL 01.34.21
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-23 Integrated Standby
Instrument System
(ISIS)
34-23-05 ISIS ILS Indication
34-23-05A C 1 0 May be inoperative.
34-23-06 ISIS Mach Number
Indication
34-23-06A C 1 0 May be inoperative.
34-30 Landing and Taxiing
Aid
34-30-04 Instrument
Landing System
(ILS)
34-30-04A C 2 1 (O)(FD) One ILS may be inoperative for VMC operations or for IMC
operations provided approach minimums do not require
use.
Note:
When the ILS 1 is inoperative, the
reactive modes of TAWS are
inoperative. Refer to Item 34-40-01
Ground Proximity Warning System
(GPWS)/Terrain Awareness and
Warning System (TAWS)
(Cont’d on next page)
01.34.22NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-30 Landing and
Taxiing Aid
34-30-04 Instrument
Landing System
(ILS)
34-30-04A (cont’d) OPERATING PROCEDURES
Note:
- When one ILS is inoperative:
Maximum landing capability is ILS CAT I.
- When both ILS are inoperative:
CAT I ILS approaches are not permitted.
34-40 GPWS/TAWS,
Radio Altimeter,
TCAS, Weather
Radar
34-40-01 Ground
Proximity
Warning System
(GPWS)/Terrain
Awareness and
Warning System
(TAWS)
34-40-01A A 1 0 (O) May be inoperative provided:
a) For the intent of returning International Flights toeither JED, RUH or DMM, the aircraft may continuethe flight sector(s) scheduled before the failure,
b) Flight is conducted under Day VMC conditions,and
c) Repairs are made within one flight day.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.34.23
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-40 GPWS/TAWS, Radio
Altimeter, TCAS,
Weather Radar
34-40-01 Ground Proximity
Warning System
(GPWS)/Terrain
Awareness and
Warning System
(TAWS)
34-40-01A (Cont’d) OPERATING PROCEDURES
Flight crew should increase their awareness of airplane
configuration, altitude and flight path at all times and
review and comply with Minimum Enroute Altitudes (MEA)
and altitude callouts.
34-40-01B Modes 1- 4 A 4 0 (O) May be inoperative provided:
1) For the intent of returning International Flights toeither JED, RUH or DMM, the aircraft may continuethe flight sector(s) scheduled before the failure,
2) Flight is conducted under Day VMC conditions,and
3) Repairs are made within one flight day.
OPERATING PROCEDURES
Flight crew should increase their awareness of airplane
configuration, altitude and flight path at all times and
review and comply with Minimum Enroute Altitudes (MEA)
and altitude callouts.
34-40-01C Test Mode A 1 0 (O) May be inoperative provided:
1) For the intent of returning International Flights to
either JED, RUH or DMM, the aircraft may continuethe flight sector(s) scheduled before the failure,
2) Flight is conducted under Day VMC conditions,and
3) Repairs are made within one flight day.
(Cont’d on next page)
01.34.24NAVIGATION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-40 GPWS/TAWS,
Radio Altimeter,
TCAS, Weather
Radar
34-40-01 Ground
Proximity
Warning System
(GPWS)/Terrain
Awareness and
Warning System
(TAWS)
34-40-01C Test Mode
(Cont’d)
OPERATING PROCEDURES
Flight crew should increase their awareness of airplane
configuration, altitude and flight path at all times and
review and comply with Minimum Enroute Altitudes (MEA)
and altitude callouts.
34-40-01D Glideslope
Deviation Mode
5
B 1 0 May be inoperative.
34-40-01E Advisory Call-
Outs
C 7 0 (O) May be inoperative provided alternate procedures are
established and used.
OPERATING PROCEDURES
The PM must be briefed to handle all the advisory calls per
FCOM instructions.
34-40-01F TAWS C 1 0 (O) May be inoperative provided alternate procedures are
established and used.
OPERATING PROCEDURES
Flight crew should increase their awareness of airplane
configuration, altitude and flight path at all times and
comply with Minimum Enroute Altitude (MEA).
12 FEB 12MEL
A320/321MEL/CDL 01.34.25
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-40 GPWS/TAWS, Radio
Altimeter, TCAS,
Weather Radar
34-40-02 Radio Altimeter
Automatic Callout
34-40-02A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Maximum Landing capability is CAT I.
30-40-03 Radio Altimeter
System
30-40-03A C 2 1 (O) One may be inoperative provided that both FCU channels,
all ELACs, SECs, ADIRUs, SFCCs, LGCIUs and FACs are
operative.
Note:
When the radio altimeter 1 is
inoperative, the reactive modes of
TAWS are inoperative.
Refer to MEL 34-40-01 Ground
Proximity Warning System
(GPWS)/Terrain Awareness and
Warning System.
OPERATING PROCEDURES
FLIGHT PREPERATION LIMITATION
Maximum landing Capability is CAT I.
The F/CTL MAINTENACE Message is displayed on the
STATUS SD page.
(Cont’d on next page)
01.34.26NAVIGATION
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-40 GPWS/TAWS,
Radio Altimeter,
TCAS, Weather
Radar
30-40-03 Radio Altimeter
System
30-40-03A (Cont’d) OPERATING PROCEDURES (Cont’d)
DURING COCKPIT PREPERATION
< If RA 1 is inoperative:
COM NAV/RAD ALTM/1 (121VU K11) C/B. . . . . . . . . . Pull
< If RA 2 is inoperative:
COM NAV/RAD ALTM/2 (121VU K12) C/B. . . . . . . . . . Pull
34-40-04 Traffic Collision
Avoidance
System (TCAS)
34-40-04A 1 1 Must be operative.
Note:
When the TCAS is deactivated, the
TAWS is also inoperative.
Refer to Item 34-40-01 Ground
Proximity Warning System
(GPWS)/Terrain Awareness and
Warning System (TAWS)
34-40-05 Weather Radar
System
34-40-05A C 2 1 One may be inoperative.
30 JUN 12MEL
A320/321MEL/CDL 01.34.27
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-40 GPWS/TAWS, Radio
Altimeter, TCAS,
Weather Radar
34-40-05 Weather Radar
System
34-40-05B B 2 0 (FD) Both may be inoperative provided:
1) Flight is conducted in Day VMC, and
2) For IMC or Night VMC flights, provided currentweather reports do not indicate any thunderstorms or other potentially hazardous weather conditions whichcan be detected by weather radar.
Note:
When the captain and flight dispatcher
have determined that weather radar
inoperative requirements are met, the
associated Dispatch Release must
include the following statement:“Airborne weather radar is inoperative
and not required.”
Note:
When the weather radar system is
inoperative, the predictive Windshear
Detection System is inoperative .
Refer to Item 34-40-06 Weather
Radar/Predictive Windshear Detection
Function .
01.34.28NAVIGATION
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-40-06 Predictive
Windshear
Detection
Function
34-40-06A Refer to MEL item 22-60-03A
34-40-07 PULL UP-GPWS
pb-sw
34-40-07A One
inoperative
C 2 1 (O) One may be inoperative provided that the GPWS or the
TAWS aural and visual warnings are checked operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check of the GPWS (or TAWS) aural and visual warnings:
- PULL UP . GPWS pb-sw (operative · · · · · · · · · · Press
- Check that the GPWS (or the TAWS) aural and visualwarnings are operative.Refer to FCOM/DSC-34-70 GPWS.
34-50 ATC and Radio /
GPS Navigation
Systems
34-50-01 ATC
34-50-01A B 2 1 (O)(FD) One may be inoperative
OPERATING PROCEDURES
- An altitude encoder must be operative for theoperative transponder,
- In the event both ATC transponders becomeinoperative enroute, the flight may continue to the nextpoint of intended landing where repairs or replacementfacilities are available. Appropriate authorization from
ATC centers concerned is necessary.
- An ATC transponder must be operative to enter RVSMairspace
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL 01.34.29
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-50 ATC and Radio / GPS
Navigation Systems
34-50-01 ATC
34-50-01A (Cont’d) OPERATING PROCEDURES (Cont’d)
FLIGHT PREPARATION/LIMITATIONS
When both ATCs are inoperative, RVSM operations are
not permitted.
34-50-03 ADF
34-05-03A C 1 0 May be inoperative unless its use is required.
34-50-04 DME
34-50-04A 2 1 One may be inoperative provided both GPS is operative.
34-50-05 VOR
34-50-05A 2 2 Both must be operative.
34-50-06 MARKER
34-50-06A C 1 0 (FD) May be inoperative provided approach minimums do not
required its use.
01.34.30NAVIGATION
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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34 NAVIGATION
34-50 ATC and Radio /
GPS Navigation
Systems
34-50-09 Global
Positioning
System (GPS)
34-50-09A 2 2 (FD) Both are required to be operative for flights departing the
kingdom envolving RNAV routes, and/or RNAV/GPS
approaches.
34-50-09B B 2 1 (O)(FD) One may be inoperative on RNAV routes, and/or
RNAV/GPS approaches returning to the kingdom provided
both DME systems are operative
OPERATING PROCEDURES:
Dispatch must confirm whether the route or part of the
route is RNAV airspace and destination airport does not
have published GPS approaches only.
34-50-09C B 2 0 (O)(FD) May be inoperative provided the flight is not dispatched
through RNAV airspace.
OPERATING PROCEDURES:
Dispatch must confirm whether the route or part of the
route is not RNAV airspace and destination, alternate
airport does not have published GPS approaches only.
* * *
30 JUN 12MEL
A320/321MEL/CDL 01.34.31
NAVIGATION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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01.34.32NAVIGATION
A320/321MEL/CDL
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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35 OXYGEN
35-01 Overhead Panels
35-01-01 OXYGEN
Overhead Panel
35-01-01-01 CREW SUPPLY
pb-sw OFF light
35-01-01-01A C 1 0 May be inoperative.
35-01-01-02 PASSENGER
SYS ON light
35-01-01-02A C 1 0 May be inoperative.
35-01-01-31 MANUAL
Control of the
MASK MAN ON
pb
35-01-01-31A AUTO control
function
checkedoperative
C 1 0 (M) May be inoperative provided that the AUTO control
function is checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 35-23-00-040-008
12 FEB 12MEL
A320/321MEL/CDL 01.35.01
OXYGEN
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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35 OXYGEN
35-01 Overhead Panels
35-01-01 OXYGEN
Overhead Panel
35-01-01-32 AUTO Control of
the MASK MAN
ON pb
35-01-01-32A C 1 0 (FD) May be inoperative provided that the operating altitude is
limited to FL 300.
35-07 Indications on the
DOOR/OXY SD page
35-07-01 Crew OXY High
Pressure
Indication on the
DOOR/OXY SD
page
35-07-01A C 1 0 (O)(M) May be inoperative provided that the oxygen pressure is
checked by direct reading before each flight.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
· After application of the maintenance procedure:
Check that the oxygen pressure is sufficient for the
intended flight. Refer to FCOM/LIM-35 Cockpit Fixed
Oxygen System
MAINTENANCE PROCEDURE
Refer to AMM 35-10-00-040-001
01.35.02OXYGEN
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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35 OXYGEN
35-07 Indications on the
DOOR/OXY SD
page
35-07-02 Crew Oxygen
REGUL LO PR
Indication on the
DOOR/OXY SD
page
35-07-02A C 1 0 (O)(M) May be inoperative provided that the oxygen pressure is
checked before the first flight of each day.
OPERATING PROCEDURES
GENERAL INFORMATION
On the DOOR/OXY SD page, disregard the REGUL LO
PR indication and the associated OXY indication.
MAINTENANCE PROCEDURE
Refer to AMM 35-10-00-040-002
35-10 Crew Oxygen
35-10-01 Crew Oxygen
Mask
35-10-01A C 4 2 (FD) Each occupant of the cockpit must have his assigned
mask operative.
35-10-02 Crew Oxygen
Mask Microphone
35-10-02A C 4 2 (FD) One must be operative for each pilot.
35-10-03 Exterior Crew
Oxygen
Overpressure
Indicator Disc
(Green Disc)
35-10-03A C 1 0 (O) May be missing or damaged.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.35.03
OXYGEN
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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35 OXYGEN
35-10 Crew Oxygen
35-10-03 Exterior Crew
Oxygen
Overpressure
Indicator Disc
(Green Disc)
35-10-03A (cont’d) OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Before the first flight of each day, check that the oxygen
pressure does not decrease:
On the DOOR/OXY SD page, check the OXY pressure
indication twice.
A 15 min interval must be applied between both checks.
35-20 Passenger Oxygen
35-20-01 Passenger
Oxygen Unit
35-20-01A Associated
seats
considered
inoperative
(A320)
(A321)
C
C
46
60
0
0
(FD) One or more may be inoperative provided that the
associated seats are considered inoperative.
Refer to Item 25-20-01 Passenger Seat
01.35.04OXYGEN
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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35 OXYGEN
35-20 Passenger
Oxygen
35-20-02 Cabin Attendant
Oxygen Unit
35-20-02A (A320)
(A321)
C
C
5
7
4
5
(FD) May be inoperative provided that the associated seats are
considered inoperative.
Refer to Item 25-20-03 Cabin Attendant Seat
35-20-04 Galley Oxygen
Unit
Note:
For an inoperative cabin attendant
oxygen unit located within the galley
area: Refer to Item 35-20-02 Cabin
Attendant Oxygen Unit
35-20-04A Adjacent cabin
attendant
oxygen unit
available
B 2 0 (O) One or more may be inoperative and the associated
galley area may be occupied provided that an adjacent
cabin attendant individual oxygen unit is available for each
occupants of the associated galley area.
OPERATING PROCEDURES
IN FLIGHT
The number of galley area occupants must be in
accordance with the available adjacent cabin attendant
oxygen units.
35-20-04B Portable
oxygen
available in the
associated
galley area
B 2 0 (O) One or more may be inoperative and the associated
galley area may be occupied provided that a cabin
attendant portable oxygen device is available for each
occupants of the associated galley area.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.35.05
OXYGEN
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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35 OXYGEN
35-20 Passenger Oxygen
35-20-04 Galley Oxygen
Unit
35-20-04B (cont’d) OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Before the flight, the flight crew shall brief the cabin crew
that the galley oxygen unit is inoperative and that thecabin attendant portable oxygen device should be used
instead.
35-20-04C Associated
galley area not
occupied
B 2 0 (FD) One o r more m ay b e inoperative p rovided t hat t he
associated galley area is not occupied.
35-20-05 Manual Release
Tool
35-20-05A C 6 1 One must be available.
35-30 Portable Oxygen
35-30-01 Flight Crew
Portable Device
35-30-01A 2 2 Both must be available.
01.35.06OXYGEN
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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35 OXYGEN
35-30 Portable Oxygen
35-30-02 Cabin Attendant
Portable Device
35-30-02A PBE or Smoke
Hood
C 3 2 One required in the cockpit, and
One required in the cabin.
NOTE:
Any in excess of that required may beinoperative or missing provided the
inoperative PBE is placarded
inoperative, removed from the installed
location and placed out of sight so it can
not be mistaken for a functional unit.
35-30-02B Portable
Oxygen
Cylinder
May be inoperative or missing provided the inoperative
Portable Oxygen Cylinderis placarded inoperative,
removed from the installed location and placed out of
sight so it can not be mistaken for a functional unit.
(A320) C 7 4
(A321) C 8 5
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.35.07
OXYGEN
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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01.35.08OXYGEN
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-00 MAINTENANCE
Message on the
STATUS SD Page
36-00-01 AIR BLEED
MAINTENANCE
Message
36-00-01F C 1 - AIR BLEED MAINTENANCE message may be displayed
on the STATUS SD page.
36-01 AIR COND
Overhead Panel
36-01-01 ENG BLEED pb-
sw FAULT light
36-01-01A C 2 0 One or both may be inoperative.
36-01-02 ENG BLEED pb-
sw OFF light
36-01-02A C 2 0 One or both may be inoperative.
36-01-03 APU BLEED pb-sw
FAULT light
36-01-03A C 1 0 May be inoperative.
