Airbus 319, A320, A321 Fcom

CCM ALL

318/319/320/321 FCOM VOL.1 REV035 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 ----------------------------------------------------------------------------

1068 OO-SSB 1145 OO-SSF

CCM 1.00.70 01 DEC 2002 PAGE : CRT001

318/319/320/321 FCOM VOL. 1 SYSTEMS DESCRIPTION HIGHLIGHTS REV035

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

1 20 10 001 103 REV035 24105=(24105+US)

- TECHNICAL AMENDMENT 1)Description updated, to indicate that the aircraft is equipped with one observer seat.

1 20 20 002 001 REV035

- TECHNICAL AMENDMENT Modification of the >Antennas Location> drawing to : 1)Correctly position the TCAS antennas. 2)Add the SATCOM antenna.

1 21 10 015 001 REV035

- TECHNICAL AMENDMENT 1)Deletion of the forward cargo heating note, as the forward cargo heating option is not installed. 2)Minor text modifications for improved technical understanding and FCOM standardization.

1 21 20 007 001 REV035

- TECHNICAL AMENDMENT 1)Deletion of reference to the forward cargo outlet isolation valve, since forward cargo ventilation is not installed.

1 21 20 009 001 REV035

- TECHNICAL AMENDMENT 1)Deletion of reference to the forward cargo outlet isolation valve, since forward cargo ventilation is not installed.

1 21 20 013 001 REV035

- TECHNICAL AMENDMENT 1)Deletion of the forward passenger door airstairs indication, as it is not installed.

1 22 10 012 100 REV028 27256

- INCORPORATION OF MOD 27256 - DELETION OF MOD 27541

1 22 10 016 100 REV026 M:27256=27541=(27256+27541)

- DELETION OF MOD 27541

1 22 20 002 110 REV032 CODE 0072

1 22 20 005 110 REV026 CODE 0072

01 DEC 2002 CCM 1.00.75 PAGE 1

1 22 20 006 110 REV026 CODE 0072

1 22 20 008 100 REV026 CODE 0072

1 22 20 014 110 REV028 CODE 0207

1 22 20 023 001 REV035 CODE 0358

- TECHNICAL AMENDMENT 1)No technical change. Page covering the Honeywell or Thales-Smiths FMS2 introduction.

1 22 20 025 001 REV035 CODE 0358

1 22 20 026B 001 REV035 CODE 0358

- TECHNICAL AMENDMENT 1)No technical change. New page introduced for repagination purposes.

1 22 20 027 001 REV035 CODE 0358

- TECHNICAL AMENDMENT 1)Page moved for repagination purposes. 2)Information regarding the PERF factor for CFM 56-5B engines has been moved from the previous and next page. 3)Some figures have been corrected for CFM 56-5B engines.

1 22 30 042 205 REV035 CODE 0377

- TECHNICAL AMENDMENT 1)No technical change. The sequence number has changed to ensure correct validity to all customers.

1 22 30 051 001 REV035 STD=(20701+23892)

1 22 30 052 001 REV035 CODE 0387

01 DEC 2002 CCM 1.00.75 PAGE 2

1 22 30 056 115 REV035 CODE 0416

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631

1 22 30 056A 100 REV035 25863

- INCORPORATION OF MOD 25863 - TECHNICAL AMENDMENT 1)No technical change. New page created for repagination purposes.

1 22 30 057 100 REV035 CODE 0379

- INCORPORATION OF MOD 24160 - INCORPORATION OF MOD 24211 - TECHNICAL AMENDMENT 1)No technical change. New page created for repagination purposes.

1 22 30 071 200 REV025 CODE 0389

1 22 40 005 120 REV035 24215=24588=25534 CFM:ALL

- INCORPORATION OF MOD 24215 - INCORPORATION OF MOD 25534 - VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers.

1 23 20 005 100 REV035 27699=(27699+31907)

- TECHNICAL AMENDMENT 1)Note added to explain the procedure to couple the DME reception to the ILS or MLS reception.

1 25 00 001 001 REV035

- TECHNICAL AMENDMENT 1)Page updated to reflect the new cockpit door security chapter configuration.

1 25 20 001 001 REV035

- TECHNICAL AMENDMENT 1)Page modified to address the Cockpit Door Surveillance System.

1 26 20 001 005 REV024 CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE

01 DEC 2002 CCM 1.00.75 PAGE 3

1 26 40 002 102 REV035 22561=(20067+20069+22561)

- INCORPORATION OF MOD 22561 - TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers.

1 26 50 003 410 REV035 CODE 0324

- TECHNICAL AMENDMENT 1)Revision of the DISCH light description to emphasize that the amber >DISCH> light does not come on as soon as the DISCH pushbutton is pressed, but takes about 60 seconds, which is the approximate agent bottle discharge time.

1 27 20 008 005 REV023 CFM ALL

1 27 40 001 001 REV035

- TECHNICAL AMENDMENT 1)Information has been moved from 1-27-40, page 2.

1 27 40 002 001 REV035

- TECHNICAL AMENDMENT 1)Text modified for improved technical understanding and standardization. 2)The description of the pitch trim wheel has been enhanced to highlight the fact that, in flight, the relation between the aircraft CG and trim position displayed on the wheel does not apply. 3)Information has been moved to 1-27-40 p1.

1 27 50 003 001 REV035

- TECHNICAL AMENDMENT 1)Reference to a specific VFE value has been deleted, in order to have a common page for aircraft having higher VFE.

1 28 10 006 105 REV023 CODE 0106/CFM ALL

1 28 20 012 105 REV023 M:20024/CFM ALL

1 31 10 002 001 REV035

- TECHNICAL AMENDMENT 1)A recommendation is added to point out that the level 2 amber cautions must

01 DEC 2002 CCM 1.00.75 PAGE 4

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- be considered as soon as possible (time and situation permitting), to avoid any further degradation of the affected system.

1 31 25 002 005 REV030 CFM ALL

1 31 25 003 005 REV026 CFM ALL

1 31 25 005 005 REV030 CFM ALL

1 31 25 006 005 REV030 CFM

1 31 25 007 005 REV030 CFM ALL

1 31 40 004 005 REV026 CFM ALL

1 31 40 015 001 REV035

- TECHNICAL AMENDMENT 1)PFD drawing improved. 2)Page modified to highlight the fact that vertical speed is not only inertial, but based on both inertial and barometric data.

1 31 40 022 100 REV034 CODE 0331

- INCORPORATION OF MOD 26485

1 31 40 028 100 REV034 CODE 0331

1 31 45 018 101 REV035 M:26526=(26526+28308+28811)

- TECHNICAL AMENDMENT 1)Text moved to 1-34-70, page 8, and slightly modified for improved technical understanding.

