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ISSUE DATE : 11-Jun-2010

A320 FCOM Vol 1 ISS Rev 43D

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GENERAL INFORMATION

CONTENTS JUN 10 ISS - 00

00.00 CONTENTS 00.10 ORGANIZATION OF THE MANUAL

- FOREWORD ........................................................... 1

- COMMENTS − QUESTIONS − SUGGESTIONS........................ 1 - CONTENT.............................................................. 1 - USE .................................................................... 2 - PAGINATION........................................................... 3 - REVISIONS ............................................................ 4 - HOW TO INSERT A REVISION......................................... 5

00.20 LIST OF CODES 00.30 LIST OF NORMAL REVISIONS 00.35 RECORD OF TEMPORARY REVISIONS 00.36 LIST OF EFFECTIVE TEMPORARY REVISIONS 00.40 ABBREVIATIONS 00.50 UNITS CONVERSION TABLE 00.60 SYMBOLS 00.70 CROSS REFERENCE TABLE

00.75 HIGHLIGHTS

00.80 LIST OF EFFECTIVE PAGES 00.85 LIST OF MODIFICATIONS

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GENERAL INFORMATION

FOREWORD JUN 10 ISS - 00

Activities transfer from Meridiana S.p.A. to Meridiana fly S.p.A.

Starting from the issue of Meridiana fly COA, with reference to the activities transfer in subject, we inform you that all documents containing the logo of Meridiana S.p.A., compliant to EU-OPS and ENAC certification requirements, will be effective for Meridiana fly activities until the full replacement of the Meridiana logo has been completed.

Document Code

As per ENAC requirement the FCOMs are coded as follows:

� A319 FCOM I � ISS_DFO_A319FCOM I;

� A319 FCOM II � ISS_DFO_A319FCOM II;

� A319 FCOM III � ISS_DFO_A319FCOM III;

� A319 FCOM IV � ISS_DFO_A319FCOM IV;

� A319 QRH � ISS_DFO_A319QRH;

� A319 MEL � ISS_DFO_A319MEL.

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GENERAL INFORMATION

ORGANIZATION OF THE MANUAL JUN 10 ISS - 00

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GENERAL INFORMATION

EU-OPS 1/OM/B CROSS REFERENCE SEP 10 ISS - 00

B. AEROPLANE OPERATING MATTERS-TYPE RELATED Taking account of the differences between types, and variants of types, under the following headings:

0. GENERAL INFORMATION AND UNITS OF MEASUREMENT 0.1. General Information (e.g. aeroplane dimensions), including a description of FCOM 1.00.50 the units of measurement used for the operation of the aeroplane type concerned and conversion tables.

FCOM 1.20.00

1. LIMITATIONS 1.1. A description of the certified limitations and the applicable operational limitations including: (a) Certification status (e.g. CS.23, CS.25, ICAO Annex 16 (CS.36 and CS.34), etc.); (b) Passenger seating configuration for each aeroplane type including a pictorial presentation; (c) Types of operation that are approved (e.g. VFR/IFR, CAT II/III, RNP Type, flight in known icing conditions etc); (d) Crew composition; (e) Mass and centre of gravity; (f) Speed limitations; (g) Flight envelope(s); (h) Wind limits including operations on contaminated runways; (i) Performance limitations for applicable configurations; (j) Runway slope; (k) Limitations on wet or contaminated runways; (l) Airframe contamination; and (m) System limitations.

FCOM II 2.01.00 FCOM II 2.04.00 FCOM III 3.01.00 FCOM III 3.05.00 W & B MANUAL

2. NORMAL PROCEDURES 2.1. The normal procedures and duties assigned to the crew, the appropriate check-lists, the system for use of the checklists and a statement covering the necessary coordination procedures between flight and cabin crew. The following normal procedures and duties must be included: (a) Pre-flight; (b) Pre-departure; (c) Altimeter setting and checking; (d) Taxi, Take-Off and Climb; (e) Noise abatement; (f) Cruise and descent; (g) Approach, Landing preparation and briefing; (h) VFR Approach; (i) Instrument approach; (j) Visual Approach and circling; (k) Missed Approach; (l) Normal Landing;

FCOM II 2.04.00 FCOM III 3.03.00

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(m) Post Landing; and (n) Operation on wet and contaminated runways

3. ABNORMAL AN EMERGENCY PROCE URES 3.1. The abnormal and emergency procedures and duties assigned to the crew, the appropriate check-lists, the system for use of the check-lists and a statement covering the necessary coordination procedures between flight and cabin crew. The following abnormal and emergency procedures and duties must be included: (a) Crew Incapacitation; (b) Fire and Smoke Drills; (c) Unpressurised and partially pressurised flight; (d) Exceeding structural limits such as overweight landing; (e) Exceeding cosmic radiation limits; (f) Lightning Strikes; (g) Distress Communications and alerting ATC to Emergencies; (h) Engine failure; (i) System failures; (j) Guidance for Diversion in case of Serious Technical Failure; (k) Ground Proximity Warning; (l) TCAS Warning; (m) Wind shear; and (n) Emergency Landing/Ditching; and (o) Departure contingency procedures.

FCOM III 3.02.00

4. PERFORMANCE

4.0. Performance data must be provided in a form in which it can be used without difficulty.

4.1. Performance data. Performance material which provides the necessary data for compliance with the performance requirements prescribed in OPS 1 Subparts F, G, H and I must be included to allow the determination of: (a) Take-off climb limits . Mass, Altitude, Temperature; (b) Take-off field length (dry, wet, contaminated); (c) Net flight path data for obstacle clearance calculation or, where applicable, take- off flight path; (d) The gradient losses for banked climb outs; (e) En-route climb limits; (f) Approach climb limits; (g) Landing climb limits; (h) Landing field length (dry, wet, contaminated) including the effects of an inflight failure of a system or device, if it affects the landing distance; (i) Brake energy limits; and (j) Speeds applicable for the various flight stages (also considering wet or contaminated runways).

FCOM II 2.04.00 FCOM III 3.02.00 FCOM III 3.05.00

4.1.1. Supplementary data covering flights in icing conditions. Any certificated performance related to an allowable configuration, or configuration deviation, such as anti-skid inoperative, must be included.

FCOM III 3.04.30 MEL FM

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4.1.2.If performance Data, as required for the appropriate performance class, is not available in the approved AFM, then other data acceptance to the contain cross reference to the approved Data contained in the AFM where such Data is not likely to be used often or in an emergency

FM

4.2. Additional Performance Data. Additional performance data where applicable including:

(a) All engine climb gradients; FCOM III 3.05.00

(b) Drift-down data; FCOM III 3.06.00

(c) Effect of de-icing/anti-icing fluids; FCOM III 3.04. 1

(d) Flight with landing gear down; FCOM II 2.04.00

(e) For aeroplanes with 3 or more engines, one engine inoperative ferry flights; and N.A.

(f) Flights conducted under the provisions of the CDL. AFM

5. FLIGHT PLANNING

5.1. Data and instructions necessary for pre-flight and in-flight planning including factors such as speed schedules and power settings. Where applicable, procedures for engine(s)-out operations, ETOPS (particularly the one-engineinoperative cruise speed and maximum distance to an adequate aerodrome determined in accordance with OPS 1.245) and flights to isolated aerodromes must be included

OM/A 8.1 OM/A 8.5 FCOM II 2.05.00 FCOM III 3.06.00

5.2. The method for calculating fuel needed for the various stages of flight, in accordance with OPS 1.255. FCOM III 3.05.00

5.3 Performance Data for ETOPS Critical Fuel Reserve and Area of Operation including sufficient data to support the critical fuel reserve and area of operation calculation based on Approved Aeroplane Performance Data. The following data is required:

(a) Detailed engine(s) inoperative performance data including fuel flow for standard and non-standard atmospheric conditions and as a function of airspeed and power setting, where appropriate, covering:

(i) Drift down (includes net performance) see OPS 1.505 where applicable; (ii) Cruise altitude coverage including 10 000 feet; (iii) Holding; (iv) Altitude capability (includes net performance); and (v) Missed approach.

FCOM II 2.04.40 FCOM III 3.06.00

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(b) Detailed all-engine-operating performance data, including nominal fuel flow data, for standard and non-standard atmospheric conditions and as a function of airspeed and power setting, where appropriate, covering: (i) Cruise (altitude coverage including 10 000 feet); and (ii) Holding.

FCOM III 3.05.00

(c) Details of any other conditions relevant to ETOPS operations which can cause significant deterioration of performance, such as ice accumulation on the unprotected surfaces of the aeroplane, Ram Air Turbine (RAT) deployment, thrust-reverser deployment, etc.

MEL MANUAL FCOM III 3.04.30

The altitudes, airspeeds, thrust settings, and fuel flow used in establishing the ETOPS area of operations for each airframe-engine combination must be used in showing the corresponding terrain and obstruction clearances in accordance with this regulation.

FCOM II 2.04.00

6. MASS AN BALANCE Instructions and data for the calculation of the mass and balance including: (a) Calculation system (e.g. Index system); (b) Information and instructions for completion of mass and balance documentation, including manual and computer generated types; (c) Limiting masses and centre of gravity for the types, variants or individual aeroplanes used by the operator; and (d) Dry Operating mass and corresponding centre of gravity or index.

FCOM II 2.01.00

7. LOADING Procedures and provisions for loading and securing the load in the aeroplane. FCOM II 2.01.00

8. CONFIGURATION DEVIATION LIST

The Configuration Deviation List(s) (CDL), if provided by the manufacturer, taking account of the aeroplane types and variants operated including procedures to be followed when an aeroplane is being despatched under the terms of its CDL

AFM

MINIMUM EQUIPMENT LIST

The Minimum Equipment List (MEL) taking account of the aeroplane types and variants operated and the type(s)/area(s) of operation. The MEL must include the navigational equipment and take into account the required performance for the route and area of operation.

MEL MANUAL

10. SURVIVAL AN EMERGENCY EQUIPMENT INCLUDING OXYGEN

10.1. A list of the survival equipment to be carried for the routes to be flown and the procedures for checking the serviceability of this equipment prior to take-off. Instructions regarding the location, accessibility and use of survival and emergency equipment and its associated check list(s) must also be included.

FCOM I 1.25.30

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10.2. The procedure for determining the amount of oxygen required and the quantity that is available. The flight profile, number of occupants and possible cabin decompression must be considered. The information provided must be in a form in which it can be used without difficulty.