36-01-04 APU BLEED pb-swON light
36-01-04A C 1 0 May be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.36.01
PNEUMATIC
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-07 Indications on the
BLEED SD page
36-07-01 APU Bleed Valve
Indication on the
BLEED SD page
36-07-01A C 1 0 May be inoperative.
36-07-02 Engine Bleed
Valve Indication
on the BLEED SD
page
36-07-02A C 2 0 One or both may be inoperative.
36-07-03 Engine Bleed HP
Valve Indication
on the BLEED SD
page
36-07-03A C 2 0 One or both may be inoperative.
36-07-04 Engine Bleed
Precooler Inlet
Pressure
Indication on the
BLEED SD page
36-07-04A C 2 0 One or both may be inoperative.
36-07-05 Engine Bleed
Precooler Outlet
Temperature
Indication on the
BLEED SD page
36-07-05A C 2 0 One or both may be inoperative.
01.36.02PNEUMATIC
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-07 Indications on the
BLEED SD page
36-07-06 X Bleed Valve
Indication on the
BLEED SD page
36-07-06A C 1 0 May be inoperative.
36-11 Engine Bleed Air
Supply System
36-11-01 Engine Bleed Air
Supply System
Note:
The HP ground connection is near the
engine 1 hazardous area. If the bleed air
supply system 2 is inoperative, it is
better to use the APU bleed for engine
start. If the APU bleed is not available, a
ground cart can be used as long as the
pneumatic pipe is kept out of the
hazardous area.
36-11-01A no FL limitation C 2 1 (O)(FD) One may be inoperative provided that:
1) The associated ENG BLEED pb-sw is set to OFF,
2) The X-BLEED selector is set to OPEN,
3) The speedbrakes are operative, and
4) The aircraft is not operated in known or forecast icing
condations.
OPERATING PROCEDURES
AFTER ENGINE START
- Refer to FCOM/PRO-ABN-36-C. AIR ENG 1(2) BLEED
FAULT and Refer to FCOM/PRO-ABN-36-B. AIR ENG
1(2) BLEED ABNORM PR.
(Cont’d on next page)
01 MAY 12MEL
A320/321MEL/CDL 01.36.03
PNEUMATIC
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-11 Engine Bleed Air
Supply System
36-11-01 Engine Bleed Air
Supply System
36-11-01A (cont’d) OPERATING PROCEDURES (Cont’d)
FOR TAKEOFF
Consider selecting the air conditioning packs OFF or the
APU bleed air supply system ON.
AFTER TAKEOFF
If the APU has been used to supply the air conditioning
during the takeoff, set the APU BLEED pb-sw to OFF.
IN FLIGHT
· If Wing Anti-Ice is required:
PACK (affected side) pb-sw . . . . . . . . . . . . . . . . . OFF
· In the case of failure of the remaining engine bleed
air supply system, or in the case of failure of the
associated engine:
- Apply the associated ECAM procedure, then
- Refer to QRH/ABN-36 AIR DUAL BLEED FAULT
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E MI T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
01.36.04PNEUMATIC
A320/321MEL/CDL 01 MAY 12
MEL
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36 PNEUMATIC
36-11-02 Engine Bleed
Valve (PRV)
36-11-02A C 2 1 (M) One may be inoperative provided that:
1) The affected engine bleed valve is secured in theclosed position, and
2) The associated bleed air supply system is consideredinoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
MAINTENANCE PROCEDURE
Refer to AMM 36-11-00-040-001
36-11-03 Engine Bleed
Overpressure
Valve
36-11-03A Associated
bleed
considered
inoperative
C 2 1 One may be inoperative provided that the associated
bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
01 MAY 12MEL
A320/321MEL/CDL 01.36.05
PNEUMATIC
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-11 Engine Bleed Air
Supply System
36-11-04 Engine Bleed Fan
Air Valve
36-11-04A C 2 1 (FD) One may be inoperative provided that the associated
engine bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-05 Engine Bleed Air
Precooler
36-11-05A C 2 1 One may be inoperative provided that the associated
engine bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-06 Engine Bleed IP
Check Valve
36-11-06A Associated
bleed
considered
inoperative
C 2 1 (FD) One may be inoperative provided that the associated
engine bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-06B Associated HP
valve secured
in the closed
position
C 2 1 (O)(M) One may be inoperative in the open position provided that
the associated HP valve is secured in the closed position.
(Cont’d on next page)
01.36.06PNEUMATIC
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-11 Engine Bleed Air
Supply System
36-11-06 Engine Bleed IP
Check Valve
36-11-06B (cont’d) OPERATING PROCEDURES
DURING TAXI
When the engines operate in idle thrust:
- ENG (affected side) BLEED pb-sw . . . . . . . . . . . OFF
- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . OPEN
· If wing anti-ice is required:
One PACK pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF
DURING TAKEOFF, CLIMB, AND CRUISE
- ENG (affected side) BLEED pb-sw . . . . . . . . . . . On
- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . AUTO
DURING DESCENT
When the engines operate in idle thrust:
- ENG (affected side) BLEED pb-sw . . . . . . . . . . . OFF
- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . OPEN
· If wing anti-ice is required:
One PACK pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF
MAINTENANCE PROCEDURE
Refer to AMM 36-11-00-040-002
12 FEB 12MEL
A320/321MEL/CDL 01.36.07
PNEUMATIC
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-11 Engine Bleed Air
Supply System
36-11-07 Engine Bleed HP
Valve
36-11-07A Associated
bleed
considered
inoperative
C 2 1 (FD) One may be inoperative in the closed position provided
that the associated engine bleed air supply system is
considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-07B HP valve
secured in the
closed position
C 2 1 (O)(M) One may be inoperative provided that the affected engine
bleed HP valve is secured in the closed position.
OPERATING PROCEDURES
Refer to MEL item 36-11-06B
MAINTENANCE PROCEDURE
Refer to AMM 36-11-00-040-003
36-11-08 Bleed Monitoring
Computer (BMC)
36-11-08A C 2 1 (FD) One may be inoperative provided that the associated
engine bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
01.36.08PNEUMATIC
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-12 APU Bleed Air
Supply and
Crossbleed
Systems
36-12-01 APU Bleed Air
Supply System
36-12-01A C 1 0 May be inoperative provided that the APU BLEED pb-sw
is set to OFF.
36-12-02 APU Bleed Valve
36-12-02A APU bleed
considered
inoperative
C 1 0 (M) May be inoperative provided that:
1) The APU bleed valve is secured in the closed position,and
2) The APU bleed air supply system is consideredinoperative.
Refer to Item 36-12-01 APU Bleed Air Supply System
MAINTENANCE PROCEDURE
Refer to AMM 36-12-00-710-001
36-12-02B APU not used C 1 0 (O) May be inoperative in the open position provided that the
APU is not used in flight.
Refer to Item 49-10-01 Power Plant (APU)
OPERATING PROCEDURES
ON GROUND OR IN FLIGHT
· When the APU runs:
APU BLEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . ON
· After APU shutdown:
APU BLEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . Off
12 FEB 12MEL
A320/321MEL/CDL 01.36.09
PNEUMATIC
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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36 PNEUMATIC
36-12 APU Bleed Air Supply
and Crossbleed
Systems
36-12-03 APU Bleed Check
Valve
36-12-03A C 1 0 May be inoperative provided that the APU bleed air supply
system is considered inoperative.
Refer to Item 36-12-01 APU Bleed Air Supply System
36-12-04 Automatic Control
of the X Bleed
Valve
36-12-04A C 1 0 (O) May be inoperative provided that the manual control is
checked operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
Check of the manual control of the X BLEED valve:
- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . OPEN
- On the BLEED, check that the cross bleed valve is
indicated open.
- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . SHUT
- On the BLEED, check that the cross bleed valve is
indicated closed.
- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . AUTO
01.36.10PNEUMATIC
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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36 PNEUMATIC
36-22 Leak Detection
Loop
36-22-01 Pylon Leak
Detection System
36-22-01A C 2 1 (M) One may be inoperative provided that:
1) The associated pylon leak detection loop isdeactivated, and
2) The AIR ENG 1(2) BLEED LEAK alert is confirmed tobe false by troubleshooting, and
3) The associated bleed air supply system is consideredinoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
MAINTENANCE PROCEDURE
Refer to AMM 36-22-00-040-001
36-22-02 Wing Leak
Detection System
36-22-02A 2 2 Must be operative.
Note:
Failure of one loop in one or both wing
leading edges is indicated by a
MAINTENANCE message displayed on
the STATUS SD page.
Refer to Item 36-00-01 AIR BLEED MAINTENANCE
Message
36-22-03 APU LeakDetection Loop
36-22-03A C 1 0 May be inoperative.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.36.11
PNEUMATIC
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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01.36.12PNEUMATIC
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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38 WATER/WASTE
-10-01 Potable Water Systems C 1 0 (M) Individual components may be inoperative provided:a) Associated components are deactivated or isolated,
andb) Associated system components are verified not to
have leaks.
NOTE:
Any portion of system which is operative
may be used.
MAINTENANCE PROCEDURE
Refer to AMM 38-10-00
C 1 0 (M) May be inoperative provided:a) System is drained, andb) Procedures are established to ensure that system is
not serviced.
MAINTENANCE PROCEDURE
Refer to AMM 38-10-00
-30-01 Lavatory Waste
Systems (Including
Wheelchair Accessible
Lavatories)
C 1 0 (M) Individual components may be inoperative provided:a) Associated components are deactivated or
isolated,andb) Associated system components are verified not to
have leaks.
NOTE:
Any portion of system which is operative
may be used.
MAINTENANCE PROCEDURE
Refer to AMM 38-30-00
(Cont’d on next page)
12 FEB 12
MEL
A320/321MEL/CDL 01.38.01
WATER/WASTE
I T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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38 WATER/WASTE
-30-01 Lavatory Waste
Systems (Including
Wheelchair Accessible
Lavatories)
(Cont’d)
C 1 0 (M)(FD) Associated Lavatory system(s) may be inoperative
provided:a) Associated components are deactivated or isolated to
pervent leaks,b) Extra safety pilot should be assigned to operate the
flight in case the forward lavatory placarded,c) Associated Lavatory door (s) is secured closed and
placarded, “INOPERATIVE - DO NOT ENTER”, andd) Two lavatories must be operative.
NOTE:
These provisions are not intended to
prohibit inspections by crew members.
MAINTENANCE PROCEDURE
Refer to AMM 38-30-00
1) Vacuum Generator
Systems (Toilet)
C 2 0 (M)(FD) May be inoperative provided:a) Vacuum generator is deactivated, and
b) Procedures are established and used toonly allow use of the associated lavatory
at or above 16000 FT MSL.
MAINTENANCE PROCEDURE
Refer to AMM 38-30-00
* * *
01.38.02
WATER/WASTE
A320/321MEL/CDL 04 APR 12
MEL
I T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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46 INFORMATION SYSTEM
46-11 Aircraft
Information
Network Systems
46-11-01 Electronic Flight
Bag (EFB)
46-11-01A B 2 0 (FD) One or both may be inoperative provided that the
following documents must be provided to the FDC by
dispatch:
1. Flight Dispatch Release and attachments.(including ATS FP)
2. Computer Flight Plan or manual flight log.
3. NOTAMS.
4. Latest current available TAFs/ METARs.
5. Temporary/ MTTL takeoff and landing preformancecharts (when applicable) and takeoff data cards.
6. NOTOC (if applicable).
7. ASR/ Flight Crew Report forms.
8. Manual Loadsheet Calculation Form.
46-21 Air Traffic and
Information
Management
System
46-21-01 Air Traffic Service
Unit (ATSU)
46-21-01A B 1 0 (O)(FD) May be inoperative provided altenate procedures are
used.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.46.01
INFORMATION SYSTEM
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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46 INFORMATION SYSTEM
46-21 Air Traffic and
Information
Management System
46-21-01 Air Traffic Service
Unit (ATSU)
46-21-01A (cont’d) OPERATING PROCEDURES
1) Flight crew must transmit depature, enroute, and the
arrival reports in accordance with the route manualcommunication requirement.
2) Flight crew must complete the in-flight cruiseperformance data records if required.
Note:
Any portion of the system that is
operative may be used
46-21-02 Datalink Control
and Display Unit
(DCDU)
46-21-02A B 2 0 (FD) One or both may be inoperative provided two way
communications established with ATC and inroute not
require its use.
46-21-03 ATC MSG pb
46-21-03A B 2 0 (FD) Refer to MEL 46-21-02A
* * *
01.46.02INFORMATION SYSTEM
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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47 INERT GAS SYSTEM
47-00 MAINTENANCE
Message on the
STATUS SD Page
47-00-01 FUEL INERT
MAINTENANCE
Message
47-00-01A C 1 - FUEL INERT MAINTENANCE Message may be displayed
on the STATUS SD page.
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E MI T E M
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
12 FEB 12MEL
A320/321MEL/CDL 01.47.01
INERT GAS SYSTEM
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01.47.02INERT GAS SYSTEM
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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49 AIRBORNE AUXILIARY
POWER
49-00 MAINTENANCE
Message on the
STATUS SD page
49-00-01 APU
MAINTENANCE
Message
49-00-01A C 1 - APU MAINTENANCE message may be displayed on the
STATUS SD page.
49-01 APU Overhead
Panel
49-01-01 APU MASTER SW
pb-sw FAULT light
49-01-01A C 1 0 May be inoperative provided that the N and the EGT
indications are operative on the APU SD page.
49-01-02 APU MASTER SW
pb-sw ON light
49-01-02 C 1 0 May be inoperative.
49-01-03 APU START pb-sw
AVAIL light
49-01-03A C 1 0 May be inoperative provided that the N indication is
operative on the APU SD page.
49-01-04 APU START pb-sw
ON light
49-01-04A C 1 0 May be inoperative.
12 FEB 12MEL
A320/321MEL/CDL
01.49.01 AIRBORNE AUXILIARY
POWER
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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49 AIRBORNE AUXILIARY
POWER
49-07 Indications on the
APU SD page
49-07-01 Indications on the
APU SD page
49-07-01A C 9 0 One or more may be inoperative.
49-10 Power Plant
49-10-01 Power Plant (APU)
49-10-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
GENERAL INFORMATION
No APU bleed air will be available for Main Engine Start
(MES) or air conditioning.
No electrical power will be available from the APU
generator.
DURING COCKPIT PREPARATION
APU MASTER SW pb-sw . . . . . . . . . . . . . . . . . . . Off
49-10-02 APU Air Intake
Flap
49-10-02A APU not used C 1 0 May be inoperative in the closed position provided that the
APU is not used.
49-10-02B APU used A 1 0 (M) May be inoperative in the open position for 10 days.
MAINTENANCE PROCEDURE
Refer to AMM 49-16-00-040-002
* * *
01.49.02 AIRBORNE AUXILIARYPOWER
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panels
52-01-01 CKPT DOOR
CONT Normal
Overhead Panel
52-01-01-01 CHAN (1, 2)
LEDs on the
CKPT DOOR
CONT Overhead
Panel
52-01-01-01A C 2 1 One may be inoperative.
52-01-01-02 STRIKE (TOP,
MID, BOT) LEDs
on the CKPT
DOOR CONT
Overhead Panel
52-01-01-02A C 3 2 One may be inoperative.
52-01-01-03 Pressure RateSensor on the
CKPT DOOR
CONT Overhead
Panel
52-01-01-03A One inoperative A 2 1 (M) One may be inoperative for 60 consecutive calendar
days provided that the remaining pressure rate sensor is
checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 52-51-00-040-011
52-01-01-03B Both
inoperative
C 2 0 Both may be inoperative provided that the CDLS normal
system is considered inoperative.
Refer to Item 52-51-01 CDLS Normal System (Normal
Control Unit, Switch and Lights on the CKPT DOOR
Panel, Buzzer, Keypad).