1 31 45 018 200 REV035 M:26526+28308

- TECHNICAL AMENDMENT 1)Text moved to 1-34-70, page 8, and slightly modified for improved technical understanding.

1 31 45 021 200 REV035 CODE 0183

- TECHNICAL AMENDMENT 1)Page modified to include the overflow arrow in the item 9 description. 2)Information has been moved to the next

01 DEC 2002 CCM 1.00.75 PAGE 5

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- page to accommodate additional text on this page.

1 31 45 022 100 REV035 M:22536=23227=23529

- INCORPORATION OF MOD 22536 - INCORPORATION OF MOD 23227 - INCORPORATION OF MOD 23529 - TECHNICAL AMENDMENT 1)Text moved from the previous page to accommodate additional information on page 21.

1 34 10 001 203 REV023 CODE 0010

- INCORPORATION OF MOD 23510 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495

1 34 10 003 100 REV023 CODE 0407

- INCORPORATION OF MOD 23885 - INCORPORATION OF MOD 24075 - INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 27646 - INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635

1 34 10 009 001 REV025 STD=M:23450=(23450+20406)

- TECHNICAL AMENDMENT MEMO DISPLAY UPDATED

1 34 15 003 110 REV032 CODE:0101

- INCORPORATION OF MOD 27646 - DELETION OF MOD 30241 - DELETION OF MOD 30631 - DELETION OF MOD 30635

1 34 30 003 200 REV025 CODE 0077

- INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 - DELETION OF MOD 27646

1 34 60 003 100 REV035 CODE 0013

- TECHNICAL AMENDMENT 1)A note has been added to indicate that, if the selected weather radar fails when two weather radars are installed, the PWS function is recovered by selecting the non-failed weather radar on the control panel.

1 34 70 001 109 REV035 CODE 0230

- TECHNICAL AMENDMENT

01 DEC 2002 CCM 1.00.75 PAGE 6

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- 1)Suppression of the Geometric Altitude description that was inadvertently introduced on this page. 2)TAD and TCF have been added to the list of events that can cause the GPWS light to come on. 3)Text modified for improved technical understanding.

1 34 70 002 103 REV035 26526

- TECHNICAL AMENDMENT 1)Page updated to further specify the aircraft definition : GPWS / G/S pushbuttons on the glareshield.

1 34 70 006 001 REV035

- TECHNICAL AMENDMENT 1)The conditions for activating GPWS Modes 4A and 4B have been revised to reflect the actual design. 2)Addition of a note to highlight the fact that the upper operational limit is reduced to 800 feet, when an overflight is detected.

1 34 70 007 103 REV035 M:26526

- TECHNICAL AMENDMENT 1)Page modified to explain that the glideslope alert is normally only triggered with the gear down, except for a few airports. 2)Addition of a note to explain the fact that the upper operational limit of the Mode 4C warning envelope linearly depends on the aircraft speed.

1 34 70 008 100 REV035 MOD 28244 OR (26526 + 28244)

- TECHNICAL AMENDMENT 1)Text moved from 1-31-45 page 18, for improved technical understanding.

1 34 97 001 206 REV035 CODE 0399

- INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495

1 34 97 001 206 REV025 CODE 0051

1 34 97 001 206 REV035 CODE 0399

- TECHNICAL AMENDMENT 1)The DDRMI has been moved to the NAVAIDS section for improved technical understanding and standardization.

1 36 10 006 100 REV035 22562=(22562+25888+27609)

- INCORPORATION OF MOD 22562 - TECHNICAL AMENDMENT 1)New page corresponding to the APIC

01 DEC 2002 CCM 1.00.75 PAGE 7

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- APS 3200 APU : The APU bleed valve is operated by fuel pressure.

1 70 00 001 005 REV023 CFM ALL

1 70 00 002 005 REV023 CFM ALL

1 70 10 001 120 REV028 CODE:0227/CFM 56-5-B

1 70 20 001 005 REV023 CFM ALL

1 70 20 002 105 REV024 MOD.22238/CFM ALL

1 70 20 005 005 REV028 CFM ALL

1 70 20 006 005 REV032 CFM ALL

1 70 30 001 105 REV023 MOD.22112/CFM ALL

1 70 30 002 005 REV023 CFM=PW

1 70 30 003 005 REV023 CFM=PW

1 70 30 004 105 REV023 24035 CFM/PW

1 70 30 005 005 REV023 CFM=PW

1 70 30 006 005 REV023 STD=M:27441 CFM ALL

1 70 40 001 105 REV024 CODE:0204/CFM

1 70 40 002 005 REV023 CFM ALL

1 70 40 004 005 REV023 CFM ALL

01 DEC 2002 CCM 1.00.75 PAGE 8

1 70 40 004 005 REV023 CFM ALL

1 70 40 006 005 REV023 CFM ALL

1 70 40 007 005 REV023 CFM ALL

1 70 50 001 005 REV023 CFM ALL

1 70 60 001 005 REV023 CFM ALL

1 70 60 002 005 REV023 CFM ALL

1 70 70 001 005 REV023 CFM ALL

1 70 70 003 106 REV028 M:25404/CFM ALL

1 70 80 002 005 REV031 CFM

1 70 80 003 005 REV031 CFM

1 70 80 004 005 REV023 CFM ALL

1 70 80 006 005 REV023 CFM ALL

1 70 90 001 005 REV023 CFM ALL

1 70 90 002 005 REV031 CFM

1 70 90 003 005 REV024 CFM ALL

1 70 90 004 005 REV023 CFM ALL

01 DEC 2002 CCM 1.00.75 PAGE 9

1 70 90 005 105 REV033 CODE 0062/CFM ALL

1 70 90 006 025 REV023 CFM56-5-B

1 70 90 007 005 REV033 CFM ALL

1 70 90 008 148 REV033 22707/CFM 56-5-B

1 70 90 009 118 REV033 CODE 0061/CFM ALL

1 70 90 010 107 REV028 M:22707/CFM ALL

1 70 90 011 005 REV023 CFM ALL

1 70 90 012 105 REV023 MOD.22707/CFM ALL

1 70 90 014 146 REV035 26017=22634+26017/CFM 56-5-B

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)Correction of the flight phase inhibitions for the ENG 1(2) THR LEVER FAULT procedure. 2)With the FWC E2 Standard, the >ENG REV UNLOCKED> message is only inhibited in flight phase 8.