FCOM I 1.25.30 FCOM III 3.01.00

11. EMERGENCY EVACUATION PROCEDURES

11.1. Instructions for preparation for emergency evacuation including crew co-ordination and emergency station assignment. FCOM III 3.02.00

11.2. Emergency evacuation procedures. A description of the duties of all members of the crew for the rapid evacuation of an aeroplane and the handling of the passengers in the event of a forced landing, ditching or other emergency

FCOM III 3.02.0

12. AEROPLANE SYSTEMS A description of the aeroplane systems, related controls and indications and operating instructions.

FCOM I SYSTEM DESCRIPTION

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GENERAL INFORMATION

LIST OF NORMAL REVISION SEP 10 ISS - 01

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AIRBUS REVISION ISS REVISION

N° ISSUE DATE INSERTED

BY N° ISSUE DATE INSERTED

BY 00 JUL 86 ISS-00 JUN 10 01 NOV 86 ISS-01 SEP 10 02 FEB 87 03 OCT 87 04 JAN 88 05 MAR 88 06 MAY 88 07 JUL 88 08 OCT 88 09 JAN 89 10 APR 89 11 SEP 89 12 MAR 90 13 SEP 90

14 NOT DISPATCHED

15 AUG 91 16 MAR 92 17 DEC 92 18 MAR 93 19 SEP 93 20 DEC 93 21 JUL 94 22 OCT 95 23 JAN 97 24 NOV 97 25 APR 98 26 SEP 98 27 FEB 99 28 JUL 99 29 FEB 00 30 JUN 00

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BY 31 NOV 00 32 MAY 01 33 NOV 01 34 JUL 02 35 DEC 02 36 OCT 03 37 MAR 04 38 DEC 04 39 FEB 06 40 DEC 06 41 SEP 07 42 DEC 08 43 DEC 09

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32 MAY 01

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318/319/320/321 FCOM VOL.1 REV043D CROSS REFERENCE TABLE

THIS TABLE GIVES, FOR EACH AIRCRAFT INCLUDED IN THE MANUAL, THE CROSS REFERENCE BETWEEN :

- THE MANUFACTURING SERIAL NUMBER (MSN) WHICH APPEARS IN THE LIST OF EFFECTIVE PAGES

- THE REGISTRATION NUMBER OF THE AIRCRAFT AS KNOWN BY AIRBUS INDUSTRIE.

---------------------------------------------------------------------------- MSN REGISTRATION ----------------------------------------------------------------------------

0588 F-OOUA 1048 EI-DFP 1102 EI-DEY 1283 EI-DEZ 1305 EI-DFA

ISS 1.00.70 11 JUN 2010 PAGE : CRT001

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318/319/320/321 FCOM VOL. 1 SYSTEMS DESCRIPTION HIGHLIGHTS REV043D

V CH SEC ---PAGE-- SEQ- --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE---------------------------------------------------------------------------------------------------------

1 22 20 002 110 REV032 CODE 1791

- INCORPORATION OF MOD 25205

1 22 20 003 110 REV042 CODE:1636

- INCORPORATION OF MOD 24075 - INCORPORATION OF MOD 25205

1 22 20 004 105 REV038 CODE 1437

- INCORPORATION OF MOD 25205

1 22 20 005 110 REV026 CODE 1794

- INCORPORATION OF MOD 25205

1 22 20 006 110 REV026 CODE 0477

- INCORPORATION OF MOD 25205

1 22 20 007 110 REV042 CODE 1640

- INCORPORATION OF MOD 25205

1 22 20 008 100 REV043 CODE 1637

- INCORPORATION OF MOD 25205

1 22 20 009 106 REV043 CODE 1639

- INCORPORATION OF MOD 25205

1 22 20 010 100 REV042 CODE 0040

- INCORPORATION OF MOD 25205

1 22 20 013 105 REV038 CODE 1904

- INCORPORATION OF MOD 25205

1 22 30 056 115 REV035 CODE 1795

- INCORPORATION OF MOD 25205

1 22 60 002 100 REV038 CODE 0061

- INCORPORATION OF MOD 25205

1 23 10 002 001 REV038 CODE 0598

- INCORPORATION OF MOD 20036 - INCORPORATION OF MOD 20037 - INCORPORATION OF MOD 20170

1 23 30 001 205 REV028 CODE:0698

- INCORPORATION OF MOD 24624

1 23 40 001 100 REV025 CODE 0699

- INCORPORATION OF MOD 23099

11 JUN 2010 ISS 1.00.75 PAGE 1

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V CH SEC ---PAGE-- SEQ- --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE---------------------------------------------------------------------------------------------------------

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N 1 22 20 019 001 REV025 CODE 0358 0588N 1 22 20 020 001 REV041

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N 1 22 30 007 001 REV025 CODE 0264 0588N 1 22 30 008 100 REV042 26497

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1 22 30 007 100 REV041 CODE 0262 1048-1305 1 22 30 008 100 REV042 26497

1 22 30 009 001 REV040 ALL 1 22 30 010 001 REV032

N 1 22 30 011 001 REV039 CODE 0358 0588N 1 22 30 012 001 REV039

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1 22 30 023 001 REV025 ALL 1 22 30 024 001 REV023 EQ 200

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1 22 30 037 300 REV026 CODE:1552 ALL 1 22 30 038 210 REV028 CODE:1554

1 22 30 039 100 REV023 24414=24414+32600 ALL 1 22 30 040 105 REV028 CODE 0408

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N 1 22 30 047 200 REV037 CODE:1595 0588N 1 22 30 048 100 REV025 M:24035=24160=24211

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1 22 30 057 360 REV042 CODE 0175 1048-1305 1 22 30 058 001 REV025

1 22 30 059 001 REV023 ALL 1 22 30 060 001 REV039

N 1 22 30 061 001 REV028 0588N 1 22 30 062 200 REV043 CODE:1651

1 22 30 061 001 REV028 1048-1305 1 22 30 062 203 REV043 CODE 0038

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N 1 22 30 065 100 REV034 24035=24160=24211 0588N 1 22 30 066 001 REV025 CODE 0358

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1 22 45 005 100 REV041 25295 1048-1305 1 22 45 006 100 REV041 25295

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1 22 45 007 100 REV041 25295 1048-1305 1 22 45 008 100 REV041 25295

1 22 46 001 100 REV041 25381=25295+25381 1048-1305 1 22 46 002 202 REV042 25295+25381

N 1 22 60 001 200 REV039 CODE 0054 0588N 1 22 60 002 100 REV038 CODE 0061

1 22 60 001 307 REV041 CODE 1155 1048-1305 1 22 60 002 200 REV038 CODE 1452

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1 23 00 001 100 REV039 CODE 0157 0588-1048 1 23 00 002 001 REV041 STD

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N 1 23 10 005 001 REV023 0588

1 23 10 005 100 REV023 20137 1048-1305

1 23 20 001 001 REV023 ALL 1 23 20 002 001 REV023

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N 1 23 20 015 001 REV039 STD=(K4453+K7741) 0588N 1 23 20 016 100 REV039 22013=24105=K5070

1 23 20 015 100 REV039 CODE 0697 1048-1305 1 23 20 016 100 REV039 22013=24105=K5070

1 23 20 017 001 REV029 ALL 1 23 20 018 001 REV024

1 23 20 019 001 REV032 CODE 1031 ALL 1 23 20 020 002 REV024

1 23 30 001 205 REV028 CODE:0698 ALL 1 23 30 002 001 REV034 STD

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N 1 23 40 009 100 REV037 CODE 0699 0588

1 23 46 001 100 REV030 28138=36224 1283-1305 1 23 46 002 200 REV032 30162+28138=36224+36480

1 23 46 003 100 REV032 30162=36480 1283-1305 1 23 46 004 100 REV032 30162=36480

1 23 46 005 100 REV032 30162=36480 1283-1305

N 1 23 50 001 001 REV023 STD 0588

1 23 50 001 120 REV036 CODE 0206 1048-1305

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N 1 23 60 001 100 REV023 M:21858 0588

1 24 00 001 001 REV023 ALL

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1 24 10 003 001 REV023 STD=(27140+34895) ALL 1 24 10 004 001 REV040 STD

1 24 10 004A 100 REV040 22013=24105=28160 ALL

1 24 10 005 001 REV023 ALL 1 24 10 006 001 REV023 STD=(30368+35270)

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1 24 10 007 001 REV023 STD=(30368+35270) ALL 1 24 10 008 001 REV023

N 1 24 10 009 001 REV023 STD=(30368+35270) 0588N 1 24 10 010 001 REV023 STD=(30368+35270)

1 24 10 009 001 REV023 STD=(30368+35270) 1048-1305 1 24 10 010 105 REV041 37317=30368+35270+37317

1 24 10 011 001 REV023 STD=(30368+35270) ALL 1 24 10 012 001 REV023 STD=(30368+35270)

1 24 10 013 100 REV025 CODE 0976 ALL 1 24 10 014 100 REV023 M:22013=24105=28160

1 24 10 015 001 REV023 ALL 1 24 10 016 001 REV023

1 24 10 017 001 REV042 STD=(30368+35270) ALL 1 24 10 018 001 REV023

1 24 10 019 100 REV025 M:22013=24105=28160 ALL

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1 24 20 001 200 REV028 M:21230+27498 1048-1305 1 24 20 002 200 REV023 M:21230+21213

N 1 24 20 003 001 REV023 0588N 1 24 20 004 001 REV023

1 24 20 003 001 REV023 1048-1305 1 24 20 004 210 REV042 M:27498+37317

1 24 20 005 001 REV023 ALL 1 24 20 006 100 REV025 M:22013=24105=28160

1 24 20 007 001 REV023 ALL 1 24 20 008 001 REV023

1 24 20 009 001 REV023 STD=(30368+35270) ALL 1 24 20 010 001 REV023

1 24 20 011 001 REV023 STD=(30368+35270) ALL 1 24 20 012 001 REV023 STD=(30368+35270)

1 24 20 013 001 REV023 ALL 1 24 20 014 001 REV023

1 24 20 015 001 REV032 ALL 1 24 20 016 001 REV023 STD=(IAE ALL+25409)=25409

N 1 24 20 017 001 REV041 0588N 1 24 20 018 001 REV036

1 24 20 017 001 REV041 1048-1305 1 24 20 018 100 REV043 25999

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N 1 25 00 001 105 REV036 M:32088=32090 0588

1 25 00 001 200 REV036 CODE 0136 1048-1305

1 25 10 001 001 REV039 ALL 1 25 10 002 001 REV034

1 25 10 003 100 REV034 20047=20255=23577 ALL 1 25 10 004 001 REV039

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1 25 11 009 105 REV040 32087 1048-1305

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N 1 27 10 012A 001 REV039 STD 0588

1 27 10 012A 110 REV037 MOD:34097=37858 1048-1305

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N 1 27 10 013 001 REV042 0588N 1 27 10 014 100 REV024 M:22013=24105=26334=26335