12 FEB 12MEL
A320/321MEL/CDL 01.52.01
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panels
52-01-02 CKPT DOOR
CONT BK UP
Overhead Panel
52-01-02-01 CHAN (1, 2)
LEDs on the
CKPT DOOR
CONT BK UP
Overhead Panel
52-01-02-01A CTL pb FAULT
light checked
operative
C 2 0 (O) One or more may be inoperative provided that the CTL pb
FAULT light is checked operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . TEST
- Check that the associated CTL pb FAULT light comes
on.
52-01-02-01B CDLS back-up
system
considered
inoperative
C 2 0 One or more may be inoperative provided that the CDLS
back-up system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up
Control Unit, CTL pb and Lights on the CKPT DOOR BK
UP Panel)
01.52.02DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panels
52-01-02 CKPT DOOR
CONT BK UP
Overhead Panel
52-01-02-02 STRIKE (TOP,
MID, BOT) LEDs
on the CKPT
DOOR CONT BK
UP Overhead
Panel
52-01-02-02A CTL pb FAULT
light checked
operative
C 3 2 (O) One may be inoperative provided that the CTL pb FAULT
light is checked operative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
- ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . TEST
- Check that the associated CTL pb FAULT light comeson.
52-01-02-02B CDLS back-up
system
considered
inoperative
C 3 0 One or more may be inoperative provided that the CDLS
back-up system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up
Control Unit, CTL pb and Lights on the CKPT DOOR BK
UP Panel)
12 FEB 12MEL
A320/321MEL/CDL 01.52.03
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panels
52-01-02 CKPT DOOR
CONT BK UP
Overhead Panel
52-01-02-03Pressure Rate
Sensor on the
CKPT DOOR
CONT BK UP
Overhead Panel
52-01-02-03A One
inoperative
A 2 1 (M) One may be inoperative for 60 consecutive calendar
days provided that the remaining pressure rate sensor is
checked operative.
MAINTENANCE PROCEDURE
Refer to AMM 52-51-00-040-012
52-01-02-03B Both
inoperative
C 2 0 Both may be inoperative provided that the CDLS back-up
system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up
Control Unit, CTL pb and Lights on the CKPT DOOR BK
UP Panel)
01.52.04DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panels
52-01-03 CKPT DOOR BK
UP Overhead
Panel
52-01-03-01 CTL pb FAULT
light on the
CKPT DOOR BK
UP Overhead
Panel
52-01-03-01A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
· To ensure that the door is closed and locked:
On the CKPT DOOR CONT BK UP panel, check that the
three STRIKE LEDs are off.
52-01-03-01B C 1 0 May be inoperative provided that the CDLS back-up
system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up
Control Unit, CTL pb and Lights on the CKPT DOOR BK
UP Panel)
12 FEB 12MEL
A320/321MEL/CDL 01.52.05
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panel
52-01-03 CKPT DOOR BK
UP Overhead
Panel
52-01-03-02 CTL pb OPEN
light on the
CKPT DOOR BK
UP Overhead
Panel
52-01-03-02A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION
· To ensure that the door is closed and locked:
On the CKPT DOOR CONT BK UP panel, check that the
three STRIKE LEDs are off.
52-01-03-02B C 1 0 May be inoperative provided that the CDLS back-up
system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up
Control Unit, CTL pb and Lights on the CKPT DOOR BK
UP Panel)
01.52.06DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panel
52-01-03 CKPT DOOR BK
UP Overhead
Panel
52-01-03-31 CTL pb on the
CKPT DOOR BK
UP Overhead
Panel
52-01-03-31A C 1 0 (O) May be inoperative.
OPERATING PROCEDURES
- Manual opening from the cockpit has to be performed by
the cockpit crew.
One additional crew member must lock or unlock the
cockpit door manually whenever access to the flight deck
is granted or one of the crew leaves the cockpit.
52-01-03-31B C 1 0 May be inoperative provided that the CDLS back-up
system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up
Control Unit, CTL pb and Lights on the CKPT DOOR BK
UP Panel)
12 FEB 12MEL
A320/321MEL/CDL 01.52.07
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panel
52-01-03 CKPT DOOR BK
UP Overhead
Panel
52-01-03-32 BK UP Function
of the LKG SYS
sw on the CKPT
DOOR BK UP
Overhead Panel
52-01-03-32A C 1 0 May be inoperative provided that the CDLS back-up
system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up
Control Unit, CTL pb and Lights on the CKPT DOOR BK
UP Panel)
52-01-03-33 NORM Function
of the LKG SYS
sw on the CKPT
DOOR BK UP
Overhead Panel
52-01-03-33A C 1 0 May be inoperative provided that the CDLS normal
system is considered inoperative.
Refer to Item 52-51-01 CDLS Normal System (Normal
Control Unit, Switch and Lights on the CKPT DOOR
Panel, Buzzer, Keypad)
01.52.08DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-01 Overhead Panel
52-01-03 CKPT DOOR BK
UP Overhead
Panel (cont’d)
52-01-03-34 OFF Function of
the LKG SYS sw
on the CKPT
DOOR BK UP
Overhead Panel
52-01-03-34A C 1 0 (M) May be inoperative.
Note:
For maintenance purpose only, the
CDLS normal and the CDLS back-up
systems can be deactivated by
performing the associated maintenance
procedure.
MAINTENANCE PROCEDURE
Refer to AMM 52-51-00-040-008
12 FEB 12MEL
A320/321MEL/CDL 01.52.09
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-01 Passenger Door
Permanently
Indicated Open on
the DOOR/OXY SD
page
(A320)
52-07-01A Check of
associated door
and 'C' repair
interval
C 4 0 (O)(FD) One or more may be permanently indicated open when
actually closed provided that:
1) The associated door is visually checked to be closedand locked before each flight, and
2) The white SLIDE ARMED light on the associateddoor does not come on when the door is closed andlocked and the slide arming lever is in the armedposition.
OPERATING PROCEDURES
GENERAL INFORMATION
If passenger doors are affected, indications on the PTP or
the FAP may be affected.
If passenger doors are affected, the time recorded in the
ACARS movement report may be wrong.
AFTER ENGINE START
· In the case of false door alert:
EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note:the limitation MAX FL : 100/MEA
remains displayed on the STATUS SD
page.
(Cont’d on next page)
01.52.10DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-01 Passenger Door
Permanently
Indicated Open on
the DOOR/OXY SD
page
(A320)
52-07-01A Check of
associated door
and 'C' repair
interval (cont’d)
OPERATING PROCEDURES (cont’d)
BEFORE TAKEOFF
- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will
not replace the "T.O CONFIG . . TEST" line.
- Consider normal configuration for takeoff provided that
no alert was displayed during the T.O CONFIG TEST.
CAUTION
The T.O CONFIG pb must be
maintained pressed to check that there
is no alert.
12 FEB 12MEL
A320/321MEL/CDL 01.52.11
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-01 Passenger Door
Permanently
Indicated Open on
the DOOR/OXY SD
page
(A320)
52-07-01B Check of
associated door
and 'B' repair
interval
B 4 0 (O)(FD) One or more may be permanently indicated open when
actually closed provided that the associated door is
visually checked to be closed and locked before each
flight.
OPERATING PROCEDURES
GENERAL INFORMATION
If passenger doors are affected, indications on the PTP or
the FAP may be affected.
If passenger doors are affected, the time recorded in the
ACARS movement report may be wrong.
The SLIDE ARMED light on passenger doors may be
permanently illuminated.
AFTER ENGINE START
· In the case of false door alert:
EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note:
the limitation MAX FL : 100/MEA
remains displayed on the STATUS SDpage.
(Cont’d on next page)
01.52.12DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-01 Passenger Door
Permanently
Indicated Open on
the DOOR/OXY SD
page
(A320)
52-07-01B Check of
associated door
and 'B' repair
interval (cont’d)
OPERATING PROCEDURES (cont’d)
BEFORE TAKEOFF
- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will
not replace the "T.O CONFIG . . TEST" line.
- Consider normal configuration for takeoff provided that
no alert was displayed during the T.O CONFIG TEST.
CAUTION
The T.O CONFIG pb must be
maintained pressed to check that there
is no alert.
52-07-01C No night
operations
C 4 0 (O)(FD) One or more may be permanently indicated open when
actually closed provided that:
1) The aircraft is not operated at night, and
2) The associated door is visually checked to be closed
and locked before each flight.
OPERATING PROCEDURES
Refer to MEL item 52-07-01B
12 FEB 12MEL
A320/321MEL/CDL 01.52.13
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-01 Passenger
Door/Emergency
Exit Permanently
Indicated Open on
the DOOR/OXY SD
page
(A321)
52-07-01A Check of
associated door
and 'C' repair
interval
C 8 0 (O)(FD) One or more may be permanently indicated open when
actually closed provided that:
1) The associated door is visually checked to be closedand locked before each flight, and
2) The white SLIDE ARMED light on the associateddoor does not come on when the door is closed andlocked and the slide arming lever is in the armedposition.
OPERATING PROCEDURES
GENERAL INFORMATION
If passenger doors/emergency exits are affected,
indications on the PTP or the FAP may be affected.
If passenger doors are affected, the time recorded in the
ACARS movement report may be wrong.
(Cont’d on next page)
01.52.14DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-01 Passenger
Door/Emergency
Exit Permanently
Indicated Open on
the DOOR/OXY SD
page
(A321)
52-07-01A Check of
associated door
and 'C' repair
interval (cont’d)
OPERATING PROCEDURES (cont’d)
AFTER ENGINE START
· In the case of false door alert:
EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note:
the limitation MAX FL : 100/MEA
remains displayed on the STATUS SDpage.
BEFORE TAKEOFF
- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will
not replace the "T.O CONFIG . . TEST" line.
- Consider normal configuration for takeoff provided that
no alert was displayed during the T.O CONFIG TEST.
CAUTION
The T.O CONFIG pb must be
maintained pressed to check that there
is no alert.
12 FEB 12MEL
A320/321MEL/CDL 01.52.15
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-01 Passenger
Door/Emergency
Exit Permanently
Indicated Open on
the DOOR/OXY SD
page
(A321)
52-07-01B Check of
associated door
and 'B' repair
interval
B 8 0 (O)(FD) One or more may be permanently indicated open when
actually closed provided that the associated door is
visually checked to be closed and locked before each
flight.
OPERATING PROCEDURES
GENERAL INFORMATION
If passenger doors/emergency exits are affected,
indications on the PTP or the FAP may be affected.
If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.
The SLIDE ARMED light on passenger doors/emergency
exit may be permanently illuminated.
AFTER ENGINE START
· In the case of false door alert:
EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note:
the limitation MAX FL : 100/MEAremains displayed on the STATUS SD
page.
(Cont’d on next page)
01.52.16DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-01 Passenger
Door/Emergency
Exit Permanently
Indicated Open on
the DOOR/OXY SD
page
(A321)
52-07-01B Check of
associated door
and 'B' repair
interval (cont’d)
OPERATING PROCEDURES (cont’d)
BEFORE TAKEOFF
- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will
not replace the "T.O CONFIG . . TEST" line.
- Consider normal configuration for takeoff provided that
no alert was displayed during the T.O CONFIG TEST.
CAUTION
The T.O CONFIG pb must be
maintained pressed to check that there
is no alert.
52-07-01C No night
operations
C 8 0 (O)(FD) One or more may be permanently indicated open when
actually closed provided that:
1) The aircraft is not operated at night, and
2) The associated door is visually checked to be closed
and locked before each flight.
OPERATING PROCEDURES
Refer to MEL item 52-07-01B
12 FEB 12MEL
A320/321MEL/CDL 01.52.17
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-02 Passenger Door
Permanently
Indicated Closed
on the DOOR/OXY
SD page
(A320)
52-07-02A No night
operations
C 4 0 (O)(FD) One or more may be permanently indicated closed when
actually open provided that:
1) The aircraft is not operated at night, and
2) The associated door is visually checked to be closedand locked before each flight.
OPERATING PROCEDURES
GENERAL INFORMATION
If passenger doors are affected, indications on the PTP or the FAP may be affected.
If passenger doors are affected, the time recorded in the
ACARS movement report may be wrong.
01.52.18DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-02 Passenger
Door/Emergency
Exit Permanently
Indicated Closed
on the DOOR/OXY
SD page
(A321)
52-07-02A No night
operations
C 8 0 (O)(FD) One or more may be permanently indicated closed when
actually open provided that:
1) The aircraft is not operated at night, and
2) The associated door is visually checked to be closedand locked before each flight.
OPERATING PROCEDURES
GENERAL INFORMATION
If passenger doors/emergency exits are affected,
indications on the PTP or the FAP may be affected.
If passenger doors are affected, the time recorded in the
ACARS movement report may be wrong.
12 FEB 12MEL
A320/321MEL/CDL 01.52.19
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-03 Overwing
Emergency Exit
Permanently
Indicated Open on
the DOOR/OXY SD
page
52-07-03A Check of
associated exit
and 'C' repair
interval
C 2 0 (O)(M)
(FD)
One or both may be permanently indicated open when
actually closed provided that:
1) The associated exit is visually checked to be closedand locked before each flight, and
2) The relevant SLIDE indication on the DOOR/OXYSD page is normally displayed in white.
OPERATING PROCEDURES
GENERAL INFORMATION
Indications on the PTP or the FAP ñ– may be affected.
AFTER ENGINE START
· In the case of false door alert:
EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note:
the limitation MAX FL : 100/MEA
remains displayed on the STATUS SD
page.
(Cont’d on next page)
01.52.20DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-03 Overwing
Emergency Exit
Permanently
Indicated Open on
the DOOR/OXY SD
page
52-07-03A Check of
associated exit
and 'C' repair
interval (cont’d)
OPERATING PROCEDURES (Cont’d)
BEFORE TAKEOFF
- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will
not replace the "T.O CONFIG . . TEST" line.
- Consider normal configuration for takeoff provided that
no alert were displayed during the T.O CONFIG TEST.
CAUTION
The T.O CONFIG pb must be
maintained pressed to check that there
is no alert.
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-010
12 FEB 12MEL
A320/321MEL/CDL 01.52.21
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-03 Overwing
Emergency Exit
Permanently
Indicated Open on
the DOOR/OXY SD
page (A320)
52-07-03B Check of
associated exit
and 'B' repair
interval
B 2 0 (O)(M) One or both may be permanently indicated open when
actually closed provided that the associated exit is visually
checked to be closed and locked before each flight.
OPERATING PROCEDURES
Refer to MEL item 52-07-03A
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-010
52-07-03C No night
operations
C 2 0 (O)(M)
(FD)
One or more may be permanently indicated open when
actually closed provided that:
1) The aircraft is not operated at night, and
2) The associated exit is visually checked to be closedand locked before each flight.
OPERATING PROCEDURES
Refer to MEL item 52-07-03A
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-010
01.52.22DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-04 Overwing
Emergency Exit
Permanently
Indicated Closed
on the DOOR/OXY
SD page (A320)
52-07-04A No night
operations
C 2 0 (O)(M)
(FD)
One or more may be permanently indicated closed when
actually open provided that:
1) The aircraft is not operated at night, and
2) The associated exit is visually checked to be closedand locked before each flight.
OPERATING PROCEDURES
GENERAL INFORMATION
Indications on the PTP or the FAP may be affected.
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-011
12 FEB 12MEL
A320/321MEL/CDL 01.52.23
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-05 Cargo Door
Indication on the
DOOR/OXY SD
page
52-07-05A C 3 0 (O)(M)
(FD)
One or more may be inoperative provided that the
associated door is visually checked to be closed and
locked before each flight.
OPERATING PROCEDURES
GENERAL INFORMATION
· If cargo indication is inoperative due to a proximity
switch failure:
The relevant cargo heating is inhibited. Live animals must
not be carried in the cargo.
AFTER ENGINE START
· In the case of false door alert:
EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note:
the limitation MAX FL : 100/MEA
remains displayed on the STATUS SD
page.
(Cont’d on next page)
01.52.24DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD
page
52-07-05 Cargo Door
Indication on the
DOOR/OXY SD
page
52-07-05A (cont’d) OPERATING PROCEDURES (Cont’d)
BEFORE TAKEOFF
- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will
not replace the "T.O CONFIG . . TEST" line.