1 70 90 015 220 REV026 CODE 0042 CFM ALL

01 DEC 2002 CCM 1.00.75 PAGE 10

318/319/320/321 FCOM VOL.1 (SYSTEMS DESCRIPTION ) -REV 035 LIST OF EFFECTIVE PAGES (LEP) -

M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----EFFECTIVITY-----M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----EFFECTIVITY------------------------------------------------------------------------------------------

1 00 00 001 001 REV024 CONTENTS ALL

1 00 10 001 001 REV034 ORGANIZATION OF THE MANUAL ALL 1 00 10 002 001 REV034

1 00 10 003 001 REV024 ALL 1 00 10 004 001 REV024

1 00 10 005 001 REV024 ALL

R 1 00 20 001 001 REV035 LIST OF CODES ALLR 1 00 20 002 001 REV035 LIST OF CODES

N 1 00 20 013 001 REV035 LIST OF CODES ALLN 1 00 20 014 001 REV035 LIST OF CODES

N 1 00 20 017 001 REV035 LIST OF CODES ALL

R 1 00 30 001 001 REV027 LIST OF NORMAL REVISIONS ALLR 1 00 30 002 001 REV035 LIST OF NORMAL REVISIONS

1 00 35 001 001 REV024 RECORD OF TEMPORARY REV. ALL

R 1 00 36 001 001 REV035 LIST OF EFFECTIVE TR ALL

1 00 40 001 001 REV028 ABBREVIATIONS ALL 1 00 40 002 001 REV031 ABBREVIATIONS

01 DEC 2002 CCM 1.00.80 PAGE 01

1 00 50 001 001 REV023 UNITS CONVERSION TABLE ALL

1 00 60 001 001 REV023 SYMBOLS ALL

R 1 00 70 CRT 001 REV035 CROSS REFERENCE TABLE ALL

R 1 00 75 HL 001 REV035 HIGHLIGHTS ALL

R 1 00 80 LEP 001 REV035 LIST OF EFFECTIVE PAGES ALL

R 1 00 85 LOM 001 REV035 LIST OF MODIFICATIONS ALL

1 20 00 001 001 REV023 ALL

R 1 20 10 001 103 REV035 24105=(24105+US) ALL

R 1 20 20 001 100 REV031 M:24105 ALLR 1 20 20 002 001 REV035

1 20 20 003 206 REV030 M:20268+24105 ALL 1 20 20 004 103 REV032 M:24105

1 21 00 001 001 REV030 ALL

1 21 10 001 001 REV023 ALL 1 21 10 002 001 REV023

1 21 10 003 001 REV023 ALL 1 21 10 004 105 REV028 M:26363

1 21 10 005 100 REV033 M:24139=24340=(24139+24340) ALL 1 21 10 006 105 REV028 M:26363

1 21 10 007 001 REV023 ALL 1 21 10 008 001 REV024

1 21 10 009 100 REV034 26363 ALL 1 21 10 010 001 REV033

1 21 10 011 105 REV032 CODE 0299 ALL 1 21 10 012 001 REV033

1 21 10 013 001 REV023 ALL 1 21 10 014 001 REV023

R 1 21 10 015 001 REV035 ALLR 1 21 10 016 001 REV023

1 21 10 017 001 REV030 ALL 1 21 10 018 001 REV033

1 21 10 019 001 REV023 ALL

1 21 20 001 001 REV032 ALL 1 21 20 002 100 REV023 M:23344

01 DEC 2002 CCM 1.00.80 PAGE 02

1 21 20 003 001 REV033 ALL 1 21 20 004 001 REV023

1 21 20 005 001 REV032 STD=(26251+32221) ALL 1 21 20 006 001 REV023

R 1 21 20 007 001 REV035 ALLR 1 21 20 008 100 REV032 M:23344

R 1 21 20 009 001 REV035 ALLR 1 21 20 010 001 REV025

1 21 20 011 001 REV028 ALL 1 21 20 012 001 REV024

R 1 21 20 013 001 REV035 ALLR 1 21 20 014 100 REV026 M:23124

1 21 30 001 001 REV023 ALL 1 21 30 002 001 REV023 STD=M:28221=28240

1 21 30 003 001 REV026 ALL 1 21 30 004 001 REV026

1 21 30 005 001 REV026 ALL 1 21 30 006 001 REV023

1 21 30 007 001 REV023 ALL 1 21 30 008 001 REV023 STD=M:22190

1 21 30 009 001 REV023 ALL 1 21 30 010 001 REV023 STD=M:22190

1 21 30 011 001 REV023 STD=M:22190 ALL 1 21 30 012 001 REV023 STD=M:22190

1 21 30 013 001 REV030 STD=M:22190 ALL

1 21 40 001 100 REV023 CODE 0105 ALL 1 21 40 002 103 REV023 20059=30067

1 21 40 003 103 REV023 20059=30067 ALL 1 21 40 004 103 REV023 20059=30067

1 21 40 005 100 REV023 CODE 0082 ALL 1 21 40 006 110 REV033 CODE 0337

1 21 40 007 100 REV026 CODE 0341 ALL 1 21 40 008 100 REV023 M:20057=20059=(20057+20059)

1 21 50 001 100 REV025 M:21678 ALL

1 22 00 001 001 REV031 ALL 1 22 00 002 001 REV025

1 22 10 001 001 REV032 ALL 1 22 10 002 001 REV032 CODE 0358

01 DEC 2002 CCM 1.00.80 PAGE 03

1 22 10 003 001 REV025 ALL 1 22 10 004 001 REV025

1 22 10 005 110 REV034 CODE 0296 ALL 1 22 10 006 001 REV023

1 22 10 007 001 REV028 ALL 1 22 10 008 001 REV024

1 22 10 009 001 REV024 ALL 1 22 10 010 105 REV028 M:27541=(27256+27541)