1 27 10 013 110 REV042 MOD:34097=37858 1048-1305 1 27 10 014 100 REV024 M:22013=24105=26334=26335

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1 27 30 003 001 REV041 STD ALL 1 27 30 004 001 REV023 STD

1 27 30 005 001 REV032 STD ALL 1 27 30 006 001 REV023 STD

N 1 27 30 007 001 REV023 STD 0588

1 27 30 007 100 REV036 30977=33879 1048-1305

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N 1 27 40 013 103 REV041 22013=24105=26334=26335 0588N 1 27 40 014 001 REV036

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1 27 50 001 001 REV023 STD=M:24105 ALL 1 27 50 002 001 REV023 STD=M:24105

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1 27 50 007 001 REV023 STD=(30368+35270) 0588-1102 1 27 50 008 001 REV041 STD

1 27 50 007 001 REV023 STD=(30368+35270) 1283-1305 1 27 50 008 100 REV040 P6146

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1 28 20 003 100 REV023 CODE 0163 ALL 1 28 20 004 100 REV023 M:20164=32255

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1 29 10 001 001 REV023 ALL 1 29 10 002 100 REV023 M:22013=24105=26334=26335

1 29 10 003 001 REV023 ALL 1 29 10 004 001 REV023

1 29 10 005 100 REV033 CODE 0306 ALL 1 29 10 006 100 REV023 M:22013=24105=26334=26335

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1 29 20 003 001 REV027 STD=M:21679=(21591+21679) ALL 1 29 20 004 001 REV030 STD=(30368+35270)

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1 31 25 005 005 REV030 STD=35270=(30368+35270)/CFM ALL 1 31 25 006 005 REV030 STD=35270=(30368+35270)/CFM

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1 31 40 019 001 REV024 EQ 200 1283-1305 1 31 40 020 105 REV043 CODE 0622

1 31 40 021 001 REV031 CODE 0621 0588-1102 1 31 40 022 100 REV042 CODE 1459

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1 31 40 023 100 REV026 M : 24035=24160=24189 ALL 1 31 40 024 001 REV024

N 1 31 40 025 001 REV023 0588N 1 31 40 026 100 REV034 CODE 1363

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1 31 40 027 100 REV038 CODE 1647 1283-1305 1 31 40 028 205 REV036 CODE 0676

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1 31 45 010 110 REV041 36562=36609=36772 1048-1305

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1 31 45 011 001 REV023 STD=26358+30980 0588-1102 1 31 45 012 100 REV023 M:22707

1 31 45 011 100 REV036 M:26358 1283-1305 1 31 45 012 100 REV023 M:22707

N 1 31 45 013 001 REV023 0588N 1 31 45 014 001 REV024 CODE 0611

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1 31 45 016 100 REV031 CODE 1754 1048-1305

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1 31 45 019 202 REV038 CODE 1897 1048-1305 1 31 45 020 100 REV024 CODE 0686

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1 31 65 001 001 REV023 ALL 1 31 65 002 001 REV023

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N 1 32 20 005 001 REV039 0588

1 32 20 005 103 REV036 28479=28702=28916 1048-1305

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1 32 30 003 105 REV042 CODE 0265 ALL 1 32 30 004 100 REV030 M:30062

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1 35 30 001 110 REV041 26923=27255=27572 1048-1305 1 35 30 002 001 REV023

1 35 30 003 001 REV038 ALL

1 35 40 001 112 REV023 CODE 0465 ALL 1 35 40 002 112 REV023 CODE 0225

1 35 50 001 001 REV031 STD=M:25110 ALL

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1 36 10 001 001 REV023 ALL 1 36 10 002 001 REV023

1 36 10 003 001 REV023 ALL 1 36 10 004 050 REV024 CODE 1034

1 36 10 005 001 REV040 STD ALL 1 36 10 006 100 REV035 CODE 0226

1 36 10 007 001 REV023 MOD:STD=(30368+35270) ALL 1 36 10 008 001 REV023

1 36 10 009 001 REV023 ALL 1 36 10 010 001 REV023

1 36 20 001 001 REV023 ALL 1 36 20 002 001 REV023

1 36 20 003 001 REV023 M:STD=(30368+35270) ALL 1 36 20 004 100 REV036 M:24805

1 36 20 005 001 REV036 M:STD=(30368+35270) ALL 1 36 20 006 100 REV023 M:24805

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1 38 10 001 001 REV023 1048-1305 1 38 10 002 105 REV036 CODE:1482

N 1 38 10 003 001 REV023 0588N 1 38 10 004 100 REV034 20109

1 38 10 003 001 REV023 1048-1305 1 38 10 004 210 REV034 MOD 20109+26250

N 1 38 10 005 100 REV023 M:20109 0588

1 38 10 005 205 REV036 M:20109+26250 1048-1305

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1 45 10 001 001 REV023 0588-1102 1 45 10 002 001 REV023 STD OR (27522+28360)

1 45 10 001 001 REV023 1283-1305 1 45 10 002 100 REV028 CODE 1026

1 45 10 003 100 REV032 23119=22013 ALL 1 45 10 004 001 REV023

1 45 10 005 001 REV023 ALL

1 45 20 001 001 REV043 STD=M:27522+28360 0588-1102 1 45 20 002 001 REV023

1 45 20 001 100 REV043 CODE 1893 1283-1305 1 45 20 002 001 REV023

1 45 20 003 103 REV032 CODE 0363 1048-1305 1 45 20 004 001 REV032

N 1 45 20 003 200 REV032 20201+24287 0588N 1 45 20 004 001 REV032

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1 45 20 007 001 REV032 ALL 1 45 20 008 001 REV023

1 45 20 009 100 REV023 CODE 0366 0588 1283-1305

N 1 45 25 001 001 REV030 STD=M:25293+28552 0588

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1 46 10 001 100 REV043 CODE 1210 1283-1305 1 46 10 002 100 REV043 CODE 0587

1 46 20 001 100 REV028 CODE 1028 1283-1305 1 46 20 002 100 REV028 CODE 0511

1 46 20 003 100 REV028 CODE 0513 1283-1305 1 46 20 004 100 REV028 CODE 0514

1 46 20 005 100 REV028 CODE 1046 1283-1305 1 46 20 006 100 REV028 CODE 1053

1 46 20 007 105 REV037 CODE 1056 1283-1305 1 46 20 008 100 REV038 CODE 1028

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1 46 30 003 100 REV029 CODE 1026 1283-1305

1 46 60 001 100 REV028 CODE 1061 1283-1305

1 46 70 001 100 REV028 CODE 0634 1283-1305

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1 49 20 003 001 REV023 ALL 1 49 20 004 100 REV042 CODE 1878

1 49 20 005 103 REV032 CODE 0226 ALL 1 49 20 006 100 REV023 CODE 0226

1 49 30 001 100 REV032 M:22013 OR 24105 OR 28160 ALL

1 52 00 001 001 REV038 STD =20062+22188 ALL

1 52 10 001 106 REV023 M:24105 ALL 1 52 10 002 001 REV023

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1 52 10 003 001 REV023 1048-1305 1 52 10 004 100 REV039 M:26088

1 52 10 005 100 REV035 32088=32090 ALL 1 52 10 006 103 REV032 M:24105

1 52 10 007 103 REV023 M:24105=(AFR+24105) ALL 1 52 10 008 100 REV038 32088=32090

1 52 10 009 001 REV023 ALL 1 52 10 010 103 REV025 M:24105

1 52 10 011 103 REV039 24105=24105+30020 ALL

1 52 20 001 203 REV024 CODE 1039 ALL 1 52 20 002 100 REV034 MOD 24105

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1 70 20 005 120 REV040 M:32619=33239/ALL CFM 1048-1305 1 70 20 006 100 REV041 32619=33239=32619+33239/CFM

1 70 30 001 105 REV023 MOD.22112/CFM ALL ALL 1 70 30 002 005 REV023 CFM=PW

1 70 30 003 005 REV023 CFM=PW ALL 1 70 30 004 105 REV023 24035=24160=24211/ CFM/PW

1 70 30 005 065 REV039 CFM ALL ALL 1 70 30 006 060 REV039 CFM/PW ALL

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1 70 40 003 105 REV034 22238/CFM ALL 1 70 40 004 005 REV023 CFM ALL

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1 70 60 001 005 REV023 CFM ALL ALL 1 70 60 002 005 REV023 CFM ALL

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1 70 90 005 105 REV033 CODE 1642/CFM ALL ALL 1 70 90 006 025 REV023 CODE 1051/56-5-B

1 70 90 007 005 REV033 20484+27441/CFM ALL 1 70 90 008 148 REV033 22707/CFM 56-5-B

1 70 90 009 118 REV033 24035=24160=24189/CFM ALL ALL 1 70 90 010 107 REV028 CODE 1052/CFM ALL

1 70 90 011 005 REV023 CFM ALL ALL 1 70 90 012 105 REV023 CODE 1052/CFM ALL

N 1 70 90 013 110 REV042 24035=24160=24189/CFM 0588N 1 70 90 014 045 REV042 STD/CFM 56-5-B

1 70 90 013 250 REV042 CODE 1100 CFM ALL 1048-1305 1 70 90 014 160 REV042 35220=30660+35220/56-5-B

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MV REV MOD MP TITLET SB VALIDITY

. 040A ...... K0385 LIGHTS-CABIN-MODIFY SIGN CONTROL OF FSB ........... EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A ...... K4453 COMMUNICATION - INSTALL AN ALL CABIN ATTENDA ........... CALL PUSH BUTTON IN THE FLIGHT COMPARTMENT EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A ...... K5043 COMMUNICATIONS - CIDS - CABIN CONFIGURATION ........... FOR NON-SMOKING FLIGHTS EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A ...... P0164 COMMUNICATIONS - DATA LINK SYSTEM - ........... DEFINE PIN PROGRAMMING ALL

. 036A ...... P2878 INDICATING RECORDING SYSTEM - SDAC - ........... DEFINE A PIN PROGRAM FOR REAR C.C. VENTILATION ALL

. 041 ...... P6146 INDICATING/RECORDING SYSTEM - FWC - ........... INTRODUCE �F/CTL FLAP LVR NOT ZERO� RED WARNING EI-DEZ EI-DFA

. 042 ...... P8232 INDICATING/RECORDING SYSTEMS - FWC - 31-1266 02 INTRODUCE IAS DISCREPANCY AND DUAL PITOT MONITORING ON FWC H2F1 EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 20024 ...... FUEL- INSTALL A CENTRE TANK SYSTEM- ........... ALL