- Consider normal configuration for takeoff provided that
no alert was displayed during the T.O CONFIG TEST.
CAUTION
The T.O CONFIG pb must be
maintained pressed to check that thereis no alert.
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-001
52-07-06 Avionics
Compartment
Access Door
Indication on the
DOOR/OXY SD
page
52-07-06A C 4 0 (O)(M)
(FD)
One or more may be inoperative provided that the
associated door is visually checked to be closed and
locked before each flight.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.52.25
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-07 Indications on the
DOOR/OXY SD page
52-07-06 Avionics
Compartment
Access Door
Indication on the
DOOR/OXY SD
page
52-07-06A (cont’d) OPERATING PROCEDURES
AFTER ENGINE START
· In the case of false door alert:
EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note:
the limitation MAX FL : 100/MEA
remains displayed on the STATUS SD
page.
BEFORE TAKEOFF
- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will
not replace the "T.O CONFIG . . TEST" line.
- Consider normal configuration for takeoff provided that
no alert were displayed during the T.O CONFIG TEST.
MAINTENANCE PROCEDURE
Refer to AMM 52-70-00-040-004
01.52.26DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-10 Passenger/Crew
Door
52-10-01 Cabin Passenger
Door
52-10-01A 4 4 Must be operative.
52-10-02 Overwing
Emergency Exit
(A320)
52-10-02A 2 2 Must be operative.
52-10-03 Passenger Exit
Stop Fitting
52-10-03A (A320)
(A321)
C
C
56
96
52
90
(FD) A maximum of one per exit may be inoperative provided
that the flight is not pressurized, and
Refer to FCOM/PRO-SPO-20 Fligt Without Cabin
Pressurized.
Flight must be conducted in accordance with FOPM CH 8
Maintenance Ferry Flights.
52-10-04 Door Damper
Function
(A320)
52-10-04A C 4 0 One or more may be inoperative.
52-10-04 Door Damper
Function
(A321)
52-10-04A C 8 0 One or more may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL 01.52.27
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-10 Passenger/Crew Door
52-10-05 Door Emergency
Opening Function
52-10-05A (A320)
(A321)
4
8
4
8
52-10-06 CHECK DOOR
PRESSURE
Message on the
Flight Attendant
Panel (FAP)
52-10-06A (A320)
(A321)
C
C
4
8
0
0
(M) One or more messages may be displayed provided that
the door bottle pressure is checked on the associated
bottle pressure gauge before the first dispatch and then
every 8 days.
MAINTENANCE PROCEDURE
Refer to AMM 52-00-00-040-003
52-10-07 Passenger Door
Stay Mechanism
52-10-07A (A320)
(A321)
4
8
4
8
01.52.28DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-10 Passenger/Crew
Door
52-10-08 CABIN PRESSURE
light (on Doors)
52-10-08A (A320)
(A321)
C
C
4
8
0
0
One or more may be inoperative.
52-30 Cargo Door
52-30-01 Cargo Door (FWD,
AFT and BULK)
52-30-01A Cargo door
indicated locked
on the
DOOR/OXY SD
page
C 3 0 One or more may be inoperative in the closed and locked
position provided that they are indicated locked on the
DOOR/OXY SD page.
52-30-01B Visual check of
the cargo door
C 3 0 (M) One or more may be inoperative in the closed and locked
position provided that the associated cargo door isvisually checked to be closed and locked before each
flight.
MAINTENANCE PROCEDURE
Refer to AMM 52-30-00-040-001
52-30-02 Cargo Door
Actuator
52-30-02A A maximum of
one actuator
inoperative per
cargo door
A 4 2 (FD) A maximum of one per cargo door may be inoperative
provided that:
1) The integrity of the yellow hydraulic system is notaffected, and
2) The wind velocity during loading and unloadingoperations is below 30 kt, and
3) The operation of the door with a single actuator islimited to 100 open/close cycles.
12 FEB 12MEL
A320/321MEL/CDL 01.52.29
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-30 Cargo Door
52-30-02 Cargo Door
Actuator
52-30-02B One or more
actuator
inoperative
C 4 0 (M) One or more may be inoperative provided that:
1) The integrity of the yellow hydraulic system is notaffected, and
2) The associated cargo door is manually closed and
locked.
MAINTENANCE PROCEDURE
Refer to AMM 52-36-00-040-001
52-30-03 Cargo Door
Electrical Control
52-30-03A Cargo door
operated using
hand pump
C 2 0 One or more may be inoperative provided that the
associated cargo doors can be operated using the hand
pump.
52-30-03B Cargo door considered
inoperative
C 2 0 (FD) One o r more m ay b e inoperative p rovided t hat t heassociated cargo doors are considered inoperative.
Refer to Item 52-30-01 Cargo Door (FWD, AFT)
52-30-04 Cargo Door
Locking Hooks
and Spools
(Rollers)
52-30-04A (Hooks)
(Spools)
C
C
14
14
11
11
(FD) A maximum of one locking hook or one spool per cargo
door may be inoperative provided that:
1) All the others have no damage, and
2) The flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Fligt Without Cabin
Pressurized.
Flight must be conducted in accordance with FOPM CH 8
Maintenance Ferry Flights.
01.52.30DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-30 Cargo Door
52-30-05 Cargo Door Hand
Pump
52-30-05A C 1 0 May be inoperative provided that the integrity of the yellow
hydraulic system is not affected.
52-30-06 Cargo Door Drift
Pin
52-30-06A A 4 0 One or both on each cargo door may be inoperative for
one flight.
52-30-07 Cargo Doors
Open/Locked
Indicator light
52-30-07A C 2 0 (O) One or both may be inoperative provided that the
associated cargo door is in the fully open position during
loading and unloading operations.
OPERATING PROCEDURES
ON GROUND
· When the Cargo Door Open/Locked Indicator light
is inoperative, it is necessary to inform the ground
personnel:
- To visually check that the affected cargo door is in the
fully open position, with no downward movement after
releasing the lever of the manual selector valve.
- To visually check that the lever of the manual selector
valve stays in the neutral position.
12 FEB 12MEL
A320/321MEL/CDL 01.52.31
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-33 Bulk Cargo
Compartment Door
52-33-01 Cargo Door
Balance
Mechanism
52-33-01A C 1 0 (M) May be inoperative or damaged provided that:
1) A safety hold device is used to maintain the cargo
door in the open position during loading andunloading operations, and
2) The associated cargo door is visually checked to beclosed and locked.
MAINTENANCE PROCEDURE
Refer to AMM 52-33-00-040-001
52-51 Reinforced Cockpit
Door (CDLS)
52-51-01 CDLS Normal
System (NormalControl Unit,
Switch and Lights
on the CKPT
DOOR Panel,
Buzzer, Keypad)
Note:
Any part of the CDLS may beinoperative provided the complete
system is deactivated in the unlocked
position and is not required by
operational regulations for the intended
flight.
52-51-01A CDLS back-up
control unit
operative
C 1 0 (O) May be inoperative provided that:
1) The interphone system between the cabin and thecockpit is operative, and
2) The LKG SYS selector on the CKPT DOOR BK UPpanel is set to the BK UP position , and
3) The CDLS back-up control unit is operative.
(Cont’d on next page)
01.52.32DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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52 DOORS
52-51 Reinforced
Cockpit Door
(CDLS)
52-51-01 CDLS Normal
System (Normal
Control Unit,
Switch and Lights
on the CKPT
DOOR Panel,
Buzzer, Keypad)
52-51-01A CDLS back-up
control unit
operative
(cont’d)
OPERATING PROCEDURES
PIC brief cabin crew before departure to use the cabin
interphone to communicate with the cockpit crew to
request access to the cockpit, and
A third crew member must be available in the cockpit
when a flight crew member leaves the cockpit during flight
DURING COCKPIT PREPARATION
LKG SYS sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BK UP
The CDLS keypad operation is not available in back-up
mode.
The cockpit crew must brief the cabin crew that the CDLS
keypad is inoperative.
IN FLIGHT
At least two people must always be present in the cockpitthroughout the entire flight.
12 FEB 12MEL
A320/321MEL/CDL 01.52.33
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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52 DOORS
52-51 Reinforced Cockpit
Door (CDLS)
52-51-02 CDLS BK UP
System (Back-up
Control Unit, CTL
pb and Lights on
the CKPT DOOR
BK UP Panel)
52-51-02A C 1 0 May be inoperative.
52-51-03 CDLS Buzzer
52-51-03A C 1 0 (O) May be inoperative provided:
1) Keypad is deactivated, and
2) Alternate procedures are established and used.
OPERATING PROCEDURES
Flight attendants shall be briefed not to use the keypad
and instead use interphone and pre-arranged knocks on
the door when entry is required.
52-51-04 CDLS Keypad
52-51-04A C 1 0 (O)(M)
(FD)
May be inoperative provided :
1) The interphone system between the cabin and thecockpit is operative, and
2) The keypad is deactived.
(Cont’d on next page)
01.52.34DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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52 DOORS
52-51 Reinforced
Cockpit Door
(CDLS)
52-51-04 CDLS Keypad
52-51-04A (Cont’d) OPERATING PROCEDURES
1. Flight attendants shall be briefed on an alternate flightdeck entry procedure which requires the use of cabin
interphone and a specified sequence of knocks on thedoor.
2. A third crew member must be available in the cockpitwhen a flight crew member leaves the cockpit duringflight.
MAINTENANCE PROCEDURE
Refer to AMM 52-51-00-040-007
52-51-05 CDLS Keypad
Green and RedLEDs
52-51-05A C 2 0 (O)(FD) May be inoperative provided alternate procedures are
established and used.
OPERATING PROCEDURES
1. Flight attendants shall be briefed on an alternate flightdeck entry procedure which requires the use of cabininterphone and a specified sequence of knocks on thedoor.
2. A third crew member must be available in the cockpitwhen a flight crew member leave the cockpit duringflight.
12 FEB 12MEL
A320/321MEL/CDL 01.52.35
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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52 DOORS
52-51 Reinforced Cockpit
Door (CDLS)
52-51-06 CDLS Door
Release Strike
(Catch, Spring,
Solenoid, Bolt)
52-51-06A C 3 2 (M) One may be inoperative provided associated door release
strike is deactivated or removed.
NOTE:
Application of the maintenance
procedure is only necessary when the
inoperative door release strike is failed
in locked position.
MAINTENANCE PROCEDURE
Refer to AMM 52-51-00-040-010
52-53 COCKPIT DOOR Panel
on the Center Pedestal
52-53-01 COCKPIT DOOR
FAULT light
52-53-01 B 1 0 (M) May be inoperative provided:
1) Automatic lock controls are verified operative, and
2) Door chime is operative.
MAINTENANCE PROCEDURE
Refer to AMM 52-51-00-810-801
01.52.36DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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52 DOORS
52-53 COCKPIT DOOR
Panel on the
Center Pedestal
52-53-02 COCKPIT DOOR
OPEN light
52-53-02A B 1 0 May be inoperative provided automatic lock controls are
verified operative.
52-53-03 LOCK Function of
the COCKPIT
DOOR sw
52-53-03A B 1 0 (O) May be inoperative provided:
1) The cockpit door locking system keypad isdeactivated.
2) Alternate procedures are established and used.
OPERATING PROCEDURES
Refer to MEL item 52-51-01A
52-53-04 UNLOCK Function
of the COCKPIT
DOOR sw
52-53-04A B 1 0 (O) May be inoperative provided alternate procedures are
established and used.
OPERATING PROCEDURES:
One additional crew member must lock or unlock the
cockpit door manually whenever access to the flight deckis granted or one of the crew leaves the cockpit.
* * *
01 MAY 12MEL
A320/321MEL/CDL 01.52.37
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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01.52.38DOORS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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56 WINDOWS
56-10 Cockpit
56-10-01 Front Windshield Note:
A cockpit window with minor damages
(as described in the associated
maintenance procedure) is considered
operative, but the vision through this
cockpit window must be acceptable to
the flight crew.
56-10-01C For SPS
Windshields
(P/N STA320-1-
3-1 and
STA320-2-3-1)
A 2 2 (O)(M)
(FD)
One front windshield external ply may be cracked for one
flight provided that:
1) The other front windshield is not damaged, and
2) The associated windshield heating is deactivated, and
3) The visibility through the associated front windshield isacceptable to the flight crew, and
4) The aircraft is not operated in known or forecast icingconditions.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
< When PF side is affected:
Maximum landing capability is CAT I
< When PNF side is affected:
Maximum landing capability is not affected and is still
CAT II.
MAINTENANCE PROCEDURE
Refer to AMM 56-10-00-040-001
12 FEB 12MEL
A320/321MEL/CDL 01.56.01
WINDOWS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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56 WINDOWS
56-10 Cockpit
56-10-01 Front Windshield
56-10-01D For SPS
Windshields
(only P/N
STA320-1-3-1
and STA320-2-
3-1)
C 2 2 (O)(M)
(FD)
One front windshield may have burn spots in the bus bar
area beyond the limits provided that:
1) The other front windshield is not damaged, and
2) The associated windshield heating is deactivated,and
3) The visibility through the associated front windshieldis acceptable to the flight crew, and
4) The aircraft is not operated in known or forecasticing conditions.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
< When PF side is affected:
Maximum landing capability is CAT I
< When PNF side is affected:
Maximum landing capability is not affected and is still
CAT II.
MAINTENANCE PROCEDURE
Refer to AMM 56-10-00-040-001
56-10-02 Lateral
Fixed/Sliding
Window
Note:
A cockpit window with minor damages
(as described in the associated
maintenance procedure) is consideredoperative, but the vision through this
cockpit window must be acceptable to
the flight crew.
01.56.02WINDOWS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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56 WINDOWS
56-10 Cockpit
56-10-03 Sliding Window
Opening/Closing
Mechanism
56-10-03A 2 2 Both must be operative.
56-20 Cabin
56-20-01 Cabin Window
56-20-01A (A320)
(A321)
A
A
36
44
30
40
(FD) One or more may be cracked for one flight day provided
that the flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Fligt Without Cabin
Pressurized.
Flight must be conducted in accordance with FOPM CH 8
Maintenance Ferry Flight
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.56.03
WINDOWS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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01.56.04WINDOWS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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70 ENGINE
70-00 MAINTENANCE
Messages on the
STATUS SD page
70-00-01 ENG FADEC
MAINTENANCE
Message
70-00-01B For Engines
Affected by
CFM VSB 73-
0241
A 1 - ENG FADEC MAINTENANCE message may be displayed
on the STATUS SD page for 25 flight hours or 3 days,
whichever occurs first.
70-00-01C For Engines
Affected by
CFM VSB 73-
0241
C 1 - (M) ENG FADEC MAINTENANCE message may be displayed
on the STATUS SD page provided it is checked before
the first flight of each day that the CFDS does not report
any fault on a T12 sensor.
MAINTENANCE PROCEDURE
Refer to AMM 73-29-00-040-001
70-00-02 ENG EIU
MAINTENANCEMessage
70-00-02A C 1 - ENG EIU MAINTENANCE message may be displayed on
the STATUS SD page.
70-00-03 ENG EVMU
MAINTENANCE
Message
70-00-03A C 1 - ENG EVMU MAINTENANCE message may be displayed
on the STATUS SD page.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.70.01
ENGINE
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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01.70.02ENGINE
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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73 ENGINE FUEL
AND CONTROL
73-07 Indications on the
ENGINE SD page
73-07-01 F. USED Indication
on the ENGINE SD
page
73-07-01A One indication
inoperative
C 2 1 One may be inoperative provided that the fuel quantity
indications of the associated tanks are operative on the
FUEL SD page.
73-07-02 Fuel Filter Clog
Indication on the
ENGINE SD page
73-07-02A C 2 0 One or both may be inoperative.
73-08 Indications on the
EWD
73-08-01 Fuel Flow
Indication on the
EWD
73-08-01A C 2 1 One may be inoperative.