1 22 10 011 100 REV028 M:27541=(27256+27541) ALL 1 22 10 012 100 REV028 27256

1 22 10 013 001 REV023 ALL 1 22 10 014 001 REV025

1 22 10 015 001 REV025 ALL 1 22 10 016 100 REV026 27256

1 22 10 017 100 REV034 23742=(26358+30980) 1068 1 22 10 018 100 REV030 M:23742

1 22 10 017 105 REV034 26358 1145 1 22 10 018 100 REV030 M:23742

1 22 10 019 100 REV023 M:23742 ALL 1 22 10 020 100 REV023 M:23742

1 22 10 021 001 REV025 CODE 0177 ALL 1 22 10 022 200 REV034 23742+24414

1 22 10 023 305 REV034 23585+23742+24414 ALL

1 22 20 001 001 REV023 ALL 1 22 20 002 110 REV032 CODE 0378

1 22 20 003 110 REV034 CODE 0072 ALL 1 22 20 004 001 REV032

1 22 20 011 100 REV027 CODE 0141 ALL 1 22 20 012 001 REV030

1 22 20 015 100 REV026 M:24064=24065=24066=24067 ALL 1 22 20 016 001 REV023

01 DEC 2002 CCM 1.00.80 PAGE 04

1 22 20 017 001 REV025 ALL 1 22 20 018 001 REV025

1 22 20 019 001 REV025 CODE 0358 ALL 1 22 20 020 001 REV025

1 22 20 021 001 REV027 ALL 1 22 20 022 001 REV029 CODE 0358

N 1 22 20 023 001 REV035 CODE 0358 ALLN 1 22 20 024 100 REV034 24064=24065=24066=24067

N 1 22 20 025 001 REV035 CODE 0358 ALLN 1 22 20 026 001 REV032

N 1 22 20 026B 001 REV035 CODE 0358 ALL

1 22 20 029 100 REV030 M:24035=24160=(24189+24211) ALL 1 22 20 030 001 REV030 CODE 0358

1 22 30 001 100 REV033 24035=24160=24211 ALL 1 22 30 002 100 REV026 M:24035=24160=24211

1 22 30 003 001 REV031 ALL 1 22 30 004 215 REV026 CODE 0001

1 22 30 005 100 REV025 M:24035=24160=24189 ALL 1 22 30 006 100 REV029 M:26497

1 22 30 007 001 REV025 ALL 1 22 30 008 303 REV034 CODE 0233

1 22 30 009 001 REV023 ALL 1 22 30 010 001 REV032

1 22 30 011 001 REV026 CODE 0358 ALL 1 22 30 012 001 REV025

1 22 30 013 001 REV025 ALL 1 22 30 014 001 REV025 CODE 0358

1 22 30 015 100 REV033 24035=24160=24211 ALL 1 22 30 016 001 REV025

1 22 30 017 001 REV025 ALL 1 22 30 018 100 REV027 M:24035=24160=24211

1 22 30 019 001 REV025 CODE 0358 ALL 1 22 30 020 001 REV025

1 22 30 021 001 REV032 ALL 1 22 30 022 100 REV026 M:24035=24160=24211

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

01 DEC 2002 CCM 1.00.80 PAGE 05

1 22 30 025 001 REV030 ALL 1 22 30 026 001 REV030

1 22 30 027 100 REV025 M:24035=24160=24211 ALL 1 22 30 028 100 REV026 M:24035=24160=24211

1 22 30 029 001 REV025 ALL 1 22 30 030 001 REV025

1 22 30 031 100 REV025 M:24064=24065=24066=24067 ALL 1 22 30 032 100 REV025 M:26497

1 22 30 033 100 REV034 24035=24160=24211 ALL 1 22 30 034 105 REV034 CODE 0243

1 22 30 035 200 REV025 CODE 0109 ALL 1 22 30 036 100 REV025 M:24035=24160=24211

1 22 30 040A 001 REV032 ALL

1 22 30 040B 100 REV026 M:24035=24160=24211 ALL

N 1 22 30 041 203 REV028 CODE:0002 ALLN 1 22 30 042 205 REV035 CODE 0377

1 22 30 045 100 REV025 M:26497 ALL 1 22 30 046 001 REV025

1 22 30 047 200 REV025 CODE 0380 ALL 1 22 30 048 100 REV025 M:24035=24160=24211

1 22 30 049 001 REV025 ALL 1 22 30 050 001 REV030

N 1 22 30 051 001 REV035 STD=(20701+23892) ALLN 1 22 30 052 001 REV035 CODE 0387

1 22 30 052A 001 REV033 ALL

1 22 30 053 100 REV030 26017 ALL 1 22 30 054 200 REV027 CODE 0238

N 1 22 30 055 001 REV033 ALLN 1 22 30 056 115 REV035 CODE 0416

N 1 22 30 056A 100 REV035 25863 ALL

01 DEC 2002 CCM 1.00.80 PAGE 06

1 22 30 059 001 REV023 ALL 1 22 30 060 001 REV028

1 22 30 061 001 REV028 ALL 1 22 30 062 200 REV031 CODE 0034

1 22 30 063 100 REV031 M:24035=24160=24189 ALL 1 22 30 064 100 REV023 M:24035=24160=24211

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

1 22 30 067 100 REV034 CODE 0388 ALL 1 22 30 068 100 REV034 22013=24105=25225

1 22 30 069 100 REV028 M:24035=24160=24189 ALL 1 22 30 070 106 REV032 M:24035=24160=(24189+24211)

1 22 30 071 200 REV025 CODE 0389 ALL 1 22 30 072 100 REV023 M:24035=24160=24211

1 22 30 073 100 REV032 CODE 0379 ALL 1 22 30 074 100 REV023 M:24035=24160=24211

1 22 40 001 001 REV025 ALL 1 22 40 002 001 REV025

1 22 40 003 110 REV026 M:24105 ALL 1 22 40 004 001 REV024

N 1 22 40 005 120 REV035 24215=24588=25534 CFM:ALL ALLN 1 22 40 006 100 REV025 M:22249

1 22 60 001 200 REV032 CODE 0148 ALL 1 22 60 002 001 REV032

1 22 75 001 100 REV023 ALL

1 23 00 001 001 REV031 CODE 0192 ALL 1 23 00 002 001 REV030

01 DEC 2002 CCM 1.00.80 PAGE 07

1 23 10 001 001 REV023 ALL 1 23 10 002 001 REV033

1 23 10 003 001 REV026 ALL 1 23 10 004 001 REV026

1 23 10 005 100 REV023 M:20137 ALL

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

1 23 20 003 001 REV023 ALL 1 23 20 004 001 REV028

R 1 23 20 005 100 REV035 27699=(27699+31907) ALLR 1 23 20 006 001 REV026

1 23 20 007 001 REV023 ALL 1 23 20 008 001 REV023

1 23 20 009 001 REV026 ALL 1 23 20 010 001 REV028

1 23 20 011 001 REV023 ALL 1 23 20 012 001 REV026

1 23 20 013 001 REV023 ALL 1 23 20 014 001 REV026

1 23 20 015 100 REV023 M:20308=26023=26433=MPK4453 ALL 1 23 20 016 100 REV032 22013=24105=K5070

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

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

1 23 30 001 205 REV028 CODE:0168 ALL 1 23 30 002 001 REV034 STD

1 23 40 001 100 REV025 CODE 0075 ALL 1 23 40 002 100 REV025 CODE:0075

1 23 50 001 001 REV023 ALL

1 23 60 001 001 REV023 ALL

1 24 00 001 001 REV023 ALL

01 DEC 2002 CCM 1.00.80 PAGE 08

1 24 10 001 001 REV023 ALL 1 24 10 002 001 REV023

1 24 10 003 001 REV023 ALL 1 24 10 004 100 REV031 M:22013=24105=28160

1 24 10 005 001 REV023 ALL 1 24 10 006 001 REV023

1 24 10 007 001 REV023 ALL 1 24 10 008 001 REV023

1 24 10 009 001 REV023 ALL 1 24 10 010 001 REV023

1 24 10 011 001 REV023 ALL 1 24 10 012 001 REV023

1 24 10 013 100 REV025 M:22013=24105=28160 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 REV027 ALL 1 24 10 018 001 REV023