N 043D 20036 ...... COMMUNICATIONS - HF SYSTEM - INSTALL 23-1202 09 SYSTEM PROVISION FOR A SINGLE SYSTEM - F-OOUA

N 043D 20037 ...... COMMUNICATIONS - HF SYSTEM - INSTALL 23-1202 09 A FULL PROVISION FOR A SINGLE SYSTEM - F-OOUA

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. 036A 20042 ...... LIGHTS - EXTERNAL LIGHTS - INSTALL ........... LOGO LIGHTS ALL

N 043D 20048 ...... AIR CONDITIONING- FLIGHT COMPARTMENT- ........... INSTALL ELECTRICAL FOOT WARMERS- F-OOUA

. 036A 20059 ...... AIR CONDITIONING - CARGO COMPARTMENT - ........... VENTILATION - INSTALL SYSTEM IN AFT COMPARTMENT - ALL

. 036A 20067 ...... FIRE PROTECTION - FWD CARGO COMPARTMENT - ........... INSTALL SMOKE DETECTION SYSTEM - ALL

. 036A 20069 ...... FIRE PROTECTION - AFT CARGO COMPARTMENT - ........... INSTALL SMOKE DETECTION SYSTEM - ALL

. 036A 20071 ...... FIRE PROTECTION - CARGO COMPARTMENT ........... FIRE EXTINGUISHING - INSTALL A SINGLE SHOT SYSTEM - ALL

. 036A 20073 ...... INDICATING/RECORDING SYSTEMS - ........... INSTALL AN AIRCRAFT INTEGRATED DATA SYSTEM - ALL

. 036A 20081 ...... LIGHTS - EXTERIOR LIGHTS - INSTALL ........... SYNCHRONIZED STROBE LIGHTS ALL

. 036A 20109 ...... WATER/WASTE- INSTALL VACUUM TOILET ........... SYSTEM - ALL

. 036A 20137 ...... COMMUNICATIONS - RADIO MANAGEMENT - ........... INSTALL A 3RD RMP - EI-DFP EI-DEY EI-DEZ EI-DFA

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. 036A 20164 ...... FUEL - REFUEL/DEFUEL SYSTEM - ........... INSTALL A FUEL QUANTITY PRE-SELECTOR IN FLIGHT COMPARTMENT - ALL

. 036A 20167 ...... STRUCTURE - REINFORCE STRUCTURE TO ........... ALLOW MTOW 72T-MLW 63T-MZFW 59T DESIGN WEIGHTS ALL

N 043D 20170 ...... COMMUNICATIONS - HF SYSTEM - INSTALL 23-1024 45 A SINGLE SYSTEM F-OOUA

. 036A 20201 ...... COMMUNICATIONS-INSTALL DATA LINK SYSTEM ........... F-OOUA EI-DFP EI-DEY

. 036A 20230 ...... LIGHTS - NAVIGATION LIGHTS - INSTALL A ........... SECOND NAVIGATION LIGHT SYSTEM - ALL

. 036A 20268 ...... WINGS-WING TIP FENCES-INTRODUCE WING ........... TIPS INCLUDING FENCES- ALL

. 036A 20283 ...... COMMUNICATIONS - PROVIDE �HOT MIKE� ........... RECORDING ALL

N 043D 20316 ...... NAVIGATION - AIR DATA - INSTALL METRIC ........... ALTIMETER - F-OOUA

. 036A 20319 ...... ICE AND RAIN PROTECTION-WINDSHIELD ........... RAIN PROTECTION - ADD AN INTERMITTENT FUNCTION EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 20324 ...... FUEL - COUPLING REFUEL/DEFUEL - 28-1030 10 ADD COUPLING ON LH WING (72T MTOW A/C) ALL

. 036A 20327 ...... MINOR IMPROVEMENTS INTRODUCED FROM ........... A/C 60 - AS ZONE - ALL

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. 036A 20994 ...... LANDING GEAR-WHEELS AND BRAKES-INSTALL ........... BSCU STD5- ALL

. 036A 21003 ...... WATER/WASTE - RELOCATE POTABLE WATER ........... TANK - ALL

. 042 21204 ...... COMMUNICATIONS - ACARS - MANAGEMENT UNIT NON 23-1076 14 INSTALLATION - ADAPT SYSTEM EI-DFP EI-DEY

. 036A 21213 ...... ELECTRICAL POWER - DC GENERATION - ........... REVISE �BAT OFF� INDICATION - ALL

. 036A 21230 ...... ELECTRCIAL POWER - DC - IMPROVE BCL - ........... ALL

. 036A 21237 ...... APU - INTRODUCE APU MODE 6 AND ........... ASSOCIATED ECB (GARRETT) ALL

. 036A 21678 ...... ELECTRICAL POWER-AC/DC ESSENTIAL POWER ........... DISTRIBUTION-PROVIDE PROVISIONS FOR ETOPS- ALL

. 036A 21679 ...... HYDRAULIC POWER-MODIFY ELECTRICAL ........... ROUTING OF GREEN LEAKAGE MEASUREMENT ELECTROVALVE CONTROL ALL

N 043D 21858 ...... COMMUNICATIONS - INSTALL HF1 FOR EROPS 23-1024 45 F-OOUA 23-1049 16

. 036A 21964 ...... FLIGHT CONTROLS - ELAC/EFCS SYSTEM - ........... INTRODUCE SOFTWARE L62 ALL

. 036A 22089 ...... ENGINE FUEL AND CONTROL - EIU/CFM - ........... INTRODUCE SOFTWARE 11 ALL

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. 036A 22112 ...... MINOR IMPROVEMENTS INTRODUCED FROM ........... A/C 268 - AS ZONE ALL

. 036A 22238 ...... ENGINE FUEL AND CONTROL - CFM 56 - ........... INTRODUCE EIU VERSION 12 AND ADDITIONAL WIRING ALL

. 036A 22249 ...... AUTO FLIGHT - ACTIVATE WINDSHEAR ........... FUNCTION ALL

. 036A 22311 ...... NAVIGATION - TCAS II - INTRODUCE ........... COMPLETE PROVISIONS ALL

. 036A 22536 ...... NAVIGATION - INSTALL A BENDIX TCAS II ........... COLLISION AVOIDANCE SYSTEM EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 22561 ...... FIRE PROTECTION - LAVATORY SMOKE ........... DETECTION - INTRODUCE AMBIENT SYSTEM ALL

. 036A 22562 ...... AIRBORNE AUXILIARY POWER UNIT - ........... INTRODUCE APIC APS-3200 ALL

. 036A 22567 ...... EQUIPMENT/FURNISHINGS - EMERGENCY ........... EQUIPMENT - INTRODUCE PBE DRAEGER IN THE COCKPIT ALL

. 036A 22706 ...... INDICATING/RECORDING SYSTEMS - CENTRAL ........... WARNING SYSTEM - INSTALL SDAC A320/321 STANDARD ALL

. 036A 22707 ...... INDICATING RECORDING SYSTEMS - EIS - ........... DEFINE COF A STANDARD FOR A320/A321 DMC ALL

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. 036A 22769 ...... NAVIGATION - GPWS - INSTALL GPWC ........... MARK V WITH INTERFACE WITH CFDS ALL

N 043D 22791 ...... NAVIGATION-ATC MODE �S�(SELECT) INSTALL ........... ATC/TCAS CONTROL PANEL P/N 6990/20 (BFE) F-OOUA

. 036A 22875 ...... ICE AND RAIN PROTECTION - ICE DETECTION - ........... INSTALL DUAL ADVISORY ICE DETECTION SYSTEM ALL

. 036A 22941 ...... EQUIPMENT/FURNISHINGS - COCKPIT SEATS - ........... INTRODUCE TYPE A340 SEATS ALL

. 036A 23099 ...... COMMUNICATIONS - ACARS - INSTALL ........... SUNDSTRAND ACARS MANAGEMENT UNIT BFE F-OOUA EI-DFP EI-DEY

. 036A 23119 ...... HYDRAULIC POWER-BLUE MAIN HYDRAULIC ........... POWER-IMPROVE MAINTENANCE STATUS OF BLUE HYDRAULIC RESERVOIR ALL

. 036A 23124 ...... AIR CONDITIONING - PRESSURIZATION ........... CONTROL - IMPROVE CONTROLLER TO ENABLE USE OF EXTERNAL MODE ALL

. 036A 23208 ...... LANDING GEAR - WHEELS AND BRAKES - ........... INTRODUCE BSCU STD 6 ALL

N 043D 23227 ...... NAVIGATION - INSTALL A TCAS II ........... COLLISION AVOIDANCE SYSTEM (HONEYWELL) F-OOUA

. 036A 23344 ...... AIR CONDITIONING - IMPROVE CABIN PRESSURIZA- ........... TION CONTROL ON 25VU PANEL. ALL

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MV REV MOD MP TITLET SB VALIDITY

. 036A 23577 ...... EQUIPMENT/FURNISHINGS-COCKPIT SEATS- ........... INTRODUCE ADDITIONAL BONDING STRIP ON FOURTH CREW MEMBER�S SEAT ALL

. 036A 23585 ...... AUTO FLIGHT - FCU - INTRODUCE FCU ........... M-9 STD ALL

. 036A 23642 ...... LIGHTS - COCKPIT ILLUMINATION - ........... INTRODUCE IMPROVED COCKPIT LIGHTING ALL

. 036A 23672 ...... NAVIGATION - ADIRS - INSTALL LITTON ........... 4MCU ON A321 A/C ALL

. 036A 23742 ...... AUTO FLIGHT - FCU - INTRODUCE FCU ........... STANDARD M10 ALL

. 036A 23795 ...... HYDRAULIC POWER - INDICATING - REMOVE ........... SENSOR AND ASSOCIATED WIRING FOR BLUE RESERVOIR INDICATION ALL

. 036A 23839 ...... FIRE PROTECTION - DETECTION - INTRODUCE ........... MODIFIED ENGINE AND APU FIRE PANEL ALL

. 036A 24035 ...... INDICATING/RECORDING SYSTEMS - ........... GENERAL- DEFINE CPIP3 ALL

. 036A 24064 ...... AUTO FLIGHT-FMS-INTRODUCE FMGC A320/321 ........... B1 STD WITH OPTIONS AND 400 KILOWORDS FOR CFM 56 VERSIONS ALL

N 043D 24075 ...... NAVIGATION - SATELLITE NAVIGATION - ........... INSTALL SUPPLEMENTARY MEANS OF NAV BASED ON HONEYWELL GPS (HYBRID ARCHI.) F-OOUA

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. 036A 24077 ...... LANDING GEAR - BSCU - TWIN WHEEL - ........... INTRODUCE A320/A321 STD 6 VERSION 60C ALL