12 FEB 12MEL
A320/321MEL/CDL
01.73.01ENGINE FUEL
AND CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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73 ENGINE FUEL
AND CONTROL
73-09 ECAM Alert
73-09-01 ENG 1(2) FUEL
FILTER CLOG
Alert
73-09-01A C 2 1 (M) One may be displayed provided that:
1) The alert is confirmed to be false by troubleshooting,
and2) The associated filter is replaced every day.
MAINTENANCE PROCEDURE
Refer to AMM 73-30-00-040-043
73-10 Distribution
73-10-01 Fuel Return Valve
73-10-01A Inoperative in
closed position
C 2 1 One may be inoperative in the closed position on one
engine provided that the APU and the AC auxiliary
generation are operative.
73-10-01B Inoperative in
open position
C 2 0 One or both may be inoperative in the open position
provided that the four wing tank pumps are operative.
73-10-03 Fuel Metering
Valve
73-10-03A 2 2 Both must be operative.
73-20 Controlling
73-20-01 Flex Takeoff
Mode
73-20-01A C 2 0 May be inoperative on one or both engines provided that
the maximum thrust is used for takeoff.
01.73.02ENGINE FUEL
AND CONTROL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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73 ENGINE FUEL
AND CONTROL
73-20 Controlling
73-20-05 Minimum Idle on
Ground
73-20-05A C 2 0 (O) One or both may be inoperative provided that the Flight
Manual performance penalties are applied.
OPERATING PROCEDURES (A321)
FLIGHT PREPARATION/LIMITATIONS
Takeoff performance:
For performance calculations request Modified Tailored
Takeoff and Landing charts (MTTL) from FPE through
Flight Dispatch or use the following penalties for takeoff
and landing performance determination if MTTL charts are
not available.
Takeoff must be performed with full thrust.
VMCG/VMCA limitation No VMCG/VMCAlimitation
Weight decrement (kg) 1300 400
V1, VR, V2 decrement
(kt IAS)0 2
Landing performance:
No penalty.
(Cont’d on next page)
30 JUN 12MEL
A320/321MEL/CDL
01.73.03ENGINE FUEL
AND CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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73 ENGINE FUEL
AND CONTROL
73-20 Controlling
73-20-05 Minimum Idle on
Ground
73-20-05A (cont’d) OPERATING PROCEDURES (A320)
FLIGHT PREPARATION/LIMITATIONS
Takeoff performance:
For performance calculations request Modified Tailored
Takeoff and Landing charts (MTTL) from FPE through
Flight Dispatch or use the following penalties for takeoff
and landing performance determination if MTTL charts are
not available..
Takeoff must be performed with full thrust.
VMCG/VMCA limitationNo VMCG/VMCA
limitation
Weight decrement (kg) 1500 200
V1, VR, V2 decrement
(kt IAS)0 1
Landing performance:
No penalty.
* * *
01.73.04ENGINE FUEL
AND CONTROL
A320/321MEL/CDL 30 JUN 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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74 IGNITION
74-07 Indications on the
ENGINE SD page
74-07-01 Selected Igniter
Indication on the
ENGINE SD page
74-07-01A C 4 0 (O) One or more may be inoperative provided that the
associated ENG 1(2) IGN A(B)(A+B) FAULT alert is
checked operative.
OPERATING PROCEDURES
AFTER ENGINE START
· If engine 1 is affected:
- ENGINE/1 AND 2/IGN/SYS A (49VU A03)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
- ENGINE/IGN/ENG 1/ SYS A BAT (121VU P39)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
- ENGINE/IGN/ENG 1/ SYS B (121VU P41)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
· If engine 2 is affected:
- ENGINE/1 AND 2/IGN/SYS A (49VU A03)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
- ENGINE/IGN/ENG 2/ SYS A BAT (121VU P40)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
- ENGINE/IGN/ENG 2/ SYS B (121VU P42)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.74.01
IGNITION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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74 IGNITION
74-07 Indications on the
ENGINE SD page
74-07-01 Selected Igniter
Indication on the
ENGINE SD page
74-07-01A (cont’d) OPERATING PROCEDURES (Cont’d)
On the EWD, check that the ENG 1(2) A+B IGN FAULT
alert is displayed.
· If engine 1 is affected:
- ENGINE/1 AND 2/IGN/SYS A (49VU A03)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
- ENGINE/IGN/ENG 1/ SYS A BAT (121VU P39)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
- ENGINE/IGN/ENG 1/ SYS B (121VU P41)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
· If engine 2 is affected:
- ENGINE/1 AND 2/IGN/SYS A (49VU A03)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
- ENGINE/IGN/ENG 2/ SYS A BAT (121VU P40)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
- ENGINE/IGN/ENG 2/ SYS B (121VU P42)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
01.74.02IGNITION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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74 IGNITION
74-09 ECAM Alert
74-09-01 ENG 1(2) IGN
A(B)(A+B) FAULT
Alert
74-09-01B One displayed C 4 3 (M) One may be displayed provided that the associated
engine ignition system is checked operative every day.
MAINTENANCE PROCEDURE
Refer to AMM 74-31-040-001
74-09-01C Two displayed C 4 2 (M) Two may be displayed provided that the associated
engine ignition systems are checked operative before
each flight.
MAINTENANCE PROCEDURE
Refer to AMM 74-31-040-001
74-31 Ignition Starting
and Continuous
Relight
74-31-01 Ignition System A
74-31-01A C 2 1 (O) One may be inoperative provided that the associated
engine ignition system B is operative.
OPERATING PROCEDURES
BEFORE ENGINE START
ENGINE/1 AND 2/IGN/SYS A (49 VU A03)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
AFTER ENGINE START
ENGINE/1 AND 2/IGN/SYS A (49 VU A03)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
12 FEB 12MEL
A320/321MEL/CDL 01.74.03
IGNITION
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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74 IGNITION
74-31 Ignition Starting and
Continuous Relight
74-31-02 Ignition System B
74-31-02A C 2 0 (O) One or both may be inoperative.
OPERATING PROCEDURES
BEFORE ENGINE START
ENGINE/IGN/ENG (1 and/or 2)/SYS B (121 VU P41/P42)
C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
* * *
01.74.04IGNITION
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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76 ENGINE CONTROLS
76-11 Throttle Control
76-11-01 Thrust lever
Position Sensor
76-11-01A A 4 3 One may be inoperative on one engine for three days
provided that:
1) The A/THR is operative, and
2) Both LGCIUs are operative, and
3) The L/G shock absorbers proximity detectors areoperative.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.76.01
ENGINE CONTROLS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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01.76.02ENGINE CONTROLS
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
I T E M
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77 ENGINE INDICATING
77-07 Indications on SD
pages
77-07-01 Indications on the
CRUISE SD page
77-07-01-01 N1 Vibration
Indication on the
CRUISE SD page
77-07-01-01A Refer to Item 77-07-02-05 N1 Vibration Indication on the
ENGINE SD page
77-07-01-02 N2 Vibration
Indication on the
CRUISE SD page
77-07-01-02A Refer to Item 77-07-02-06 N2 Vibration Indication on the
ENGINE SD page
77-07-01-03 F. USED (Fuel
Used) Indication
on the CRUISESD page
77-07-01-03A Refer to Item 73-07-01 Fuel Used Indication on the
ENGINE SD page
77-07-01-04 OIL QT (Oil
Quantity)
Indication on the
CRUISE SD page
77-07-01-04A Refer to Item 79-07-03 Oil Quantity Indication on the
ENGINE SD page
12 FEB 12MEL
A320/321MEL/CDL 01.77.01
ENGINE INDICATING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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77 ENGINE INDICATING
77-07 Indications on SD
pages
77-07-02 Indications on the
ENGINE SD page
77-07-02-01 Engine Bleed
Pressure
Indication on the
ENGINE SD
page
77-07-02-01A Refer to Item 36-07-04 Engine Bleed Precooler Inlet
Pressure Indication on the BLEED SD page
77-07-02-02 Fuel Filter Clog
Indication on the
ENGINE SD
page
77-07-02-02A Refer to Item 73-07-02 Fuel Filter CLOG Indication on the
ENGINE SD page
77-07-02-03 Fuel Used
Indication on the
ENGINE SD
page
77-07-02-03A Refer to Item 73-07-01 Fuel Used Indication on the
ENGINE SD page
77-07-02-04 Nacelle
Temperature
Indication on the
ENGINE SD
page
77-07-02-04A C 2 0 One or both may be inoperative.
01.77.02ENGINE INDICATING
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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77 ENGINE INDICATING
77-07 Indications on SD
pages
77-07-02 Indications on the
ENGINE SD page
77-07-02-05 N1 Vibration
Indication on the
ENGINE SD
page
77-07-02-05A One indication
inoperative
C 2 1 One may be inoperative.
77-07-02-05B Both indications
inoperative
A 2 0 Both may be inoperative for three flights provided that no
vibration advisory was displayed during the previous flight.
77-07-02-06 N2 Vibration
Indication on the
ENGINE SD
page
77-07-02-06A One indicationinoperative
C 2 1 One may be inoperative.
77-07-02-06B Both indications
inoperative
A 2 0 Both may be inoperative for three flights provided that no
vibration advisory was displayed during the previous flight.
77-07-02-07 Oil Filter Clog
Indication on the
ENGINE SD
page
77-07-02-07A Refer to Item 79-07-01 CLOG Indication on the ENGINE
SD page
12 FEB 12MEL
A320/321MEL/CDL 01.77.03
ENGINE INDICATING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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77 ENGINE INDICATING
77-07 Indications on SD
pages
77-07-02 Indications on the
ENGINE SD page
(cont’d)
77-07-02-08 Oil Pressure
Indication on the
ENGINE SD
page
77-07-02-08A Refer to Item 79-07-02 Oil Pressure Indication and
Advisory on the ENGINE SD page
77-07-02-09 Oil Quantity
Indication on the
ENGINE SD
page
77-07-02-09A Refer to Item 79-07-03 Oil Quantity Indication on the
ENGINE SD page
77-07-02-10 Oil Temperature
Indication on the
ENGINE SD
page
77-07-02-10A Refer to Item 79-07-04 Oil Temperature Indication on the
ENGINE SD page
77-07-02-11 Selected Igniter
Indication on the
ENGINE SD
page
77-07-02-11A Refer to Item 74-07-01 Selected Igniter Indication on the
ENGINE SD page
01.77.04ENGINE INDICATING
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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77 ENGINE INDICATING
77-07 Indications on SD
pages (cont’d)
77-07-02 Indications on the
ENGINE SD page
77-07-02-12 Start Valve
Position
Indication on the
ENGINE SD
page
77-07-02-12A Refer to Item 80-07-01 Start Valve Position Indication on
the ENGINE SD page
77-08 Indications on the
EWD
77-08-01 EGT Indication on
the EWD
77-08-01A 2 2 Must be operative.
77-08-03 Fuel Flow
Indication on the
EWD
77-08-03A Refer to Item 73-08-01 Fuel Flow Indication on the EWD
77-08-04 N1 Indication on
the EWD
77-08-04A 2 2 Must be operative.
77-08-05 N2 Indication on
the EWD
77-08-05A 2 2 Must be operative.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.77.05
ENGINE INDICATING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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01.77.06ENGINE INDICATING
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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78 EXHAUST
78-08 Indications on the
EWD
78-08-01 REV Indication on
the EWD
78-08-01A - 2 2 Both must be operative.
78-30 Thrust Reversers
78-30-01 Thrust Reverser
78-30-01A C 2 1 (O)(M)
(FD)
One may be inoperative provided that:
1) The inoperative thrust reverser is deactivated andsecured in the stowed position, and
2) All stow and deploy switches circuits on theinoperative thrust reverser are checked operative, and
3) The ENG 1(2) REV PRESSURIZED alert is notdisplayed on the EWD after deactivation, and
4) The appropriate performance adjustments are applied.
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.78.01
EXHAUST
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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78 EXHAUST
78-30 Thrust Reversers
78-30-01 Thrust Reverser
78-30-01A (cont’d) OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS
Performance Adjustments:
One Thrust
Reverser
Inoperative
Runway State Performance Adjustments
Takeoff Dry, or
Landing Dry, or
Landing Wet
No performance adjustments are
necessary (Basic performance data is
computed without thrust reversers)
Takeoff Wet
Use performance data computed with :
- One thrust reverser inoperative.
(Refer to SV A320/321
Performance Manual CH 12)
FOR TAKEOFF
During the takeoff briefing, the flight crew must
review:
- The status of the thrust reversers, and
- The use of the thrust reversers
(Cont’d on next page)
01.78.02EXHAUST
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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78 EXHAUST
78-30 Thrust Reversers
78-30-01 Thrust Reverser
78-30-01A (cont’d) OPERATING PROCEDURES (cont’d)
REJECTED TAKEOFF
Ensure that both engine thrust levers are set to IDLE
detent, then:
· If one thrust reverser is inoperative:
Use both thrust levers when applying reverse thrust.
Note:
ENG (AFFECTED SIDE) REVERSER
FAULT alert is displayed on the EWD
after selection of the reverse thrust.
IN FLIGHT
· Should a failure occur with "LDG DIST
PROC.......APPLY" message displayed on the STATUS
SD page,
and
Whatever the actual thrust reversers selection at
landing:
To calculate the LDG DIST with the in-flight failure, use,
as a conservative approach, the LDG DIST factors
“WITHOUT REV” (LDG CONF/APP SPD/LDG DISTFOLLOWING FAILURES tables in the QRH part 2).
(Cont’d on next page)
12 FEB 12MEL
A320/321MEL/CDL 01.78.03
EXHAUST
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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78 EXHAUST
78-30 Thrust Reversers
78-30-01 Thrust Reverser
78-30-01A (cont’d) OPERATING PROCEDURES (cont’d)
DURING APPROACH
During the approach briefing, the flight crew must
review:
- The status of the thrust reversers, and
- The use of the thrust reversers
FOR LANDING
Before the touchdown, ensure that both engine thrust
levers are set to IDLE detent for the flare.
· After touchdown, if one thrust reverser is
inoperative:
Use both thrust levers when applying reverse thrust.
Note:
ENG (AFFECTED SIDE) REVERSER
FAULT alert is displayed on the EWD
after selection of the reverse thrust.
MAINTENANCE PROCEDURE
Refer to AMM 78-30-00-040-040
01.78.04EXHAUST
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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78 EXHAUST
78-30 Thrust Reversers
78-30-02 Thrust Reverser
Inhibition Relay
sw
78-30-02A C 4 2 Two may be inoperative provided that the associated
thrust reverser is considered inoperative.
Refer to Item 78-30-01 Thrust Reverser
78-30-03 Thrust Reverser
Shutoff Valve
78-30-03A C 2 0 One or both may be inoperative in the open position.
* * *
12 FEB 12MEL
A320/321MEL/CDL 01.78.05
EXHAUST
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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01.78.06EXHAUST
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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79 OIL
79-07 Indications on the
ENGINE SD page
79-07-01 CLOG Indication
on the ENGINE SD
page
79-07-01A C 2 1 One may be inoperative.
79-07-02 Oil Pressure
Indication and
Advisory on the
ENGINE SD page
Note:
Simultaneous illumination of the BLUE
ELEC PUMP pb-sw FAULT light and the
ENG 1(2)PUMP pb-sw FAULT light with
engines off may be due to a failed
engine oil low pressure switch. In this
case, the ENG 1(2) OIL LO PR alert is
inoperative.
Refer to Item 79-09-01 ENG 1(2) OIL
LO PR Alert
79-07-02A Associated
thrust reverser
checked
operative
C 2 1 (M) One may be inoperative provided that:
1) The associated ENG 1(2) OIL LO PR alert isoperative, and
2) The associated oil quantity indication is operative onthe ENGINE SD page, and
3) The associated thrust reverser is checked operative.
MAINTENANCE PROCEDURE
Refer to AMM task
79-07-02B Associated
thrust reverser
considered
inoperative
C 2 1 One may be inoperative provided that:
1) The associated ENG 1(2) OIL LO PR alert is
operative, and2) The associated oil quantity indication is operative on
the ENGINE SD page, and
3) The associated thrust reverser is consideredinoperative.