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

1 24 20 001 200 REV028 M:21230+27498 ALL 1 24 20 002 200 REV023 M:21230+21213

1 24 20 003 001 REV023 ALL 1 24 20 004 100 REV028 M:27498

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 ALL 1 24 20 010 001 REV023

1 24 20 011 001 REV023 ALL 1 24 20 012 001 REV023

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

1 24 20 017 001 REV023 ALL 1 24 20 018 100 REV033 25999

R 1 25 00 001 001 REV035 ALL

01 DEC 2002 CCM 1.00.80 PAGE 09

1 25 10 001 001 REV031 ALL 1 25 10 002 001 REV034

1 25 10 003 100 REV034 20047=20255=23577 ALL 1 25 10 004 001 REV033

1 25 10 005 001 REV033 ALL 1 25 10 006 100 REV023 M:22941

1 25 10 007 001 REV028 ALL 1 25 10 008 001 REV023

1 25 10 009 001 REV023 ALL 1 25 10 010 001 REV023

1 25 10 011 110 REV029 M:27320 ALL 1 25 10 012 110 REV029 M:27320

1 25 10 013 200 REV029 M:22112+27256 ALL 1 25 10 014 206 REV031 CODE 0278

1 25 10 015 001 REV023 ALL 1 25 10 016 001 REV023

1 25 15 001 001 REV032 STD=27229+27230=27229+27540 ALL

R 1 25 20 001 001 REV035 ALL

1 26 00 001 100 REV034 CODE 0322 ALL

1 26 10 001 100 REV034 MOD 20067=20069=22006 ALL

1 26 20 001 005 REV024 CFM ALL ALL 1 26 20 002 001 REV026

1 26 20 003 100 REV033 23839 ALL 1 26 20 004 001 REV023

1 26 20 005 100 REV026 M:23839 ALL 1 26 20 006 001 REV023

1 26 20 007 001 REV024 ALL 1 26 20 008 001 REV023

1 26 20 009 001 REV023 ALL 1 26 20 010 001 REV023

1 26 30 001 001 REV030 ALL 1 26 30 002 001 REV023

1 26 30 003 001 REV023 ALL

N 1 26 40 001 001 REV030 ALLN 1 26 40 002 102 REV035 22561=(20067+20069+22561)

1 26 50 001 201 REV030 M:20067+20069 ALL 1 26 50 002 300 REV023 CODE 0320

01 DEC 2002 CCM 1.00.80 PAGE 10

R 1 26 50 003 410 REV035 CODE 0324 ALLR 1 26 50 004 200 REV023 CODE:0056

1 26 60 001 100 REV030 M:21678 ALL

1 27 00 001 001 REV023 ALL

1 27 10 001 001 REV034 ALL 1 27 10 002 001 REV023

1 27 10 003 001 REV023 ALL 1 27 10 004 001 REV023

1 27 10 005 100 REV024 M:22013=24105=26334=26335 ALL 1 27 10 006 001 REV023

1 27 10 007 100 REV023 M:21964 ALL 1 27 10 008 001 REV023

1 27 10 009 105 REV028 M:24105 OR 26334 OR 26335 ALL 1 27 10 010 001 REV030

1 27 10 011 405 REV027 M:24105+24511+24745+27276 ALL 1 27 10 012 100 REV030 CODE 0055

1 27 10 013 001 REV030 ALL 1 27 10 014 100 REV024 M:22013=24105=26334=26335

1 27 10 015 001 REV023 ALL 1 27 10 016 100 REV024 M:24105

1 27 10 017 001 REV023 ALL

1 27 20 001 001 REV023 CODE 0054 ALL 1 27 20 002 100 REV023 M:24136

N 1 27 20 003 100 REV028 M:27276 ALLN 1 27 20 004 001 REV023 STD=24105

1 27 20 005 001 REV030 ALL 1 27 20 006 001 REV030

1 27 20 007 100 REV024 M:22013=24105=26334=26335 ALL 1 27 20 008 005 REV023 CFM ALL

1 27 30 001 001 REV023 ALL 1 27 30 002 100 REV023 CODE 0058

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

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

1 27 30 007 001 REV023 ALL

N 1 27 40 001 001 REV035 ALLN 1 27 40 002 001 REV035

01 DEC 2002 CCM 1.00.80 PAGE 11

1 27 40 003 100 REV025 M:25296 OR 25477 OR 26540 ALL 1 27 40 004 100 REV023 M:26540=25477

1 27 40 005 001 REV023 ALL 1 27 40 006 100 REV024 M:22013=24105=26334=26335

1 27 40 007 001 REV023 ALL 1 27 40 008 001 REV023

1 27 40 009 100 REV033 22013=24105=26334=26335 ALL 1 27 40 010 001 REV032

1 27 40 011 100 REV024 M:22013=24105=26334=26335 ALL 1 27 40 012 201 REV033 CODE 0297

1 27 40 013 103 REV026 M:22013=24105=26334=26335 ALL

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

R 1 27 50 003 001 REV035 ALLR 1 27 50 004 001 REV023 STD=M.24105

1 27 50 005 050 REV023 IAE ALL ALL 1 27 50 006 001 REV023

1 27 50 007 001 REV023 ALL 1 27 50 008 001 REV023

1 27 60 001 001 REV023 ALL

1 28 00 001 001 REV023 ALL

1 28 10 001 203 REV025 M.20024+20167 ALL 1 28 10 002 100 REV025 M.20024

1 28 10 003 100 REV023 M.20024 ALL 1 28 10 004 100 REV024 M:20024

1 28 10 005 100 REV026 M:20024 ALL 1 28 10 006 105 REV023 CODE 0106/CFM ALL

1 28 10 007 203 REV024 M:20024+20164 ALL 1 28 10 008 001 REV023

1 28 10 009 001 REV024 ALL

1 28 20 001 100 REV024 M:20024 ALL 1 28 20 002 100 REV024 M:20024

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

1 28 20 005 001 REV023 ALL 1 28 20 006 100 REV023 M:20164=(20164+22802)