. 036A 24105 ...... FUSELAGE - REAR FUSELAGE - ADAPT ........... SECTION 17/19 STRUCTURE TO A319 DEFINITION ALL

. 042 24121 ...... WATER/WASTE - GENERAL - ADAPT ........... WATER/WASTE SYSTEM TO A319 DEFINITION ALL

. 036A 24139 ...... AIR CONDITIONING - COCKPIT AND CABIN ........... TEMPERATURE CONTROL - INTRODUCE ZONE TEMPERATURE CONTROLLER -03 ALL

. 036A 24215 ...... AUTO FLIGHT - FAC - INSTALL TWO FACS ........... P/N BAM 0509 ALL

. 036A 24287 ...... INDICATING/RECORDING SYSTEMS - CFDR - ........... INTRODUCE CFDIU STD -7 ALL

. 036A 24351 ...... INDICATING/RECORDING SYSTEMS - ........... ELECTRICAL CLOCK - INSTALL A CLOCK SMITHS TYPE 2610 ALL

. 036A 24414 ...... AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU) ........... DELETE �EXPEDITE� FUNCTION FROM FCU ALL

. 036A 24449 ...... LANDING GEAR - A320/A321 TWIN WHEELS - ........... INTRODUCE BSCU STANDARD 7 (70B VERSION) ALL

. 036A 24511 ...... FLIGHT CONTROLS -S.E.C. SYSTEM ........... INTRODUCE A320/A321 S.E.C STANDARD P/N BAM0508 ALL

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MV REV MOD MP TITLET SB VALIDITY

. 036A 24588 ...... AUTO FLIGHT-FAC-INTRODUCE FAC ........... P/N BAM 510 ALL

N 043D 24624 ...... COMMUNICATIONS - INTRODUCE SSCVR LORAL ........... FAIRCHILD P/N 200-0012 F-OOUA

. 036A 24745 ...... FLIGHT CONTROLS-SEC SYSTEM-�PARTIAL ........... LIFT DUMPING� FUNCTION ACTIVATION ALL

. 040 24748 ...... NAVIGATION-SWITCHING AND INDICATING- ........... INTRODUCE RMI/VOR/DME SEXTANT WITH MODIFIED SOFTWARE ALL

. 036A 24805 ...... PNEUMATIC-ENGINE BLEED AIR SUPPLY- ........... INTRODUCE A BLEED AIR MONITORNG COMPUTER STD6 ALL

. 036A 24851 ...... ICE AND RAIN PROTECTION-ICE DETECTION- ........... PROVIDE ICE DETECTOR ILLUMINATION ALL

. 042 24917 ...... FLIGHT CONTROLS-INTRODUCE ELAC STD ........... L69J ALL

. 036A 25184 ...... NAVIGATION-TCAS-INSTALL ATC/TCAS ........... CONTROL PANEL SEXTANT P/N 04-AA01. ALL

N 043D 25205 ...... NAVIGATION-PRIMARY MEANS USING 34-1132 02 HONEYWELL GPS (HYBRID ARCHITETURE) PROVIDING RAIM FUNCTION (CL) F-OOUA

. 036A 25287 ...... POWERPLANT - GENERAL - INSTALL ON A319 ........... ENGINE RATED VERSION OF CFM 56-5B6 23500 LBS ALL

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. 036A 25293 ...... INDICATING/RECORDING SYSTEM - INSTALL ........... A PORTABLE DATA LOADER CONNECTOR AND DISK STOWAGE EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 25294 ...... NAVIGATION - ADIRS - INSTALL HONEYWELL ........... ADIRS CAPABLE OF A319 A/C ALL

. 036A 25295 ...... AUTOFLIGHT - FMGC - ACTIVATE ACARS ........... INTERFACE IN FMS (CFM AND IAE ENGINES) EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 25296 ...... FLIGHT CONTROLS - FCDC SYSTEM - PROVIDE ........... A VISUAL INDICATION FOR SIMULTANEOUS SIDE STICK ACTION ALL

. 036A 25345 ...... AUTOFLIGHT-FCU-INTRODUCE F.C.U. ........... STANDARD M11 ALL

. 036A 25346 ...... AUTOFLIGHT-FCU-INTRODUCE FCU ........... STANDARD M11 WITHOUT EXPEDITE FUNCTION ALL

. 036A 25381 ...... AUTOFLIGHT - FMGC - ACTIVATE PRINTER ........... INTERFACE IN FMS (CFM AND IAE ENGINES) EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 25404 ...... EXHAUST-THRUST REVERSER CONTROL AND ........... INDICATING-ACTIVATE ADDITIONAL THRUST REVERSER LOCK CONTROL ALL

. 036A 25409 ...... INDICATING RECORDING SYSTEMS-DMC- ........... INTRODUCE D.M.C. V31 STANDARD ALL

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. 036A 25419 ...... ICE AND RAIN PROTECTION-WINDSHIELD ........... RAIN PROTECTION-DESACTIVATION OF RAIN REPELLENT SYSTEM ALL

. 036A 25440 ...... NAVIGATION - GENERAL - CHANGE ........... EQUIPMENTS TO COMPLY WITH MARCH 95 SPECS. EI-DFP EI-DEY EI-DEZ EI-DFA

. 039 25480 ...... NAVIGATION - R.M.I. - INSTALL ........... VOR/ADF/DDRMI (SEXTANT) P/N 63543-253-2 EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 25529 ...... NAVIGATION - WEATHER RADAR SYSTEM - ........... ACTIVATE PREDICTIVE WINDSHEAR FUNCTION EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 25530 ...... ENGINE - COMBUSTION SECTION - ........... INTRODUCE DOUBLE ANNULAR COMBUSTOR ON CFM56-5B6 (CFM56-5B6/2) ALL

. 039 25590 ...... INDICATING/RECORDING SYSTEMS - FWC - 31-1113 30 DEFINE OEB REMINDER WITHIN FWC STD -E1 31-1264 04 AND SUBSEQUENT EI-DFP EI-DEY EI-DEZ EI-DFA

. 039 25819 ...... NAVIGATION - WEATHER RADAR SYSTEM - 34-1176 05 ACTIVATE DUAL PREDICTIVE WINDSHEAR FUNCTION EI-DFA

. 036A 25863 ...... AUTO FLIGHT - FCU - DEFINE FLIGHT 22-1058 46 DIRECTOR ENGAGEMENT IN CROSSED BARS AT GO AROUND ALL

. 036A 25871 ...... ENGINE FUEL AND CONTROL-CONTROLLING- 73-1051 03 INTRODUCE ECU SOFTWARE 5DH FOR CFM56-5B (DAC -DAC/P) ENGINES ALL

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. 036A 25901 ...... INDICATING/RECORDING SYSTEMS-ELECTRICAL ........... CLOCK- INSTALL SEXTANT CLOCK IN PLACE OF SMITHS BASIC CLOCK EI-DFP

. 036A 25999 ...... ELECTRICAL POWER-DC GENERATION- ........... MODIFY TRANSFORMER RECTIFIER OVERHEAT PROTECTION EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 26018 ...... INDICATING/RECORDING SYSTEMS-DISPLAY 31-1107 02 MANAGEMENT COMPUTER (DMC)-INTRODCUE DMC V32 STD ALL

. 039 26088 ...... DOORS EMERGENCY ESCAPE SLIDE RELEASE & ........... OVERPRESS. WARNING SYSTEMS-MODIFY CTRL LOGIC OF THE OVERPRESS. WARNING SYST EI-DFP EI-DEY EI-DEZ EI-DFA

N 043D 26093 ...... AUTOFLIGHT-F.M.G.C.-INTRODUCE FMGC BAM- 22-1060 02 205 (CFM56-5A AND 5B) F-OOUA

. 036A 26194 ...... NAVIGATION - WEATHER RADAR SYSTEM - ........... ALLIED SIGNAL CONFIGURATION AND FULL PROVISION FOR A SECOND TRANSCEIVER EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 26203 ...... COMMUNICATIONS - SSCVR - INSTALL SSCVR ........... ALLIED SIGNAL P/N 980-6022-001 EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 26250 ...... WATER/WASTE-TOILET SYSTEM-INTRODUCE ........... MODIFIED TOILET ASSY EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 26274 ...... NAVIGATION - ADF - INSTALL A SECOND ADF ........... RECEIVERS EI-DFP EI-DEY EI-DEZ EI-DFA

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. 036A 26275 ...... NAVIGATION-WEATHER RADAR SYSTEM- ........... INSTALL FULL PROVISION FOR 2ND TRANSCEIVER EI-DEY EI-DEZ EI-DFA

. 036A 26358 ...... AUTOFLIGHT-FLIGHT CONTROL UNIT- ........... (FCU) INTRODUCE SEXTANT MODULAR FCU EI-DEZ EI-DFA

. 036A 26363 ...... AIR CONDITIONING-AIR COOLING SYSTEM- ........... INTRODUCE MODIFIED RAM AIR OUTLET EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 26497 ...... AUTO FLIGHT-GENERAL-ACTIVATE GLOBAL 22-1072 03 SPEED PROTECTION AND F/D DISENGAGEMENT UPON SPEED CONSTRAINTS ALL

. 036A 26526 ...... NAVIGATION - GPWS - ACTIVATE 34-1202 03 ENHANCED FUNCTIONS OF THE EGPWS ALL

. 036A 26540 ...... INDICATING/RECORDING SYSTEMS - FWC - 31-1115 12 PROVIDE NEW SYNTHETIC VOICE �DUAL INPUT� ALL

N 043D 26680 ...... NAVIGATION - TCAS - INSTALL HONEYWELL 34-1159 09 TCAS COMPUTER P/N 7517900-10002 F-OOUA

N 043D 26799 ...... AUTO FLIGHT-FMGC-INTRODUCE FMGC BAM0206 22-1063 03 (CAPABLE A319 AUTOLAND/GPS PRIMARY) ON CFM POWERED A/C F-OOUA

. 036A 26923 ...... OXYGEN-PASSENGER OXYGEN-INTRODUCE ........... MODIFIED CHEMICAL OXYGEN CONTAINER (DRAEGER) P/N -0004 EI-DEY EI-DEZ EI-DFA

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. 036A 26963 ...... ICE AND RAIN PROTECTION-WINSHIELD RAIN 30-1037 02 PROTECTION-ACTIVATION OF RAIN REPELLENT SYS.(FLUID COMPATIBLE WITH OZONE RULES) ALL

. 036A 26968 ...... AUTO FLIGHT-FMGC-INTRODUCE FMGC CAM0102 ........... FOR A319 AUTOLAND AND GPS/ACARS FOR CFM ENGINES EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 26999 ...... NAVIGATION - MMR - INSTALL COLLINS MMR ........... PROVIDING ILS AND GPS FUNCTION EI-DEZ EI-DFA