Refer to Item 78-30-01 Thrust Reverser
12 FEB 12MEL
A320/321MEL/CDL 01.79.01
OIL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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79 OIL
79-07 Indications on the
ENGINE SD page
(cont’d)
79-07-03 Oil Quantity
Indication on the
ENGINE SD page
79-07-03A C 2 1 (M) One may be inoperative provided that the associated oil
quantity is checked before each flight.
MAINTENANCE PROCEDURE
Refer to AMM 79-31-00-040-042
79-07-04 Oil Temperature
Indication on the
ENGINE SD page
79-07-04A 2 2 Must be operative.
79-09 ECAM Alerts
79-09-01 ENG 1(2) OIL LO
PR Alert
79-09-01A C 2 0 (O) One or both may be displayed.
OPERATING PROCEDURES
AFTER ENGINE START
· If both engines are affected:
RCDR GND CTL pb-sw . . . . . . . . . . . . . . . . . .CHECK ON
01.79.02OIL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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79 OIL
79-09 ECAM Alerts
79-09-02 ENG 1(2) OIL
FILTER CLOG
Alert
79-09-02B Inspection of
the visual
indicator (pop-
out) of the
electrical
master chip
detector
C 2 1 (M) One may be displayed provided that:
1) The associated filter is replaced every day, and
2) The visual indicator (pop-out) of the electrical master chip detector is checked operative before the firstMMEL dispatch, and
3) The visual indicator (pop-out) of the electrical master chip detector is inspected when the filter is replacedand does not reveal the presence of chips.
MAINTENANCE PROCEDURE
Refer to AMM 79-35-00-040-042
79-09-02C Inspection of
the electricalmaster chip
detector
C 2 1 (M) One may be displayed provided that:
1) The associated filter is replaced every day, and
2) The electrical master chip detector is inspected whenthe filter is replaced and does not reveal the presenceof chips.
MAINTENANCE PROCEDURE
Refer to AMM 79-35-00-040-044
12 FEB 12MEL
A320/321MEL/CDL 01.79.03
OIL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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79 OIL
79-20 Distribution
79-20-02 EMCD Visual Pop-
Out Indicator
79-20-02A C 2 0 One or both may be inoperative.
79-40 IDG Oil Cooling
System
79-40-01 Fuel Return Valve
79-40-01A Refer to Item 73-10-01 Fuel Return Valve
* * *
01.79.04OIL
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
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80 STARTING
80-01 ENG MAN START
Overhead Panel
80-01-31 ENG MAN START
pb-sw
80-01-31A C 2 0 One or both may be inoperative.
80-07 Indication on the
ENGINE SD page
80-07-01 Start Valve
Position Indication
on the ENGINE SD
page
80-07-01A C 2 1 (M) One may be inoperative provided that the start valve is
checked closed after the engine start.
MAINTENANCE PROCEDURE
Refer to AMM 80-11-00-040-044
80-11 Pneumatic Starter and Valve System
80-11-01 Start Valve
80-11-01A C 2 1 (O)(M) O ne may be inoperative provided that the start valve is
manually closed after the start of the affected engine.
OPERATING PROCEDURES
BEFORE ENGINE START
Refer to FCOM/PRO-SUP-70 START VALVE MANUAL
OPERATION.
MAINTENANCE PROCEDURE
Refer to AMM 80-11-00-040-045
12 FEB 12MEL
A320/321MEL/CDL 01.80.01
STARTING
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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80 STARTING
80-12 ENG MASTER Panel
on the Center
Pedestal
80-12-01 FAULT light on the
ENG MASTER
Panel
80-12-01A C 2 0 One or both may be inoperative.
* * *
01.80.02STARTING
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
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ITEM PAGE
CDL INTRODUCTION
- - - - - CDL INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.01.01
LIMITATIONS
DISPATCH FUEL PENALTY
WEIGHT REDUCTIONS
SPEED CALCULATION AND RESTRICTIONS
ENROUTE DIVERSION SPEED EFFECTS
GENERAL LOCATION PICTURES & PERFORMANCE
ATA 21 - AIR CONDITIONING
21-01 Ram air inlet flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.21.01
21-03 Ram air inle leading Edge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.02
ATA 23 - COMMUNICATIONS
23-01 Static Discharger . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.23.01
ATA 27 - FLIGHT CONTROL
27-01 Flap Track Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.01
27-02 Flap Track Fairing 1A Extension . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.03
27-03 Slat Track Closing Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.04
27-05 Access Panel For Bearings At Elevator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.05
27-06 Flat Track Fairing Rear Top Cover And Tail Cone . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.06
27-07 Rubber Seal Under Slat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.07
27-08 Seal Between Inboard And Outboard Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.08
27-09 Inboard Aileron Edge To Wing Seal. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.10
27-10 Slat End Seal And Weather Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.11
27-11 Slat Track Filler Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.12
27-12 Slat Track Sealing Packer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.13
27-13 Inter-flap Cushion Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.14
27-14 Flap Track Movable Fairing Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.15
27-15 Flap Track Fixed Fairing Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.16
27-16 Flap Track Movable Fairing Pivot Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.17
27-17 Flap Tab Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.18
ATA 28- FUEL
28-01 Refuel /defuel coupling CAP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.01
28-02 Refuel Panel Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.02
12 FEB 12CDL
A320/321MEL/CDL
02.00TABLE OF CONTEN
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ITEM PAGE
ATA 30 - ICE AND RAIN PROTECTION
30-01 Icing indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.30.01
ATA 32 - LANDING GEAR
32-03 Nose wheel hubcap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.01
32-04 Nose fitting towing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.02
ATA 33 - LIGHTS
33-01 Wing / Engine / Scan Light Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.01
33-02 Taxi Light lamp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.02
33-03 Rear navigation light lens. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.03
33-04 Upper and lower anti-collision (Beacon) light Cover . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.04
33-05 Logo light lens (Cover) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.06
33-07 Landing light lens . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.07
33-08 Turn OFF light lamp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.08
33-09 Takeoff light lamp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.09
ATA 49 - APU
49-01 APU overpressure release door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.49.01
ATA 51- STRUCTURE
51-01 Random conductive Strip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.01
51-02 Passenger door Scuff Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.02
51-03 Bulk cargo door Scuff Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.0351-04 Fairing AFT Safety Stay Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.04
02.00.02TABLE OF CONTENTS
A320/321MEL/CDL 12 FEB 12
CDL
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ITEM PAGE
ATA 52 - DOORS
52-01 Toilet sem rvicing door and drainage. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.01
52-02 Access door to hydraulic ground connectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.03
52-03 access door to potable water filling and drainage . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.05
52-04 access door to opening control of landing gear doors on ground . . . . . . . . . . . . . . . 02.52.07
52-05 access door to air conditioning ground supply. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.09
52-06 Forward jacking point access door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.11
52-07 External power ground connection access door ASSY . . . . . . . . . . . . . . . . . . . . . . . 02.52.13
52-08 Access door of cargo opening system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.14
52-09 Nose landing gear main . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.15
52-10 Nose landing gear aft doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.17
52-11 Nose landing gear leg doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.19
52-12 Main landing gear door (732, 742) (Flight with gear up) . . . . . . . . . . . . . . . . . . . . . . 02.52.21
52-13 Main landing gear door (733, 743) (Flight with gear up) . . . . . . . . . . . . . . . . . . . . . . 02.52.23
52-14 Main landing gear door (732, 742) (Flight with gear down) . . . . . . . . . . . . . . . . . . . . 02.52.25
52-15 Main landing gear door (733, 743) (Flight with gear down) . . . . . . . . . . . . . . . . . . . . 02.52.27
52-16 Main landing gear door (734, 744) (Flight with gear down) . . . . . . . . . . . . . . . . . . . . 02.52.29
52-18 Main landing gear door: Seal on secondary hinged fairing . . . . . . . . . . . . . . . . . . . . 02.52.31
52-19 Pax door upper cover plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.32
52-20 Access door to HP air ground connector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.33
52-21 Blue hydraulic access door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.35
52-22 Forward cargo door access cover panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.36
52-23 Aft cargo door access cover panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.37
ATA 53 - FUSELAGE
53-01 Belly Fairing Vent Louver Vanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.01
53-03 Root Fillet Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.03
ATA 54 - NACELLES / PYLON
54-01 Nacelle Strakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.01
54-03 Pylon Pressure relief door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.0354-04 Pylon Access Doors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.05
54-05 Pylon Fairing Seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.06
54-06 Aerodynamic Seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.07
12 FEB 12CDL
A320/321MEL/CDL
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ATA 57 - WINGS
57-01 Wing tip fences. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.01
57-02 Belly Fairing Sliding Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.03
57-03 Outboard Flaps Rubbing Strip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.04
ATA 71 - POWER PLANT
71-01 Frangible Drain Mast . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.01
71-09 Fan Cowl Hold Open Rod . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.02
ATA 78 - EXHAUST
78-09 Thrust reverser 11 and 1 O,clock Struts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.78.01
* * *
02.00.04TABLE OF CONTENTS
A320/321MEL/CDL
12 FEB 12CDL
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CDL Introduction
The Configuration Deviation List presented in this manual isa reproduction of the FAA-approved CDL in the Aircraft
Flight Manual (AFM). The numbering and designation of system in this CDL is based on ATA specification 100. Theparts within each systems are identified by functionaldescription, and when necessary by part number(s).
CDL General Limitations
The associated limitations for each applied CDL item mustbe listed on placard(s) affixed in the cockpit in clear view toboth pilots. The pilot in command shall be notified whenever a CDL restriction(s) exists by listing the CDL number in theflight dispatch release.
The maintenance log book briefing card must include a data
reflecting all imposed CDL(s). An appropriate inspectionnotation covering the missing part(s) must be noted onaircraft maintenance logbook before each flight.
If an additional part is lost in flight, the aircraftmay not departthe airport at which it landed following this event until it againcomplies with the appropriate CDL limitation. This, of course, does not preclude the issuance of a maintenanceferry authorization to allow the aircraft to be flown to a pointwhere the necessaryrepairs or replacements can be made.
No more than one part for any one system in this CDL maybe missing, unless specifically designated combinations areindicated.
The performance penalties are cumulative. Whereperformance penalties are listed as “NEGLIGIBLE”, nomore than three negligible items may be missing withoutapplying weight penalty. For each missing item in excess of three, the maximum performance limited weight for takeoff,enroute, and landing must be reduced by 50 kg.
Where performance penalties are not listed, anyaccumulative number of sub-systems may be missingwithout further penalty.
All CDL items must be relayed to the controlling dispatchcenter prior to departure.
Dispatch Fuel Penalty
The performance increase in the fuel must be applied to theminimum dispatch fuel requirement.
Minimum dispatch fuel required is the sum of trip fuel,alternate fuel and reserve fuel.
Weight Reductions
The MEL weight reductions must be applied to thmaximum performance limited weights, as follows:
1. Takeoff - Weight penalty is applied to the morestrictive of the Zero Wind weight o
Climb Limit weight.
2. Enroute - Weight penalty is applied to cruise an
one engine inoperative Altitud
Capability limited weights.
3. Landing - Weight penalty is applied to the mos
restrictive of tailored landing charts
field length or landing climb limite
weight.
Speed Calculation, and Restrictions
When takeoff weight penalty is imposed, determintakeoff speed with reference to the sum of actual aircragross weight plus the imposed takeoff weight penalty.
When landing weight penalty is imposed, the Vref, anthe minimum maneuvering speeds must be determinewith reference to the actual aircraft gross weight, plus thimposed landing weight penalty.
Operation with those missing item(s) requiring reduction of VMO/MMO is only permitted when th
appropriate alternate VMO set prior to flight.
Performance
Performance determination method.
There are two approved ways of determining thperformance impact on CDL items missing:
- Using CDL chapter of the Airplane Flight Manual, or- Using AFM_OCTO software.
If no performance data are available in OCTO_AFM forgiven item listed in this CDL chapter, the penaltie
published in this CDL chapter must be used.
These takeoff, en-route and landing penalties apply most limiting corresponding weight.
Takeoff and approach climb performance limiting weighare reduced by 50 kg
( Cont'd on next page )
12 FEB 12CDL
A320/321MEL/CDL
02.01.0CDL INTRODUCTIO
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(Cont'd)
One engine inoperative net ceiling is reduced by 60 ft (i.e.
Corresponding to 60 kg decrease of en-route performancelimiting weight.
CAUTION
The most limiting performance between the one computedwith itemsmissing and the one computed without item missing must beused.
* * *
02.01.02CDL INTRODUCTION
A320/321MEL/CDL 12 FEB 12
CDL
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21 AIR CONDITIONING
21-01 RAM AIR INLET
FLAP
2 0 All may be missing.
Note:
System performance in heating mode
will be decreased.
Performance:
The following performance penalties are applicable per
missing flap:
- Takeoff and approach climb performance limitingweights are reduced by 190 kg
- En route performance limiting weight is reduced by216 kg
- Fuel consumption is increased by 0.53 %.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.21.01
AIR CONDITIONING
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21 AIR CONDITIONING
21-03 RAM AIR INLET
LEADING EDGE
2 1 One may be missing provided the associated pack is
turned off (Refer to MEL/MI-21-52 Air Conditioning Pack).
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
02.21.02 AIR CONDITIONING
A320/321MEL/CDL 12 FEB 12
CDL
ITEM
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23 COMMUNICATION
23-01 STATIC
DISCHARGER
39 32 20 % of static dischargers may be missing or inoperative
on each the following areas:
- RH wing
- LH wing
- Vertical stabilizer (including rudder)
- RH horizontal stabilizer (including elevator)
- LH horizontal stabilizer (including elevator).
Note:
i. If a static discharger is missing or
inoperative on a flap track fairing, it
is recommended to replace it before
flight.
ii. When combined with the case of
dispatch with a wing tip fence
missing, 20 % of the remaining static
dischargers of the affected wing are
allowed to be inoperative or missing
(Refer to 57-01 Wing Tip Fence).
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.23.01
COMMUNICATION
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23 COMMUNICATION
23-01 STATIC DISCHARGER
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
02.23.02COMMUNICATION
A320/321MEL/CDL 12 FEB 12
CDL
ITEM
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27 FLIGHT CONTROL
27-01 FLAP TRACK
FAIRING
6 7 (M) One fairing may be partly or completely missing.
Note:
i. When the forward part of the fairing
is missing, the aft part must be
removed.
ii. When the aft part of the fairing is
missing, the forward part may remaininstalled.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 1 430 kg
- En route performance limiting weight is reduced by 1575 kg
- Fuel consumption is increased by 2.81 %.
MAINTENANCE PROCEDURES
Refer to AMM 57-55-00-040-001
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.27.01
FLIGHT CONTROL
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27 FLIGHT CONTROL
27-01 FLAP TRACK FAIRING
(Cont’d)
02.27.02FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-02 FLAP TRACK
FAIRING 1A
EXTENSION
2 0 All may be missing.
Performance:
The following performance penalties are applicable per
missing extension:
- Takeoff and approach climb performance limitingweights are reduced by 120 kg
- En route performance limiting weight is reduced by131 kg
- Fuel consumption is increased by 0.26 %.
12 FEB 12CDL
A320/321MEL/CDL 02.27.03
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
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27 FLIGHT CONTROL
27-03 SLAT TRACK
CLOSING PLATE
24 22 Two may be missing.
02.27.04FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-05 ACCESS PANEL
FOR BEARINGS
AT ELEVATOR
8 6 Two may be missing.
12 FEB 12CDL
A320/321MEL/CDL 02.27.05
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-06 FLAP TRACK FAIRING
REAR TOP COVER
AND TAIL CONE
6 4 (M) Both may be missing on two flap track fairings.
Note:
i. When the tail cone is missing, the
rear top cover may remain installed.
ii. When the rear top cover is missing,
the associated tail cone must be
removed.
MAINTENANCE PROCEDURES
Refer to AMM 57-55-00-040-002
02.27.06FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-07 RUBBER SEAL
UNDER SLAT
10 0 (M) 1 m per slat may be missing.