1 28 20 007 100 REV023 M:20164 ALL 1 28 20 008 100 REV023 CODE 0064

01 DEC 2002 CCM 1.00.80 PAGE 12

1 28 20 009 100 REV023 M:20024 ALL 1 28 20 010 100 REV025 M:20024

1 28 20 011 100 REV023 CODE 0064 ALL 1 28 20 012 105 REV023 M:20024/CFM ALL

1 28 20 013 203 REV026 M:20024+20164 ALL

1 28 30 001 001 REV025 STD=M:20024 ALL

1 29 00 001 001 REV023 ALL

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

1 29 20 001 001 REV030 ALL 1 29 20 002 001 REV025

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

1 29 20 005 001 REV023 ALL 1 29 20 006 001 REV023

1 29 20 007 001 REV030 STD=M:23795=(23119+23795) ALL 1 29 20 008 001 REV031

1 29 30 001 001 REV024 ALL

1 30 00 001 001 REV034 ALL

1 30 10 001 001 REV028 CODE 0132 ALL

1 30 20 003 100 REV034 22875=28558 ALL

1 30 30 001 110 REV034 20327/CFM ALL ALL 1 30 30 002 100 REV026 M:20327

1 30 30 003 100 REV034 22875=28558 ALL

1 30 40 001 001 REV028 ALL 1 30 40 002 001 REV023

1 30 50 001 001 REV026 ALL 1 30 50 002 001 REV024

1 30 60 001 100 REV032 M:20319 ALL 1 30 60 002 100 REV032 M:20319

1 30 60 003 001 REV023 ALL

01 DEC 2002 CCM 1.00.80 PAGE 13

1 30 70 001 101 REV024 M:22875 ALL

1 30 80 001 100 REV023 M:21678 ALL

1 31 00 001 001 REV023 ALL 1 31 00 002 001 REV033

1 31 00 003 001 REV026 ALL

1 31 05 001 001 REV023 ALL 1 31 05 002 001 REV023

1 31 05 003 001 REV028 ALL 1 31 05 004 001 REV023

1 31 05 005 001 REV032 ALL 1 31 05 006 001 REV026

R 1 31 10 001 001 REV023 ALLR 1 31 10 002 001 REV035

1 31 10 003 001 REV023 ALL 1 31 10 004 100 REV031 CODE 0012

1 31 10 005 200 REV031 CODE 0182 ALL

1 31 15 001 001 REV026 ALL 1 31 15 002 001 REV032

1 31 15 003 001 REV023 ALL 1 31 15 004 100 REV033 26017

1 31 15 005 100 REV023 25410 ALL

1 31 20 001 100 REV026 M:25409=26018=(25409+26018) ALL 1 31 20 002 001 REV033

1 31 20 003 100 REV028 M:25409=26018=(25409+26018) ALL 1 31 20 004 001 REV024

1 31 20 005 002 REV034 CODE 0194 1068 1 31 20 006 001 REV023

1 31 20 005 200 REV034 CODE 0309 1145 1 31 20 006 001 REV023

1 31 25 001 001 REV026 ALL 1 31 25 002 005 REV030 CFM ALL

1 31 25 005 005 REV030 CFM ALL ALL 1 31 25 006 005 REV030 CFM

1 31 25 007 005 REV030 CFM ALL ALL

1 31 30 001 001 REV033 ALL 1 31 30 002 002 REV033

01 DEC 2002 CCM 1.00.80 PAGE 14

1 31 30 003 001 REV032 ALL 1 31 30 004 001 REV032

1 31 30 005 001 REV023 ALL

1 31 40 001 001 REV026 ALL 1 31 40 002 001 REV032

1 31 40 003 001 REV033 ALL 1 31 40 004 005 REV026 CFM ALL

1 31 40 005 001 REV024 ALL 1 31 40 006 001 REV024

1 31 40 007 001 REV026 ALL 1 31 40 008 001 REV026

1 31 40 009 001 REV023 ALL 1 31 40 010 001 REV023

1 31 40 011 001 REV033 1068 1 31 40 012 001 REV028 CODE:0247

1 31 40 011 001 REV033 1145 1 31 40 012 201 REV028 CODE 0145

1 31 40 013 001 REV023 ALL 1 31 40 014 100 REV023 M:22707

R 1 31 40 015 001 REV035 ALLR 1 31 40 016 001 REV024

1 31 40 017 001 REV023 ALL 1 31 40 018 001 REV026

1 31 40 019 001 REV024 ALL 1 31 40 020 001 REV029

1 31 40 021 001 REV031 ALL 1 31 40 022 100 REV034 CODE 0331

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

1 31 40 025 001 REV023 ALL 1 31 40 026 200 REV034 CODE 0078

1 31 40 027 100 REV032 M:26018 ALL 1 31 40 028 100 REV034 CODE 0331

1 31 40 029 200 REV034 CODE 0044 ALL

1 31 45 001 001 REV028 ALL 1 31 45 002 001 REV028

1 31 45 003 001 REV028 ALL 1 31 45 004 001 REV028

01 DEC 2002 CCM 1.00.80 PAGE 15

1 31 45 005 001 REV024 ALL 1 31 45 006 100 REV028 CODE:0045

1 31 45 007 001 REV028 ALL 1 31 45 008 001 REV024

1 31 45 009 100 REV034 CODE 0356 ALL 1 31 45 010 001 REV023

1 31 45 011 001 REV023 ALL 1 31 45 012 100 REV023 M:22707

1 31 45 013 001 REV023 ALL 1 31 45 014 001 REV024

1 31 45 015 001 REV029 ALL 1 31 45 016 100 REV031 CODE 0175

R 1 31 45 017 101 REV032 M:26526 1068R 1 31 45 018 101 REV035 M:26526=(26526+28308+28811)

R 1 31 45 017 101 REV032 M:26526 1145R 1 31 45 018 200 REV035 M:26526+28308

1 31 45 019 002 REV024 ALL 1 31 45 020 100 REV024 CODE 0175

N 1 31 45 021 200 REV035 CODE 0183 ALLN 1 31 45 022 100 REV035 M:22536=23227=23529

1 31 50 001 001 REV029 STD=M:23450=(20406+23450) 1068 1 31 50 002 001 REV029

1 31 50 001 105 REV029 M:26358=(20406+23450+26358) 1145 1 31 50 002 001 REV029

1 31 50 003 100 REV030 M:26526 ALL 1 31 50 004 001 REV026

1 31 55 001 100 REV030 M:27330 ALL 1 31 55 002 110 REV026 MOD.27330=(24351+25901+27330

1 31 55 003 110 REV026 M:27330=(24351+25901+27330) ALL 1 31 55 004 110 REV032 M. 27330=(24351+25901+27330)