. 036A 27014 ...... HYDRAULIC POWER-AUXILIARY HYDRAULIC ........... POWER-INTRODUCE MODIFIED SUNDSTRAND RAM AIR TURBINE EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27255 ...... OXYGEN - PASSENGER OXYGEN SYSTEM - ........... INTRODUCE OXYGEN CONTAINER DRAGER P/N -0003 EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27256 ...... AUTO FLIGHT - MULTIPURPOSE CONTROL AND ........... DISPLAY UNIT (MCDU) - INTRODUCE MCDU HONEYWELL 2ND GENERATION (P/N -980) EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27276 ...... FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE 27-1121 01 ELAC SOFTWARE �L80� ALL

. 036A 27285 ...... NAVIGATION-ATC MODE�S�-INTRODUCE ........... ATC/TCAS CONTROL UNIT P/N C12404AB02 EI-DFP EI-DEY EI-DEZ EI-DFA

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. 036A 27320 ...... INFORMATION SYSTEM-AIR TRAFFIC AND INFO ........... MANAGEMENT SYS(ATIMS)-COCKPIT-INTRODUCE SYS PROVISIONS FOR FANS �A�(ATSU-2DCDU) EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27330 ...... INDICATING/RECORDING SYSTEMS - 31-1133 06 ELECTRICAL CLOCK- INSTALL AIR PRECISION P/N APE5100-1 CAPABLE OF GPS TIME EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27498 ...... ELECTRICAL POWER - GENERAL - AC-DC ........... MAIN DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27522 ...... INFORMATION SYSTEM - AIR TRAFFIC AND ........... INFORMATION SYSTEM (ATIMS) - INSTALL ATSU COMPUTER FOR ACARS EI-DEZ EI-DFA

. 036A 27541 ...... AUTO FLIGHT - MCDU - INSTALL AN MCDU ........... 2ND GENERATION HONEYWELL FMS (MCDU WITH A340 KEYBOARD) EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27572 ...... OXYGEN-PASSENGER OXYGEN-INTRODUCE ........... MODIFIED CHEMICAL OXYGEN CONTAINER -15 MIN- PURITAN EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27624 ...... EQUIPMENT/FURNISHINGS-MISCELLANEOUS 23-1157 20 EMERGENCY EQUIPMENT-INSTALL ELT CEIS A06V2 WITH CONTROL PANEL IN COCKPIT F-OOUA EI-DFP EI-DEZ EI-DFA

. 036A 27646 ...... NAVIGATION - MMR - INSTALL SEXTANT MMR ........... PROVIDING ILS (FM IMMUNE) EI-DFP EI-DEY EI-DEZ EI-DFA

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. 036A 27698 ...... NAVIGATION - TCAS - INSTALL ALLIED 34-1177 17 SIGNAL TCAS COMPUTER P/N 066-50000-2220 (WITH CHANGE 7.0) EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27699 ...... COMMUNICATIONS - AUDIO MANAGEMENT ........... SYSTEM - INSTALL SATCOM AMU AND ACP EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 27993 ...... AIR CONDITIONING - PACK COOLING AIR ........... CONTROL - INTRODUCE LOGIC RELAY FOR CONTROL PACK CLOSURE AT ENGINE START EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 28138 ...... COMMUNICATIONS-SATELLITE COMMUNICATION- ........... INSTALL A COLLINS AERO I SATCOM AVIONIC (6 CHANNELS) EI-DEZ EI-DFA

. 036A 28218 ...... NAVIGATION-ADIRS-INTRODUCE LITTON ........... ADIRU 4 MCU STD-312 EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 28244 ...... NAVIGATION-GPWS-INTRODUCE EGPWS 34-1193 36 P/N 206-206 AND INHIBIT AUTOMATIC DEACTIVATION ENHANCED FUNCTIONS ALL

. 036A 28293 ...... NAVIGATION - WEATHER RADAR SYSTEM - ........... REINSTALL A SINGLE WEATHER RADAR CONFIGURATION EI-DEY EI-DEZ EI-DFA

. 036A 28308 ...... INDICATING RECORDING SYSTEM-DMC- 31-1127 INTRODUCE DMC V40 STANDARD ALL

. 036A 28369 ...... INDICATING/RECORDING SYSTEMS - DMC - ........... DISPLAY ALTITUDE IN METRIC UNITS ON THE PRIMARY FLIGHT DISPLAY (PFD) EI-DEY EI-DEZ EI-DFA

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. 042 28377 ...... ICE AND RAIN PROTECTION-WINSHIELD- 30-1037 02 RAIN PROTECTION-INTRODUCE MODIFIED GAGE ASSY -P/N 4020W35-2 ALL

. 036A 28382 ...... NAVIGATION - MMR - ACTIVATE GPS PRIMARY ........... FUNCTION (HYBRID) IN SEXTANT MMR (WITH HONEYWELL OR LITTON ADIRU) EI-DFP EI-DEY EI-DEZ EI-DFA

. 041A 28479 ...... INDICATING RECORDING SYSTEM-FWC- 31-1257 01 INTRODUCE FWC STANDARD H2/E3P EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 28482 ...... LANDING GEAR-NOSE LANDING GEAR 32-1217 WHEELS-REMOVE RUBBING STRIPS EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 28495 ...... NAVIGATION - MMR - REMOVE COLLINS MMR ........... PROVIDING ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION (PREVIOUS SPEC.) EI-DEZ EI-DFA

. 036A 28558 ...... ICE AND RAIN PROTECTION-ICE DETECTION- ........... INTRODUCE ICE DETECTOR P/N 0871 DP4 EI-DEZ EI-DFA

. 040 28658 ...... NAV-STANDBY DATA: ATT AND HDG-INTRODUCE ........... COMPLETE PROV FOR INTEGRATED STANDBY INSTRUMENT SYSTEM ELECTRICAL SUPPLY EI-DEZ EI-DFA

. 042 28667 ...... ICE AND RAIN PROTECTION-WINDSHIELD RAIN 30-1037 02 PROTECTION-INTRODUCE MODIFIED GAGE ASSY WITH INPUT VALUE FUNCTION SUPPRESSED ALL

N 043D 28738 ...... NAVIGATION - TCAS - INSTALL HONEYWELL 34-1206 18 COMPUTER TCAS 2000 CHANGE 7.0 WITH HONEYWELL ATC F-OOUA

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N 043D 28739 ...... NAVIGATION - TCAS - INSTALL HONEYWELL 34-1206 18 TCAS 2000 COMPUTER (WITH CHANGE 7.0) WITH COLLINS ATC TPR720 OR TPR900 F-OOUA

. 036A 28916 ...... INDICATING RECORDING SYSTEM-FWS 31-1257 01 INTRODUCE FWC STANDARD H1PE3P EI-DFP EI-DEY EI-DEZ EI-DFA

. 038A 30062 ...... LANDING GEAR-PARKING/ULTIMATE 32-1201 04 EMERGENCY BRAKING-INTRODUCE A PRESSURE SWITCH ALL

. 036A 30162 ...... COMMUNICATION-SATCOM-ACTIVATE SATCOM ........... AERO-I COLLINS COCKPIT VOICE FUNCTION EI-DEZ EI-DFA

. 039 30365 ...... INDICATING RECORDING SYSTEM-SDAC- 31-1144 02 INTRODUCE STANDARD SDAC P/N 31-1265 03 350E5500202 EI-DFP EI-DEY EI-DEZ EI-DFA

. 041A 30660 ...... INDICATING/RECORDING SYSTEMS - FWC - 31-1257 01 INSTALL FWC STANDARD H2E4 EI-DFP EI-DEY EI-DEZ EI-DFA

. 037A 31040 ...... AUTO-FLIGHT - FLIGHT AUGMENTATION 22-1102 02 COMPUTER (FAC) - INTRODUCE FAC SOFTWARE �BAM0616� EI-DFP EI-DEY EI-DEZ EI-DFA

. 042A 31056 ...... INDICATING/RECORDING SYSTEM-DMC- 31-1286 INTRODUCE DMC V50 STANDARD ALL

. 041A 31283 ...... INDICATING RECORDING SYSTEM-FWC- 31-1257 01 INTRODUCE FWC STANDARD H2 F1 EI-DFP EI-DEY EI-DEZ EI-DFA

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. 036A 31395 ...... FLIGHT CONTROLS - ELAC SYSTEM - 27-1135 02 INTRODUCE ELAC STD L81 ALL

. 042B 32087 ...... COMMUNICATIONS-ANTI HIJACK CAMERA 23-1382 04 MONITORING-INSTALL A COCKPIT DOOR SURVEILLANCE SYSTEM EI-DFP EI-DEY EI-DEZ EI-DFA

. 036A 32088 ...... EQUIPMENT FURNISHINGS-CURTAINS AND 25-1287 05 PARTITIONS-MODIFIED INTRUSION AND 25-1305 06 PENETRATION RESISTANT COCKPIT DOOR ALL

. 036A 32090 ...... DOORS-PASSENGER COMPARTMENT FIXED 25-1287 05 INTERIOR DOORS-INSTALL ELECTRICAL 25-1305 06 COCKPIT DOOR RELEASE SYSTEM ALL

. 037A 32475 ...... AUTOFLIGHT - FMGC - INSTALL NEW THALES 22-1103 04 FMGC EQUIPED WITH FMS2 SMITHS (REV 01) 22-1152 03 FOR CFM ENGINES (BY RETROFIT ONLY) EI-DFP EI-DEY EI-DEZ EI-DFA

. 037A 32766 ...... AUTO FLIGHT - MCDU - 22-1148 11 INSTALL NEW THALES MCDU FOR FMS2 (RETROFIT ONLY) EI-DFP EI-DEY EI-DEZ EI-DFA

. 037B 32997 ...... AUTO FLIGHT - FMGC - INSTALL FMGC CFM 22-1144 01 C13043AA02 THALES 22-1152 03 (EQUIPPED WITH FMS2 THALES/SMITH) EI-DFP EI-DEY EI-DEZ EI-DFA

. 039A 33239 ...... ENGINE FUEL AND CONTROL - FADEC SYSTEM 73-1080 01 - INSTALL �5BL� STANDARD ECU SOFTWARE FOR CFM56-5B ENGINES (A318 CAPABLE) EI-DFP EI-DEY EI-DEZ EI-DFA

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. 039 33299 ...... AUTO FLIGHT - FLIGHT AUGMENTATION 22-1102 02 COMPUTER - INSTALL FAC STANDARD BAM0617 FOR A318 EI-DFP EI-DEY EI-DEZ EI-DFA