MAINTENANCE PROCEDURES
Refer to AMM 57-40-00-040-001
12 FEB 12CDL
A320/321MEL/CDL 02.27.07
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-08 SEAL BETWEEN
INBOARD AND
OUTBOARD FLAP
6 3 Three may be missing.
Note:
For dispatch with inter-flap cushion seal
missing, Refer to 27-13 Inter-flap
Cushion Seal.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 63 kg per missing seal
- En route performance limiting weight is reduced by 72kg (159 lb) per missing seal
- If two or more seals are missing, fuel consumption isincreased by 0.16 % per missing seal.
(Cont’d on next page)
02.27.08FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-08 SEAL BETWEEN
INBOARD AND
OUTBOARD FLAP
(Cont’d)
12 FEB 12CDL
A320/321MEL/CDL 02.27.09
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-09 INBOARD AILERON
EDGE TO WING SEAL
4 2 One seal per aileron may be partially or completely
missing provided that any loose or flapping seal material
is cut off.
02.27.10FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-10 SLAT END SEAL
AND WEATHER
SEAL
12 10 One seal per wing may be partially or completely missing
provided any loose or flapping seal material is cut off.
12 FEB 12CDL
A320/321MEL/CDL 02.27.11
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-11 SLAT TRACK FILLER
BLOCK
6 0 All may be missing.
Note:
May be combined with MCDL item 27-
12 (Refer to 27-12 Slat Track Sealing
Packer).
02.27.12FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-12 SLAT TRACK
SEALING PACKER
4 0 All may be missing.
Note:
May be combined with MCDL item 27-
11 (Refer to 27-11 Slat Track Filler
Block).
12 FEB 12CDL
A320/321MEL/CDL 02.27.13
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-13 INTER-FLAP CUSHION
SEAL
4 2 One cushion seal may be missing per wing.
02.27.14FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-14 FLAP TRACK
MOVEABLE
FAIRING SEAL
12 6 (M) 50 % of the seal length may be missing on each side of
the flap track fairing for 100 flight hours provided that a
visual inspection is performed before each flight to ensure
there is no flapping seal on the aircraft.
Note:
May be combined with MCDL item 27-
15 (Refer to 27-15 Flap Track Fixed
Fairing Seal).
MAINTENANCE PROCEDURES
Refer to AMM 57-55-00-040-004
12 FEB 12CDL
A320/321MEL/CDL 02.27.15
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-15 FLAP TRACK FIXED
FAIRING SEAL
18 0 (M) All may be missing provided the hole is covered with high
speed tape.
Note:
May be combined with MCDL item 27-
14 (Refer to 27-14 Flap Track Moveable
Fairing Seal).
MAINTENANCE PROCEDURES
Refer to AMM 57-55-00-040-004
02.27.16FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-16 FLAP TRACK
MOVEABLE
FAIRING PIVOT
COVER
12 0 (M) All may be missing provided the hole is covered with high
speed tape.
Note:
A visual inspection must be performed
daily to ensure that tape is still in
position and in good condition.
12 FEB 12CDL
A320/321MEL/CDL 02.27.17
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-17 FLAP TAB FAIRING 10 9 One fairing may be partly or completely missing.
Note:
i. When the forward part of the fairing
is missing, the aft part must be
removed.
ii. When the aft part of the fairing is
missing, the forward part may remain
installed.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 143 kg
- En route performance limiting weight is reduced by158 kg
- Fuel consumption is increased by 0.32 %.
(Cont’d on next page)
02.27.18FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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27 FLIGHT CONTROL
27-17 FLAP TAB
FAIRING
(Cont’d)
* * *
12 FEB 12CDL
A320/321MEL/CDL 02.27.19
FLIGHT CONTROL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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02.27.20FLIGHT CONTROL
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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28 FUEL
28-01 REFUEL/DEFUEL
COUPLING CAP
101 QM OR 41 QM
2 0 (M) All may be missing provided seal integrity of coupling is
positively confirmed (i.e. no fuel leak reported).
Note:
i. If the coupling or O-ring is damaged
and the cap cannot be fitted,
dispatch is permitted in accordance
with this CDL item provided the cap
is removed and coupling integrity is
verified.
ii. If only the lanyard is missing, the
removal of the cap is not necessary.
MAINTENANCE PROCEDURES
Refer to AMM 28-25-00-040-003
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.28.01
FUEL
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28 FUEL
28-02 REFUEL PANEL DOOR 1 0 (M) Belly fairing mounted refuel panel door 192 MB may be
missing.
Note:
If belly fairing mounted refuel panel door
192 MB is not installed, underwing
mounted refuel panel doors (622KB,
522KB) must not be missing
MAINTENANCE PROCEDURES
Refer to AMM 52-42-00-040-001
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
02.28.02FUEL
A320/321MEL/CDL 12 FEB 12
CDL
ITEM
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30 ICE AND RAIN PROTECTION
30-01 ICING INDICATOR 1 0 May be missing.
Procedures:
- If icing conditions expected:
For icing conditions definition, Refer to LIM-GEN IcingConditions Definition.Turn on engine and wing anti-ice.
* * *
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.30.01
ICE AND RAIN PROTECTION
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02.30.02ICE AND RAIN PROTECTION
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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32 LANDING GEAR
32-03 Nose wheel hubcap 2 1 (M) One may be missing.
MAINTENANCE PROCEDURES
Refer to AMM 32-41-00-040-001
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.32.01
LANDING GEAR
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32 LANDING GEAR
32-04 Nose Fitting Towing 1 0 (M) May be missing
MAINTENANCE PROCEDURES
Refer to AMM 32-21-00-040-001
* * *
02.32.02LANDING GEAR
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-01 WING/ENGINE
SCAN LIGHT
COVER 3LX, 4LX
2 1 (M) One may be missing provided the hole is covered with
high speed tape.
Note:
If non transparent high speed tape is
used, the affected light must be
deactivated (Refer to MEL/MI-33-40
Wing Scan light).
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.33.01
LIGHTS
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33 LIGHTS
33-02 TAXI LIGHT LAMP 8LR 1 0 (M) May be missing provided the hole is covered with high
speed tape and the affected light is deactivated (Refer to
MEL/MI-33-40 Taxi and Takeoff light).
MAINTENANCE PROCEDURES
Refer to AMM 33-46-00-040-001
02.33.02LIGHTS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-03 REAR
NAVIGATION
LIGHT LENS 15LA
1 0 (M) May be missing for 5 flight cycles provided visual
inspection is performed before each flight to check that
there is no structural buckling.
MAINTENANCE PROCEDURES
Refer to AMM 33-41-00-040-002
12 FEB 12CDL
A320/321MEL/CDL 02.33.03
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-04 UPPER 7LV AND
LOWER 6LV ANTI-
COLLISION (BEACON)
LIGHT COVER
2 0 (M) All may be missing provided the lamp is covered with high
speed tape and affected light is deactivated (Refer to
MMEL/MI-33-40 Beacon light).
Performance:
If upper and lower light covers are missing, the following
performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 80 kg
- En route performance limiting weight is reduced by 90kg
- Fuel consumption is increased by 0.22 %.
MAINTENANCE PROCEDURES
Refer to AMM 33-48-00-040-001
(Cont’d on next page)
02.33.04LIGHTS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-04 UPPER 7LV AND
LOWER 6LV ANTI-
COLLISION
(BEACON) LIGHT
COVER (Cont’d)
12 FEB 12CDL
A320/321MEL/CDL 02.33.05
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-05 LOGO LIGHT LENS
(COVER) 3LY, 4LY
2 0 (M) All may be missing provided the hole is covered with high
speed tape.
Note:
If non transparent high speed tape is
used, the affected light must be
deactivated.
(Refer to MEL/MI-33-40 Logo light).
MAINTENANCE PROCEDURES
Refer to AMM 33-47-00-040-001
02.33.06LIGHTS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-07 LANDING LIGHT
LENS 7LB, 8LB
2 1 (M) One may be missing provided the associated light is
retracted and deactivated and the hole is covered with
high speed tape (Refer to MEL/MI-33-40 Landing light).
MAINTENANCE PROCEDURES
Refer to AMM 33-42-00-040-001
12 FEB 12CDL
A320/321MEL/CDL 02.33.07
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-08 TURN OFF LIGHT
LAMP 3LC1, 3LC2
2 0 (M) All may be missing provided the hole is covered with high
speed tape and the affected light is deactivated (Refer to
MEL/MI-33-40 Runway Turnoff light).
MAINTENANCE PROCEDURES
Refer to AMM 33-43-00-040-002
02.33.08LIGHTS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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33 LIGHTS
33-09 TAKEOFF LIGHT
LAMP 7LR
1 0 (M) May be missing provided the hole is covered with high
speed tape and the affected light is deactivated (Refer to
MEL/MI-33-40 Taxi and Takeoff light).
MAINTENANCE PROCEDURES
Refer to AMM 33-46-00-040-002
* * *
12 FEB 12CDL
A320/321MEL/CDL 02.33.09
LIGHTS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
02.33.10LIGHTS
A320/321MEL/CDL 12 FEB 12
CDL
ITEM
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49 A PU
49-01 APU
OVERPRESSURE
RELEASE DOOR
1 0 May be missing provided APU is not used in flight and on
ground.
Limitations:
Flights for which APU is mandatory are not allowed.
* * *
12 FEB 12CDL
A320/321MEL/CDL 02.49.01
APU
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
02.49.02 APU
A320/321MEL/CDL 12 FEB 12
CDL
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51 STRUCTURE
51-01 RADOME
CONDUCTIVE
STRIP
8 7 One may be missing.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.51.01
STRUCTURE
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51 STRUCTURE
51-02 PASSENGER DOOR
SCUFF PLATE
4
8
0
0
All may be missing.
02.51.02STRUCTURE
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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51 STRUCTURE
51-03 BULK CARGO
DOOR SCUFF
PLATE
1 0 May be missing.
12 FEB 12CDL
A320/321MEL/CDL 02.51.03
STRUCTURE
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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51 STRUCTURE
51-04 FAIRING AFT SAFETY
STAY POINT 311 AL
1 0 May be missing.
* * *
02.51.04STRUCTURE
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-01 TOILET SERVICING
AND DRAINAGE
DOOR 172 AR
1 0 (M) May be missing.
Note:
i. Toilet system is inoperative on
ground.
ii. May be combined with MCDL items:
- 52-02 (Refer to 52-02 Access
Door to Hydraulic Ground
Connectors 197 CB - 197 EB -198 CB)
- 52-03 (Refer to 52-03 Access
Door to Potable Water Filling
and Drainage)
- 52-04 (Refer to 52-04 Access
Door to Opening Control of
Landing Gear Doors on Ground
195 BB - 196 BB)
- 52-05 (Refer to 52-05 Access
Door to Air Conditioning Ground
Supply 191 CB)
- 52-06 (Refer to 52-06 Forward
Jacking Point Access Door)- 52-20 (Refer to 52-20 Access
Door to HP Air Ground
Connector 191 DB).
Performance:
The following performance penalties are applicable:
- Takeoff and approach performance limiting weightsare reduced by 63 kg
En-route performance limiting weight is reduced by 72kg.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.52.01
DOORS
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52 DOORS
52-01 TOILET SERVICING
AND DRAINAGE
DOOR 172 AR
(Cont’d)
02.52.02DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-02 ACCESS DOOR TO
HYDRAULIC
GROUND
CONNECTORS 197
CB - 197 EB - 198 CB
3 2 One may be missing.
Note:
May be combined with MCDL items:
- 52-01 (Refer to 52-01 Toilet
Servicing and Drainage Door )
- 52-03 (Refer to 52-03 Access Door
to Potable Water Filling and
Drainage)
- 52-04 (Refer to 52-04 Access Door
to Opening Control of Landing Gear
Doors on Ground 195 BB - 196 BB)
- 52-05 (Refer to 52-05 Access Door
to Air Conditioning Ground Supply
191 CB)
- 52-06 (Refer to 52-06 Forward
Jacking Point Access Door)
- 52-20 (Refer to 52-20 Access Door
to HP Air Ground Connector 191
DB).
Performance:
The following performance penalties are applicable:
- Takeoff and approach performance limiting weightsare reduced by 63 kg
- En-route performance limiting weight is reduced by 72kg.
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.03
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-02 ACCESS DOOR TO
HYDRAULIC
GROUND
CONNECTORS 197
CB - 197 EB - 198 CB
(Cont’d)
02.52.04DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-3 ACCESS DOOR TO
POTABLE WATER
FILLING AND
DRAINAGE 133 AL -
171 AL - 192 NB
3 2 One may be missing.
Note:
May be combined with MCDL items:
- 52-01 (Refer to 52-01 Toilet
Servicing and Drainage Door )
- 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197
CB - 197 EB - 198 CB)
- 52-04 (Refer to 52-04 Access Door
to Opening Control of Landing Gear
Doors on Ground 195 BB - 196 BB)
- 52-05 (Refer to 52-05 Access Door
to Air Conditioning Ground Supply
191 CB)
- 52-06 (Refer to 52-06 Forward
Jacking Point Access Door)
- 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191
DB).
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.05
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-03 ACCESS DOOR TO
POTABLE WATER
FILLING AND
DRAINAGE 133 AL -
171 AL - 192 NB
(Cont’d)
02.52.06DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-04 ACCESS DOOR TO
OPENING CONTROL
OF LANDING GEAR
DOORS ON
GROUND 195 BB -
196 BB
2 1 One may be missing for five flight cycles.
Note:
May be combined with MCDL items:
- 52-01 (Refer to 52-01 Toilet
Servicing and Drainage Door )
- 52-02 (Refer to 52-02 Access Door
to Hydraulic Ground Connectors 197
CB - 197 EB - 198 CB)
- 52-03 (Refer to 52-03 Access Door
to Potable Water Filling and
Drainage)
- 52-05 (Refer to 52-05 Access Door
to Air Conditioning Ground Supply
191 CB)
- 52-06 (Refer to 52-06 Forward
Jacking Point Access Door)
- 52-20 (Refer to 52-20 Access Door
to HP Air Ground Connector 191
DB).
Limitations:
Flight in forecasted thunderstorm condition is not allowed.
Performance:
The following performance penalties are applicable:
- Takeoff and approach performance limiting weightsare reduced by 63 kg
- En-route performance limiting weight is reduced by 72
kg .
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.07
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-04 ACCESS DOOR TO
OPENING CONTROL
OF LANDING GEAR
DOORS ON
GROUND 195 BB -
196 BB
(Cont’d)
02.52.08DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-05 ACCESS DOOR TO
AIR CONDITIONING
GROUND SUPPLY
191 CB
1 0 May be missing.
Note:
May be combined with MCDL items:
- 52-01 (Refer to 52-01 Toilet
Servicing and Drainage Door )
- 52-02 (Refer to 52-02 Access Door
to Hydraulic Ground Connectors 197
CB - 197 EB - 198 CB)- 52-03 (Refer to 52-03 Access Door
to Potable Water Filling and
Drainage)
- 52-04 (Refer to 52-04 Access Door
to Opening Control of Landing Gear
Doors on Ground 195 BB - 196 BB)
- 52-06 (Refer to 52-06 Forward
Jacking Point Access Door)
- 52-20 (Refer to 52-20 Access Door
to HP Air Ground Connector 191
DB).
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.09
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-05 ACCESS DOOR TO
AIR CONDITIONING
GROUND SUPPLY
191 CB
(Cont’d)
02.52.10DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-06 FORWARD JACKING
POINT ACCESS
DOOR
1 0 May be missing.
Note:
May be combined with MCDL items:
- 52-01 (Refer to 52-01 Toilet
Servicing and Drainage Door )
- 52-02 (Refer to 52-02 Access Door
to Hydraulic Ground Connectors 197
CB - 197 EB - 198 CB)
- 52-03 (Refer to 52-03 Access Door
to Potable Water Filling and
Drainage)
- 52-04 (Refer to 52-04 Access Door
to Opening Control of Landing Gear
Doors on Ground 195 BB - 196 BB)
- 52-05 (Refer to 52-05 Access Door
to Air Conditioning Ground Supply
191 CB)
- 52-20 (Refer to 52-20 Access Door
to HP Air Ground Connector 191DB).