1 31 60 001 001 REV033 STD OR 31647 ALL 1 31 60 002 002 REV033

1 31 60 003 100 REV033 20073 ALL 1 31 60 004 110 REV026 M : 20073

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

1 31 65 003 001 REV023 ALL 1 31 65 004 001 REV023

1 31 67 001 001 REV023 ALL

01 DEC 2002 CCM 1.00.80 PAGE 16

1 31 68 001 001 REV023 ALL

1 31 70 001 001 REV032 ALL

1 31 75 001 100 REV028 M:21678 ALL

1 32 00 001 001 REV023 ALL

1 32 10 001 001 REV026 STD=M:20139+22129 ALL 1 32 10 002 001 REV023

1 32 10 003 001 REV023 STD=M:20139+22129 ALL 1 32 10 004 001 REV023

1 32 10 005 001 REV023 STD=M:20139+22129 ALL 1 32 10 006 001 REV023

1 32 10 007 001 REV023 STD=M:20139+22129 ALL 1 32 10 008 001 REV027

1 32 10 009 001 REV023 ALL 1 32 10 010 100 REV030 M:22562

1 32 10 011 001 REV023 ALL 1 32 10 012 001 REV029

1 32 10 013 001 REV023 ALL 1 32 10 014 001 REV023

1 32 10 015 100 REV030 M:22013=24105=28160 ALL 1 32 10 016 001 REV030 STD=M:20139+22129

1 32 10 017 001 REV023 ALL 1 32 10 018 001 REV025

1 32 10 019 100 REV029 M:28482 ALL 1 32 10 020 001 REV023

1 32 10 021 001 REV024 STD=M:20139+22129 ALL 1 32 10 022 001 REV023

1 32 10 023 110 REV029 CODE 0125 ALL

1 32 20 001 002 REV027 ALL 1 32 20 002 002 REV027

1 32 20 003 001 REV023 ALL 1 32 20 004 001 REV023

1 32 20 005 100 REV023 M:24612 ALL

1 32 30 001 100 REV024 M:23208=24077=(23208+24077) ALL 1 32 30 002 001 REV025 STD=M:(20139+22129)

1 32 30 003 100 REV023 M:24449 ALL 1 32 30 004 001 REV023

1 32 30 005 001 REV023 ALL 1 32 30 006 001 REV023 STD=M:(20139+22129)

01 DEC 2002 CCM 1.00.80 PAGE 17

1 32 30 007 001 REV023 ALL 1 32 30 008 100 REV027 M:20994

1 32 30 009 001 REV027 ALL 1 32 30 010 001 REV023

1 32 50 001 001 REV025 ALL

1 33 00 001 001 REV032 ALL

1 33 10 001 001 REV023 ALL 1 33 10 002 100 REV034 23642

1 33 10 003 100 REV023 M:24851 ALL 1 33 10 004 103 REV024 M:24851

1 33 10 005 100 REV023 M:23642 ALL 1 33 10 006 001 REV034

1 33 10 007 100 REV034 23642 ALL

1 33 20 001 001 REV023 ALL 1 33 20 002 200 REV025 M.20042+20081

1 33 20 003 303 REV024 CODE 0124 ALL 1 33 20 004 100 REV023 M:20081

1 33 30 001 001 REV031 ALL 1 33 30 002 103 REV033 24105

1 33 30 003 001 REV031 ALL 1 33 30 004 001 REV025

1 33 40 001 205 REV033 CODE 0193 ALL 1 33 40 002 100 REV034 20081

1 33 50 001 100 REV034 24851 ALL 1 33 50 002 001 REV023

1 34 00 001 001 REV032 ALL 1 34 00 002 001 REV029

N 1 34 10 003 100 REV023 CODE 0407 ALLN 1 34 10 004 100 REV023 CODE 0048

1 34 10 005 001 REV025 ALL 1 34 10 006 001 REV031

1 34 10 007 001 REV023 ALL 1 34 10 008 001 REV033

1 34 10 009 001 REV025 STD=M:23450=(23450+20406) ALL

01 DEC 2002 CCM 1.00.80 PAGE 18

1 34 15 001 110 REV026 CODE:0036 ALL 1 34 15 002 120 REV026 CODE:0036

1 34 15 003 110 REV032 CODE:0101 ALL

1 34 20 001 001 REV023 ALL 1 34 20 002 001 REV033

1 34 20 003 001 REV024 STD=M:21126 ALL

1 34 30 001 001 REV027 ALL 1 34 30 002 001 REV023

1 34 30 003 200 REV025 CODE 0077 ALL 1 34 30 004 001 REV023 STD OR (20210+31003)

1 34 30 005 001 REV023 STD OR(20210+31003) ALL 1 34 30 006 001 REV023

1 34 30 007 001 REV031 STD OR M:27531 ALL 1 34 30 008 001 REV031

1 34 30 009 001 REV032 ALL

1 34 40 001 002 REV024 ALL 1 34 40 002 001 REV023

R 1 34 60 003 100 REV035 CODE 0013 ALLR 1 34 60 004 100 REV026 CODE 0013

R 1 34 70 001 109 REV035 CODE 0230 ALLR 1 34 70 002 103 REV035 26526

1 34 70 003 100 REV026 M:26526 ALL 1 34 70 004 109 REV025 M:26526=(22769+26256)

R 1 34 70 005 110 REV029 M:26526 OR (22769+26526) ALLR 1 34 70 006 001 REV035

R 1 34 70 007 103 REV035 M:26526 ALLR 1 34 70 008 100 REV035 MOD 28244 OR (26526 + 28244)

1 34 70 009 100 REV030 M:26526 ALL 1 34 70 010 103 REV024 M:26526

1 34 70 011 100 REV030 M:26526=(22769+26526) ALL 1 34 70 012 100 REV026 M:26526

1 34 70 013 105 REV032 MOD 28244 OR (26526 + 28244) ALL 1 34 70 014 101 REV027 CODE 0104

01 DEC 2002 CCM 1.00.80 PAGE 19

1 34 80 005 150 REV031 CODE:0245 ALL 1 34 80 006 150 REV028 CODE 0245

1 34 80 007 210 REV031 CODE 0219 1068 1 34 80 008 100 REV031 CODE:0246

1 34 80 007 210 REV031 CODE 0219 1145 1 34 80 008 200 REV031 CODE 0128

1 34 80 013 100 REV024 CODE 0095 ALL

R 1 34 97 001 206 REV035 CODE 0399 ALL

1 35 00 001 001 REV023 ALL

1 35 10 001 001 REV024 ALL

1 35 20 001 001 REV028 ALL 1 35 20 002 001 REV034

1 35 20 003 001 REV023 ALL 1 35 20 004 001 REV034

1 35 20 005 001 REV031 ALL 1 35 20 006 001 REV029

1 35 20 007 001 REV032 ALL 1 35 20 008 001 REV025

1 35 30 001 110 REV032 M:26923=27255=27572 ALL 1 35 30 002 001 REV023

1 35 30 003 001 REV024 ALL

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

1 36 00 001 001 REV023 ALL

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 M.24105=IAE ALL=(IAE+24105)