. 038 33879 ...... FLIGHT CONTROLS - ELAC SYSTEM - INSTALL 27-1154 ELAC L83 SOFTWARE - RETROFIT ONLY EI-DFP EI-DEY EI-DEZ EI-DFA

. 041A 33907 ...... INDICATING/RECORDING SYSTEMS - FWC - 31-1266 02 INTRODUCE IAS DISCREPANCY AND DUAL PITOT MONITORING ON FWC H2F1 EI-DFP EI-DEY EI-DEZ EI-DFA

. 041 34078 ...... AUTO-FLIGHT - FMGC - INSTALL FMS2 22-1147 01 THALES �S2� ASSOCIATED TO FG STD 22-1152 03 C10 ON CFM ENGINES EI-DFP EI-DEY EI-DEZ EI-DFA

. 037A 34097 ...... FLIGHT CONTROLS - ELAC SYSTEM (ELEVATOR 27-1153 AILERON COMPUTER)- ACTIVATE THE AILERON ANTI-DROOP FUNCTION EI-DFP EI-DEY EI-DEZ EI-DFA

. 039B 34313 ...... AUTO FLIGHT - FMGC - 22-1171 01 INSTALL A NEW FMS2 THALES SMITH S3 STANDARD ON CFM A/C EI-DFP EI-DEY EI-DEZ EI-DFA

. 039 34325 ...... AUTO FLIGHT - FLIGHT MANAGEMENT AND 22-1155 01 GUIDANCE COMPUTER - INSTALL FMGC STD S2C11 ON S/A A/C WITH CFM ENGINES EI-DFP EI-DEY EI-DEZ EI-DFA

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. 042B 35000 ...... COMMUNICATIONS - ANTI HIJACK CAMERA 23-1382 04 MONITORING - REPLACE CDSS LCD/SYSTEM CONTROLLER EI-DFP EI-DEY EI-DEZ EI-DFA

. 043B 35220 ...... INDICATING/RECORDING SYSTEMS - 31-1267 03 FLIGHT WARNING COMPUTER (FWC) - 31-1300 02 INSTALL FWC STANDARD H2F3 EI-DFP EI-DEY EI-DEZ EI-DFA

. 040A 35240 ...... NAVIGATION - ATC/MODE S (SELECT) - 34-1369 01 CERTIFY EHS FUNCTION ALL

N 043D 35803 ...... AIRBORNE AUXILIARY POWER-CONTROL AND 49-1070 MONITORING - INTRODUCE ECB SOFTWARE VERSION 06.00.000 F-OOUA

. 042A 36462 ...... ENGINE FUEL AND CONTROL - FADEC SYSTEM- 73-1086 INSTALL �5BM� STANDARD ECU SOFTWARE FOR CFM 56-5B ENGINES EI-DEY EI-DEZ

. 041 36562 ...... AUTO FLIGHT - FLIGHT MANAGEMENT AND 22-1205 02 GUIDANCE COMPUTER (FMGC) - INSTALL FMS2 THALES S4 (REV2+) STD ON CFM A/C EI-DFP EI-DEY EI-DEZ EI-DFA

. 042 36994 ...... LANDING GEAR - NORMAL BRAKING - 32-1336 01 INSTALL BSCU STD 10 BY SB ONLY ALL

. 042A 37009 ...... INDICATING/RECORDING SYSTEMS - DMC - 31-1286 ACQUISITION/INTERFACE - INTRODUCE DMC-EIS1 STD V60 (SB ONLY) ALL

. 042C 37317 ...... ELECTRICAL POWER - AC ESSENTIAL ........... GENERATION SWITCHING - INSTALL AUTO SWITCHING SYSTEM FOR AC AND DC ESS BUS EI-DFP EI-DEY EI-DEZ EI-DFA

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. 043C 37329 ...... LIGHTS - INSTRUMENT AND PANEL INTEGRAL 33-1057 02 LIGHTING- ENSURE EMERGENCY LIGHTING FOR STAND-BY INSTRUMENTS (WITH ISIS PROV) EI-DFA

. 043 37935 ...... AUTO-FLIGHT - FMGC - INSTALL FMGC 22-1247 01 THALES S4C12 ON CFM A/C EI-DFP EI-DEY EI-DEZ EI-DFA

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ISS MSN 1048-1102

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EQUIPMENT

CONTENTS JUN 10 ISS - 00

25.00 CONTENTS

25.10 FLIGHT DECK

- GENERAL........................................................1 - COCKPIT PLAN ..................................................3 - SEATS ...........................................................6 - COCKPIT WINDOW ..............................................10 - PILOT’S INSTRUMENTS PANELS ...............................11 - PEDESTAL.......................................................13 - OVERHEAD PANEL..............................................14 - C/B PANELS .....................................................15

- FOOT WARMER ..............................................16 25.11 COCKPIT DOOR SECURITY SYSTEM

- DOOR DESCRIPTION............................................1 - COCKPIT DOOR LOCKING SYSTEM ............................2 - CONTROLS ......................................................3 - COCKPIT DOOR SURVEILLANCE SYSTEM .....................7

25.15 IN SEAT POWER SUPPLY SYSTEM

- GENERAL........................................................1 - CONTROLS ......................................................1

25.20 ELECTRICAL SUPPLY

- BUS EQUIPMENT LIST ..........................................1

25.30 EMERGENCY EQUIPMENT

- GENERAL........................................................1 - PORTABLE EMERGENCY EQUIPMENT LOCATION.............2 - PORTABLE EMERGENCY EQUIPMENT LOCATION.............3 - EMERGENCY EQUIPMENT QUANTITY..........................4 - OXYGEN EQUIPMENT...........................................5 - OVERWATER EMERGENCY EQUIPMENT.......................6 - FIRE FIGHTING EQUIPMENT ....................................10 - PORTABLE BREATHING EQUIPMENT (SMOKE HOOD).........13 - NEW TYPE OF SMOKE HOOD...................................15 - MISCELLANEOUS EQUIPMENT .................................17

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EQUIPMENT

EMERGENCY EQUIPMENT JUN 10 ISS - 00

GENERAL This chapter describes systems and equipment that are essential to the safety of passengers and crew in case of fire, rapid depressurization of the cabin, ditching or emergency evacuation. These include:

- oxygen equipment: (see Ch 1.35); - evacuation devices: (see Ch 1.23-1.33 and 1.52); - over-water emergency equipment; - fire-fighting equipment; - miscellaneous equipment.

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EMERGENCY EQUIPMENT JUN 10 ISS - 00

PORTABLE EMERGENCY EQUIPMENT LOCATION

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EMERGENCY EQUIPMENT JUN 10 ISS - 00

PORTABLE EMERGENCY EQUIPMENT LOCATION

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EMERGENCY EQUIPMENT JUN 10 ISS - 00

EMERGENCY EQUIPMENT QUANTITY

Q.ty Item 5 Cabin Crew Life Vests 3 Cockpit Crew Life Vests 1 Constraint Kit 1 Crash Axe 1 Dangerous Goods Kit 2 Demonstration Kit 2 Escape Lines 15 Extension Seat Belts 6 Fire Protection Gloves 3 First Aid Kit 1 First Use Aid Kit (FUAK) 8 Flashlights 5 Halon Fire Extinguisher 15 Infant Life Vests 1 Jetlight 5 Manual Release Tool 2 Megaphone 5 Oxygen Bottle + Oxygen Mask

132 Passenger Life Vests 10 Passenger Life Vests - spare items 3 Seat Belts – spare items 6 Smoke Hood

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EMERGENCY EQUIPMENT JUN 10 ISS - 00

OXYGEN EQUIPMENT GENERAL

The cabin attendants portable devices are high-pressure portable oxygen units, which are installed close to the attendant stations. They provide protection to the cabin crew during emergencies (after decompression, when fire and emission of smoke and noxious gases). they also supply first aid oxygen to passengers.

PORTABLE OXYGEN BOTTLES

For location of oxygen bottles refer to location of the portable emergency equipment; placards show where they are stowed. The capacity of each oxygen bottles is 4,25 cubic feet with a pressure of 1.800 PSI. The following items are fitted on the oxygen bottle’s head: shutoff valve, pressure contents indicators, low constant flow outlet, high constant flow outlet, charging valve and safety outlets. The oxygen bottle has a duration tested at 20,000 ft, of 46 min at the low constant flow outlet and of 26 min at the high constant flow outlet. Operating instructions:

a) extract the mask from pocket on carrying bag. b) ensure connecting tube is attached to a constant flow outlet. c) fully open the shutoff valve then partially close by 1/4. d) place the mask on user's or patient’s face.

Use of oxygen bottle must be reported to the commander.

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EMERGENCY EQUIPMENT JUN 10 ISS - 00

OVER WATER EMERGENCY EQUIPMENT

LIFE VEST

Adult life vest Location Life vest are located in each cockpit and attendant seat (refer to location of the portable emergency equipment); placards show where they are stowed. Also each passenger has under his seat an adult life vest.

Description The LIFE VEST have these main components:

- Inflatable cells. - Waistbelt harness with buckle and harness-pull-tab. - Gas inflation system. - Oral inflation system. - Water-activated light assembly. - Whistle.

Operation WARNING

DO NOT INFLATE THE LIFEJACKET BEFORE LEAVING THE AIRCRAFT!

Each LIFE VEST shows the instruction for its use: 1. Grasp the poly bag and tear the pull-tab free of the bag, thus opening the

sewn end. 2. Remove the life vest from its bag, then unroll it. a) Hold the life vest on each side of the neck opening and put the head through

the opening. b) Run the waistbelt harness around the back of the waist and back to the front. c) Hold the buckle ends:

WARNING Danger of finger clamping by closing the buckle! Close the buckle below the life vest.

Close the buckle below the life vest.

d) Pull the HARNESS PULL-TAB to tighten snugly. Note: Make sure that the life vest is drawn firmly against the body.

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Inflation

CAUTION

ORAL INFLATION PRIOR TO GAS INFLATION WILL CAUSE EXCESSIVE PRESSURE WHICH MAY BURST THE LIFE VEST.

Pull the red JERK TO INFLATE tags, this inflates the buoyancy chambers with the gas inflation system.

a) With the ORAL INFLATOR system you can inflate the life vest yourself. Inflation is done by blowing into the end of the tubes by mouth. b) If more or less pressure in the life vest is necessary, use the ORAL INFLATOR system.

Note: The oral inflation system in each inflatable cell can also be used to release

gas by depressing the valves at the tube ends. Light Assembly Activation The LIGHT ASSEMBLY is activated when the BATTERY is immersed in water.