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.11
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-06 FORWARD JACKING
POINT ACCESS
DOOR
(Cont’d)
02.52.12DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-07 EXTERNAL POWER
GROUND
CONNECTION
ACCESS DOOR
ASSY 121 AL
1 0 (M) May be missing for five fl ight cycles provided the hole is
covered with high speed tape and that a visual inspection
is performed before each flight.
Limitations:
Flight in forecasted thunderstorm condition is not allowed.
MAINTENANCE PROCEDURES
Refer to AMM 52-42-00-040-003
12 FEB 12CDL
A320/321MEL/CDL 02.52.13
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-08 ACCESS DOOR OF
CARGO OPENING
SYSTEM 134 AR -
154 AR
2 0 All may be missing.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 95 kg per missing access door
- En-route performance limiting weight is reduced by105 kg (232 lb) per missing access door
- Fuel consumption is increased by 0.21 % per missingaccess door.
02.52.14DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-09 NOSE LANDING
GEAR MAIN DOOR
(713, 714)
2 0 (M) May be missing provided both main doors (713, 714) are
removed and both aft doors (715, 716) (Refer to 52-10
Nose Landing Gear Aft Door (715, 716)) are removed.
Note:
May be combined with MCDL item 52-
11 (Refer to 52-11 Nose Landing Gear
Leg Door (712))
Limitations:
Passengers transportation is not allowed.
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
Maximum speed: 220 kt IAS/ M 0.5
Performance:
Note:
Reference performance for penaltiescomputations are performance with
landing gear down.
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 1 109 kg
- En-route performance limiting weight is reduced by 1000 kg
- Fuel consumption is increased by 2 %.
MAINTENANCE PROCEDURES
Refer to AMM 32-22-00-040-001
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.15
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-09 NOSE LANDING
GEAR MAIN DOOR
(713, 714)
(Cont’d)
02.52.16DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-10 NOSE LANDING
GEAR AFT DOOR
(715, 716)
2 0 (M) All may be missing.
Note:
May be combined with MCDL item 52-
11 (Refer to 52-11 Nose Landing Gear
Leg Door (712))
Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
Performance:
Note:
Reference performance for penalties
computations are performance with
landing gear down.
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 79 kg
- En-route performance limiting weight is reduced by100 kg
- Fuel consumption is increased by 0.25 %.
When combined with MCDL item 52-09 (Refer to 52-09
Nose Landing Gear Main Door (713, 714)), the
performance penalties published in 52-09 are applicable.
MAINTENANCE PROCEDURES
Refer to AMM 32-22-00-040-002
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.17
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-10 NOSE LANDING
GEAR AFT DOOR
(715, 716)
(Cont’d)
02.52.18DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-11 NOSE LANDING
GEAR LEG DOOR
(712)
1 0 (M) May be missing.
Note:
May be combined with MCDL items 52-
09 (Refer to 52-09 Nose Landing Gear
Main Door (713, 714)) and 52-10 (Refer
to 52-10 Nose Landing Gear Aft Door
(715, 716)).
Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
MAINTENANCE PROCEDURES
Refer to AMM 32-22-00-040-003
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.19
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-11 NOSE LANDING
GEAR LEG DOOR
(712)
02.52.20DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-12 MAIN LANDING
GEAR DOOR (732,
742) (FLIGHT WITH
GEAR UP)
2 1 (M) One may be missing.
Limitations:
Passengers transportation is not allowed.
Flight in forecasted icing conditions is not allowed.
Performance:
The following performance penalties are applicable:
- ] Takeoff and approach climb performance limitingweights are reduced by 475 kg
- ] En-route performance limiting weight is reduced by525 kg (1 158 lb)
- ] Fuel consumption is increased by 0.96 %.
MAINTENANCE PROCEDURES
Refer to AMM 32-12-00-040-005
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.21
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-12 MAIN LANDING
GEAR DOOR (732,
742) (FLIGHT WITH
GEAR UP)
(Cont’d)
02.52.22DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-13 MAIN LANDING
GEAR DOOR (733,
743) (FLIGHT WITH
GEAR UP)
2 1 (M) One may be missing.
Limitations:
Passengers transportation is not allowed.
Flight in forecasted icing conditions is not allowed.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 111 kg
- En-route performance limiting weight is reduced by126 kg
- Fuel consumption is increased by 0.28 %.
MAINTENANCE PROCEDURES
Refer to AMM 32-12-00-040-005
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.23
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-13 MAIN LANDING
GEAR DOOR (733,
743) (FLIGHT WITH
GEAR UP)
(Cont’d)
02.52.24DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-14 MAIN LANDING
GEAR DOOR (732,
742) (FLIGHT WITH
GEAR DOWN)
2 1 (M) One may be missing.
Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
Performance:
Note:
Reference performance for penalties
computations are performance with
landing gear down.
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 475 kg
- En-route performance limiting weight is reduced by450 kg
- Fuel consumption is increased by 1.00 %.
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.25
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-14 MAIN LANDING
GEAR DOOR (732,
742) (FLIGHT WITH
GEAR DOWN)
(Cont’d)
02.52.26DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-15 MAIN LANDING
GEAR DOOR (733,
743) (FLIGHT WITH
GEAR DOWN)
2 1 (M) One may be missing.
Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
Performance:
Note:
Reference performance for penalties
computations are performance with
landing gear down.
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 111 kg
- En-route performance limiting weight is reduced by200 kg
- Fuel consumption is increased by 0.30 %.
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.27
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-15 MAIN LANDING
GEAR DOOR (733,
743) (FLIGHT WITH
GEAR DOWN)
(Cont’d)
02.52.28DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-16 MAIN LANDING
GEAR DOOR (734,
744) (FLIGHT WITH
GEAR DOWN)
2 1 (M) One may be missing.
Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
Performance:
Note:
Reference performance for penalties
computations are performance with
landing gear down.
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 752 kg
- En-route performance limiting weight is reduced by700 kg
- Fuel consumption is increased by 1.50 %.
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.29
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-16 MAIN LANDING
GEAR DOOR (734,
744) (FLIGHT WITH
GEAR DOWN)
(Cont’d)
02.52.30DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-18 MAIN LANDING
GEAR DOOR : SEAL
ON SECONDARY
HINGED FAIRING
6 0 All may be missing.
Performance:
If three or more seals are missing, the following
performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 24 kg per missing seal
- En-route performance limiting weight is reduced by 27
kg per missing seal
- Fuel consumption is increased by 0.07 % per missingseal.
12 FEB 12CDL
A320/321MEL/CDL 02.52.31
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-19 PAX DOOR UPPER
COVER PLATE
8 0 All may be missing.
Note:
The affected door must be considered
as inoperative (Refer to MEL/MI-52-10
Cabin Passenger Door).
Performance:
The following performance penalties are applicable:- Takeoff and approach climb performance limiting
weights are reduced by 79 kg per missing plate
- En-route performance limiting weight is reduced by 88kg (195 lb) per missing plate
- If 2 or more plates are missing, fuel consumption isincreased by 0.18 % per missing plate.
02.52.32DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-20 ACCESS DOOR TO
HP AIR GROUND
CONNECTOR 191
DB
1 0 (M) May be missing for ten flight cycles.
Note:
May be combined with MCDL items:
- 52-01 (Refer to 52-01 Toilet
Servicing and Drainage Door )
- 52-02 (Refer to 52-02 Access Door
to Hydraulic Ground Connectors 197
CB - 197 EB - 198 CB)
- 52-03 (Refer to 52-03 Access Door
to Potable Water Filling and
Drainage)
- 52-04 (Refer to 52-04 Access Door
to Opening Control of Landing Gear
Doors on Ground 195 BB - 196 BB)
- 52-05 (Refer to 52-05 Access Door
to Air Conditioning Ground Supply
191 CB)
- 52-06 (Refer to 52-06 Forward
Jacking Point Access Door).
MAINTENANCE PROCEDURES
Refer to AMM 47-20-00-040-002
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.52.33
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-20 ACCESS DOOR TO
HP AIR GROUND
CONNECTOR 191
DB
(Cont’d)
02.52.34DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-21 BLUE HYDRAULIC
ACCESS DOOR 197
FB
1 0 (M) May be missing.
MAINTENANCE PROCEDURES
Refer to AMM 52-41-00-040-001
12 FEB 12CDL
A320/321MEL/CDL 02.52.35
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-22 FORWARD CARGO
DOOR ACCESS
COVER PANEL 825
AR
1 0 (M) May be missing provided all latching hooks are checked
latched and locked before each flight.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 234 kg
- En-route performance limiting weight is reduced by
266 kg
- Fuel consumption is increased by 0.64 %.
02.52.36DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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52 DOORS
52-23 AFT CARGO DOOR
ACCESS COVER
PANEL 826 AR
1 0 (M) May be missing provided all latching hooks are checked
latched and locked before each flight.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 190 kg
- En-route performance limiting weight is reduced by
216 kg
- Fuel consumption is increased by 0.53 %.
* * *
12 FEB 12CDL
A320/321MEL/CDL 02.52.37
DOORS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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02.52.38DOORS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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53 FUSELAGE
53-01 BELLY FAIRING
VENT LOUVER
VANE
24 18 (M) Three may be missing per vent louver.
Note:
Vane with a crack length higher than
50% must be removed before next flight.
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.53.01
FUSELAGE
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53 FUSELAGE
53-03 ROOT FILLET
FAIRING
2 0 (M) All may be missing.
Note:
Must not be combined with MCDL item
54-01 (Refer to 54-01 Nacelle Strake) or
MCDL item 54-03 (Refer to 54-03 Pylon
Pressure Relief Door 413(423) BL -
414(424) BR).
Performance:
The following performance penalty is applicable:
- Takeoff performance limiting weight is reduced by 900kg.
Note:
The above performance penalty is not
applicable if the flight crew can check
V2 greater than 1.15 VS1G.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
02.53.02FUSELAGE
A320/321MEL/CDL 12 FEB 12
CDL
ITEM
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53 FUSELAGE
53-03 ROOT FILLET
FAIRING
(Cont’d)
* * *
12 FEB 12MEL
A320/321MEL/CDL 02.53.03
FUSELAGE
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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02.53.04FUSELAGE
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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54 NACELLES / PYLON
54-01 NACELLE STRAKE 4 0 All may be missing.
Note:
Must not be combined with MCDL item
53-03 (Refer to 53-03 Root Fillet
Fairing).
Procedures:
Approach speed: VLS + 4 kt.
Landing distance: multiply by 1.09.
Performance:
The following performance penalties are applicable:
- If no internal strakes and one or both external strakesare missing, takeoff performance limiting weight isreduced by 2 380 kg
- If one or both internal strakes are missing (with or without external strakes missing), takeoff performancelimiting weight is reduced by 3 270 kg
- Increase V2 and VR by 1 kt.
Note:
The performance penalties are not
applicable if the flight crew can check
V2 greater than 1.17 VS1G.
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.54.01
NACELLES / PYLON
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54 NACELLE / PYLON
54-01 NACELLE STRAKE
(Cont’d)
02.54.02NACELLES / PYLON
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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54 NACELLES / PYLON
54-03 PYLON
PRESSURE
RELIEF DOOR
413(423) BL -
414(424) BR
4 0 (M) All may be missing for 5 fl ight cycles only.
Note:
i. If one door is missing on a pylon, the
other door on the same pylon must
be removed.
ii. Must not be combined with MCDL
item 53-03 (Refer to 53-03 Root
Fillet Fairing).
Limitations:
Maximum cruise speed: M 0.78.
Procedures:
Approach speed: VLS + 4 kt.
Landing distance: multiply by 1.09.
Performance:
The following performance penalties are applicable:
- Takeoff performance limiting weight is reduced by 2380 kg
- Increase V2 and VR by 1 kt
Note:
The above performance penalties are
not applicable if the flight crew can
check V2 greater than 1.16 VS1G.
- If two or more doors are missing, en routeperformance limiting weight is reduced by 40 kg per missing door
- If three or more doors are missing, fuel consumption isincreased by 0.09 % per missing door.
MAINTENANCE PROCEDURES
Refer to AMM 54-52-00-040-001
(Cont’d on next page)
12 FEB 12CDL
A320/321MEL/CDL 02.54.03
NACELLES / PYLON
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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54 NACELLES / PYLON
54-03 PYLON PRESSURE
RELIEF DOOR
413(423) BL -
414(424) BR
(Cont’d)
02.54.04NACELLES / PYLON
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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54 NACELLES / PYLON
54-04 PYLON ACCESS
DOOR 415(425) AL
- 415(425) AR
4 0 All may be missing for 5 flight cycles provided the hole is
covered with high speed tape.
Limitations:
Flight in forecasted thunderstorm conditions is not
allowed.
12 FEB 12CDL
A320/321MEL/CDL 02.54.05
NACELLES / PYLON
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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54 NACELLES / PYLON
54-05 PYLON FAIRING
SEAL
4 3 One may be missing per pylon.
02.54.06NACELLES / PYLON
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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54 NACELLE/PYLON
54-06 AERODYNAMIC
SEAL
2 0 (M) All may be missing.
MAINTENANCE PROCEDURES
Refer to AMM 54-53-00-040-001
12 FEB 12MEL
A320/321MEL/CDL 02.54.07
NACELLES / PYLON
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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02.54.08NACELLES / PYLON
A320/321MEL/CDL 12 FEB 12
MEL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
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57 WINGS
57-01 Wing Tip Fence
57-01a Lower Part Of A
Wing Tip Fence
2 1 (M) One lower part of a wing tip fence may be missing
provided the broken part is removed and holes are
covered.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 3 960 kg
- En-route performance limiting weight is reduced by378 kg
- Fuel consumption is increased by 0.88 %.
MAINTENANCE PROCEDURES
Refer to AMM 57-31-00-040-001
57-01b Complete Wing Tip
Fence
2 1 (M) One complete wing tip fence may be missing provided
exposed interior structure is covered, protective material
is inspected before each flight and replaced if necessary.
Performance:
The following performance penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 8 910 kg
- En-route performance limiting weight is reduced by735 kg
- Fuel consumption is increased by 1.34 %.
MAINTENANCE PROCEDURES
Refer to AMM 57-31-00-040-001
(Cont’d on next page)
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.57.01
WINGS
7/23/2019 A 320321 Mel Cdl
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57 WINGS
57-01 Wing Tip Fence
(Cont’d)
02.57.02WINGS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
7/23/2019 A 320321 Mel Cdl
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57 WINGS
57-02 BELLY FAIRING
SLIDING PANEL
2 0 All may be missing.
Performance:
If two panels are missing, the following performance
penalties are applicable:
- Takeoff and approach climb performance limitingweights are reduced by 96 kg
- En route performance limiting weight is reduced by
108 kg- Fuel consumption is increased by 0.28 %.
12 FEB 12CDL
A320/321MEL/CDL 02.57.03
WINGS
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
7/23/2019 A 320321 Mel Cdl
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57 WINGS
57-03 OUTBOARD FLAP
RUBBING STRIP
ITEMS 40, 70, 80, 85,
100, 120
12 0 All may be missing.
* * *
02.57.04WINGS
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
7/23/2019 A 320321 Mel Cdl
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71 POWER PLANT
71-01 FRANGIBLE
DRAIN MAST
2 0 ((M) All may be missing.
MAINTENANCE PROCEDURES
Refer to AMM 71-71-42-040-044
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
12 FEB 12CDL
A320/321MEL/CDL 02.71.01
POWER PLANT
7/23/2019 A 320321 Mel Cdl
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71 POWER PLANT
71-09 FAN COWL HOLD
OPEN ROD
8 0 (M) All may be missing.
MAINTENANCE PROCEDURES
Refer to AMM 71-13-12-000-040
02.71.02POWER PLANT
A320/321MEL/CDL 12 FEB 12
CDL
1. 2. NUMBER INSTALLED
SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH
SEQUENCE
OF ITEMS 4. REMARKS OR EXCEPTIONS
ITEM
Recommended