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EQUIPMENT

EMERGENCY EQUIPMENT JUN 10 ISS - 00

Infant life jacket Similar in construction, operation to an adult lifejacket except it must be inflated on board

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EMERGENCY EQUIPMENT JUN 10 ISS - 00

FIRE FIGHTING EQUIPMENT PORTABLE FIRE EXTINGUISHERS For location details refer to location of the portable emergency equipment. Placards show where they are stowed. All portable fire extinguisher are Halon type.

Description The portable fire extinguisher, filled with HALON 1211, extinguishes small fires as such its capacity is limited. The instruction for operation of the fire extinguisher is shown on a placard bonded on the body of the extinguisher.

Operation

It is recommended to use a smoke hood when fighting a fire. Smoke from fire and gas from the fire extinguisher may cause irritation of the eyes and respiratory organs.

1) Remove the portable fire extinguisher from the bracket.

Read the Instruction, Cautions and Warnings bonded on the fire extinguishers bottle.

2) Carry the portable fire extinguisher by its CARRYING HANDLE; 3) To operate, hold the extinguisher upright; 4) Pull SAFETY PIN; 5) Stand at least 1.8 m (6 ft.) away from the fire and aim the nozzle at the base of flame; 6) To start the flow of extinguishant, hold the device in one hand and firmly press

with the thumb on the LEVER of the TRIGGER;

Note 1: Only the fully developed cloud of extinguishant is effective, not the stream from the nozzle outlet. If the cloud does not developed around the fire, move back. Note 2: NEVER point the full stream into liquid fires. Start at the base and always fight the front of the fire and follow the flames.

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Note 3: When fighting fires on burning solids, apply the extinguishant in sharp bursts 7) To stop the flow of extinguishant, release the LEVER.

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CRASH AXE The crash axe is used to cut through light structures, panels and windows. It has an insulated handle which is resistant to high voltages. The crash axe is put into brackets on board the aircraft. For quantity and location refer to “Portable Emergency Equipment Location”. FIRE FIGHTING GLOVES Fire-fighting gloves are kept in pockets on board of the aircraft. The gloves are for use by crew member to grasp hot metal or burning parts. Placards are pointing to the location of the part’s installation. For location of the gloves refer to location of the portable emergency equipment. Note: The Fire Fighting Gloves are not required to dispatch the flight.

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PORTABLE BREATHING EQUIPMENT (SMOKE HOOD) The smoke hood is a closed circuit protective breathing equipment for use by a crew member, specifically designed to combat fire and to protect from the effect of: - dangerous environment caused by smoke - hypoxia after a cabin decompression. The smoke hood provides sufficient oxygen flow for more than 15 minutes. It is designed to be donned easily and quickly also in presence of glasses, long hair or beards. When donned allows easy movement leaving both hands free. The hood is stored in a special sachet mounted inside a rigid container in a such way that, after opening the container, removing the hood is done with a single movement. The container is equipped with a "Good Condition" indicator on the cover. If a leak occurs, the oxygen will escape from its container and fill the sachet. The inflated sachet will activate a lever system turning the indicator from green to red. This equipment is also certified to be donned by Cabin Attendants to protect them against hypoxia when it is necessary to assist passengers after an emergency descent, if the aeroplane must continue the flight above 12000 feet. For quantity and locations refer to “Portable Emergency Equipment Location” section. Donning/ Operation - Verify "Good Condition" indicator in green band. (see fig. 2);

Note: In case of a rapid decompression above 30.000 ft Cabin Altitude the "Good Condition" indicator may turn to red. However, in this case the hood continues to be operative.

- Grasp the Smoke Hood Container firmly and pull the tamper seal to disengage the cover from the container (see fig. 3);

- Open the cover and remove Smoke Hood from its sealed package pulling it out firmly; the sealed package will brake automatically (See fig. 4);

- Grasp the Smoke Hood with both hands and shake it down to deploy the flexible hood (See fig. 5);

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- Place both thumbs inside the neck seal to open it as shown in fig. 6; With the head bent forward, guide the hood neck seal over the top of the head and down over the face using the hands as shown in fig. 6. As the hood is put on, oxygen starts to flow automatically. The breathing action of wearer ensure correct operation.

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NEW TYPE OF SMOKE HOOD The manufacturer of the equipment in object, will not produce anymore the smoke hood present on board, but will replace it at the expiration limit life with an other of new type. The differences between the actual and the future smoke hoods are:

a) Colour of the container: grey/blu; b) Presence of handle for opening the container of yellow colour; c) Opening the envelope in order to take out the smoke hood.

The smoke hood, inside of the new type of container is identical to that one currently in use and that the "Good Condition Indicator" remain unchanged. For more details a brief description reported below: USE – OPERATION - Check that the good condition indictor is in operating position. - Hold the case in one hand on the handle marked 1 “LIFT” and the other pull

sharply on the grey part of the cover marked 2 “PULL” to brake the protective seal and open the cover.

- Hold the vacuum packed hood in one hand and take it out of the case by pulling it toward you.

- Hold it with one hand and pull one of the tear-off strips. Take out the hood. - Holding the 02 container with both hands, through the fabric, turn the hood

downwards in one clean movement. - Place your thumbs on the orange marks and open the black collar at the base of

the hood. - Pass the hood over your head, starting from the back. Breathe normally. The hood is now operational.

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INSTRUCTIONAL PICTOGRAM AFTER USE Proceed as follows: - Place both thumbs inside the collar, at the front of the hood. - Take hold of the oxygen container, through the fabric. - Pull the hood backwards until completely free of the head. - Place the hood in a dry, fire protected place, away from sources of heat and/or

toxic fumes.

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MISCELLANEOUS EQUIPMENT FIRST AID KIT AND FIRST USE AID KIT (FUAK) For quantity and location refer to “Portable Emergency Equipment Location”. Placards show where they are stowed. The First Aid Kit (FAK) is a white sealed box containing medicines and medical devices useful to give assistance and comfort to injured people. Since it is a MEL item, required by norms, it shall be avoided, as far as possible, its opening for less important needs or little problems not involved with an emergency situation. For these needs the First Use Aid Kit (FUAK) is provided (the red one) containing medicines of common use only. The content of each kit is described inside the box. (refer to OM part A). Note: FUAK is not required to dispatch the aircraft.

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FLASHLIGHT Emergency flashlights, independent of the aircraft emergency lighting system, are stowed in brackets near each flight attendant seat and in the cockpit. For location details refer to location of the portable emergency equipment. Placards show where they are stowed. Two different type of flashlights are installed. One is operated rotating the black reflector assembly, the other is operated by a sliding switch.

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MEGAPHONES The portable has portable megaphones, battery powered, located in the cabin area. For location refer to location of the portable emergency equipment. Placards show where they are stowed. Operation of the Megaphone 1. Hold the megaphone to the mouth. Note: Do not place the hand around the mouthpiece. 2. Point the megaphone towards the passengers.

Do not operate the megaphone near a person’s ears. Amplified sound or howling can cause damage to the inner ear.

3. Contact the mouthpiece of the megaphone with the lips. 4. Push the push-button switch and then speak slowly with a strong

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DANGEROUS GOODS KIT INSTALLATION In order to facilitate the isolation and manipulation of dangerous goods in case of incident caused by their spillages or leakages in passenger cabin, a “Dangerous Good Kit” is installed. This kit, contained in a sealed envelope, is installed in the forward stowage bin left side. The kit includes: one pair of neoprene gloves, two white plastic bags, two red colored ropes for bag tie and one protective breath–mask. The instructions and procedures related to use of “Dangerous Goods Kit” are specified in OM part A chapt. 9 “Flight Crew/Cabin Crew Checklist for Dangerous Goods Incident” and also reported in the CA’s ABN/EMER checklist. At the first flight leg on each A/C or whenever changing aircraft, the SCCM shall check the integrity and location of Dangerous Good Kit. Note: The DANGEROUS GOODS KIT is not required to dispatch the flight. SUPPLEMENTARY LOOP BELT FOR INFANT For location and quantity refer to Emergency Equipment Location chart. CONSTRAINT KIT INSTALLATION is installed. The kit is comprising of a plastic transparent bag containing one cutting tool and ten flexible nylon handcuffs. The kit is installed in the Passenger Cabin (Overhead Stowage Bin–Left Side) near the Dangerous Good Kit. At the first flight leg on each A/C or whenever changing aircraft, the SCCM shall check the integrity and location of the Constraint Kit. DEMONSTRATION KIT For quantity and location refer to “Portable Emergency Equipment Location”. Placards show where they are stowed. The demonstration kit is a grey coloured bag showing a label “Equipaggiamenti dimostrativi”.

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It contains:

- An adult life vest; - An infant life vest; - An oxygen mask;

Note: the life vests and the oxyen mask are labelled “Solo per uso dimostrativo/ Demonstrative Equipment”.

- A seat belt; - A safety instruction card.

Warning: Life vest are not provided with CO2 cartridge and battery. FLU KIT In order to prevent the spread of the influenza A (H1N1), a “FLU KIT” is installed. The kit, contained in a bag labelled” FLU KIT”, is installed in the Last LH Stowage Compartment. The kit includes:

Description Q.ty Disposable latex gloves powder free, hypoallergenic unsterile.

2 packs of 100 pieces

Oro-nasal non-sterile surgical masks 2 packs of 50 pieces Non-sterile cloth gowns with cuffs 5 Remote thermometer “thermofocus” for the detection of temperature on the forehead non-contact

1

Waste bag trasparenti 3

At the first flight leg on each A/C or whenever changing aircraft, the Senior Cabin Crew Member (CA1) shall check the integrity and location of Flu Kit.

Note

The Flu Kit is not required to dispatch the flight

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ISS MSN 1048

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ISS MSN 1102-1305

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ISS MSN 1048-1305

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ISS MSN 0588-1048

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ISS MSN 0588-1048

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ISS MSN 1102-1305

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ISS MSN 0588-1102

ISS

UE

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ISS MSN 1283-1305

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UE

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ISS MSN 0588-1102

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ISS MSN 1283-1305

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ISS MSN 0588-1102

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ISS MSN 0588-1102

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ISS MSN 1283-1305

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ISS MSN 0588-1102

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ISS MSN 0588-1102

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ISS MSN 1283-1305

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ISS MSN 1283-1305

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UE

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ISS MSN 0588-1102

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ISS MSN 1283-1305

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ISS MSN 0588-1102

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ISS MSN 1283-1305

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ISS MSN 0588-1102

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: 11

-Jun

-201

0

ISS MSN 0588

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 1048-1305

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 1048-1305

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 0588

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 0588

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 1048-1305

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 1048-1305

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 0588

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS MSN 1048-1305

ISS

UE

DA

TE

: 11

-Jun

-201

0

ISS ALL

ISS

UE

DA

TE

: 01

-Mar

-201

0