N 1 36 10 005 001 REV028 ALLN 1 36 10 006 100 REV035 22562=(22562+25888+27609)

01 DEC 2002 CCM 1.00.80 PAGE 20

1 36 10 007 001 REV023 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 ALL 1 36 20 004 100 REV023 M:24805

1 36 20 005 001 REV023 ALL 1 36 20 006 100 REV023 M:24805

1 36 20 007 001 REV023 ALL

1 36 30 001 100 REV023 M:21678 ALL

1 38 00 001 001 REV023 ALL

1 38 10 001 001 REV023 ALL 1 38 10 002 100 REV025 M:21003

1 38 10 003 001 REV023 ALL 1 38 10 004 100 REV034 20109

1 38 10 005 100 REV023 M:20109 ALL

1 38 20 001 100 REV034 MOD 20109 ALL

1 45 00 001 001 REV030 ALL

1 45 10 001 001 REV023 ALL 1 45 10 002 001 REV023 STD OR (27522+28360)

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 REV023 STD=M:27522+28360 ALL 1 45 20 002 001 REV023

1 45 20 003 200 REV032 20201+24287 ALL 1 45 20 004 001 REV032

1 45 20 005 001 REV023 ALL 1 45 20 006 001 REV023

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

1 45 20 009 100 REV023 CODE 0004 ALL

1 45 25 001 100 REV030 M:25293 ALL

1 45 30 001 001 REV023 ALL

01 DEC 2002 CCM 1.00.80 PAGE 21

1 45 40 001 001 REV023 ALL

1 49 00 001 001 REV023 ALL

1 49 10 001 100 REV023 M:22562 ALL 1 49 10 002 001 REV023

1 49 10 003 100 REV023 M:22562OR(22562+25888+27609) ALL

1 49 20 001 100 REV023 CODE 0027 ALL 1 49 20 002 100 REV028 M:22562OR(22562+25888+27609)

1 49 20 003 001 REV023 ALL 1 49 20 004 203 REV024 M:22562+25409

1 49 20 005 103 REV032 M:22562OR(22562+25888+27609) ALL 1 49 20 006 100 REV023 M:22562

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

1 52 00 001 001 REV023 ALL

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

1 52 10 003 001 REV023 ALL 1 52 10 004 001 REV028

1 52 10 005 001 REV023 ALL 1 52 10 006 103 REV032 M:24105

1 52 10 007 103 REV023 M:24105=(AFR+24105) ALL 1 52 10 008 001 REV034

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

1 52 10 011 103 REV034 24105=30020 ALL

1 52 20 001 203 REV024 M:24105+22707 ALL 1 52 20 002 100 REV034 MOD 24105

1 52 30 001 001 REV023 STD=M:(20062+22188) ALL 1 52 30 002 001 REV026 STD=M:(20062+22188)

1 52 40 001 001 REV023 ALL

1 70 00 001 005 REV023 CFM ALL ALL 1 70 00 002 005 REV023 CFM ALL

1 70 10 001 120 REV028 CODE:0227/CFM 56-5-B ALL

1 70 20 001 005 REV023 CFM ALL ALL 1 70 20 002 105 REV024 MOD.22238/CFM ALL

1 70 20 003 001 REV023 ALL 1 70 20 004 001 REV023

01 DEC 2002 CCM 1.00.80 PAGE 22

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 CFM/PW

1 70 30 005 005 REV023 CFM=PW ALL 1 70 30 006 005 REV023 STD=M:27441 CFM ALL

1 70 40 001 105 REV024 CODE:0204/CFM ALL 1 70 40 002 005 REV023 CFM ALL

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

1 70 40 005 105 REV033 CODE:0204/CFM ALL 1 70 40 006 005 REV023 CFM ALL

1 70 40 007 005 REV023 CFM ALL ALL

1 70 50 001 005 REV023 CFM ALL ALL

1 70 70 001 005 REV023 CFM ALL ALL 1 70 70 002 110 REV031 CODE:0018/CFM

1 70 70 003 106 REV028 M:25404/CFM ALL ALL

1 70 80 001 001 REV023 ALL 1 70 80 002 005 REV031 CFM

1 70 80 003 005 REV031 CFM ALL 1 70 80 004 005 REV023 CFM ALL

1 70 80 005 240 REV031 M:22562+27993/CFM ALL 1 70 80 006 005 REV023 CFM ALL

1 70 80 007 320 REV032 CODE 0295/CFM ALL

1 70 90 001 005 REV023 CFM ALL ALL 1 70 90 002 005 REV031 CFM

1 70 90 005 105 REV033 CODE 0062/CFM ALL ALL 1 70 90 006 025 REV023 CFM56-5-B

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

1 70 90 009 118 REV033 CODE 0061/CFM ALL ALL 1 70 90 010 107 REV028 M:22707/CFM ALL

01 DEC 2002 CCM 1.00.80 PAGE 23

1 70 90 011 005 REV023 CFM ALL ALL 1 70 90 012 105 REV023 MOD.22707/CFM ALL

R 1 70 90 013 209 REV024 CODE 0060/CFM ALL ALLR 1 70 90 014 146 REV035 26017=22634+26017/CFM 56-5-B

1 70 90 015 220 REV026 CODE 0042 CFM ALL ALL

1 70 98 001 001 REV028 STD=M:20165 ALL

01 DEC 2002 CCM 1.00.80 PAGE 24

318/319/320/321 FCOM VOLUME : 1 SYSTEMS DESCRIPTION LIST OF MOD/MP/SB AFFECTING THE MANUAL REVISION : 035

MV REV MOD MP TITLET SB VALIDITY

. 034A ...... K0385 LIGHTS - CABIN - MODIFY SIGN CONTROL ........... OF FSB - ALL

. 034A ...... K4453 COMMUNICATION - INSTALL AN ALL CABIN ATTENDA ........... CALL PUSH BUTTON IN THE FLIGHT COMPARTMENT ALL

. 034A ...... K5043 COMMUNICATIONS - CIDS - CABIN CONFIGURATION ........... FOR NON-SMOKING FLIGHTS ALL

N 035 ...... P0164 COMMUNICATIONS - DATA LINK SYSTEM - ........... DEFINE PIN PROGRAMMING ALL

. 034A ...... P2878 INDICATING RECORDING SYSTEM - SDAC - ........... DEFINE A PIN PROGRAM FOR REAR C.C. VENTILATION ALL

. 034A 20024 ...... FUEL- INSTALL A CENTRE TANK SYSTEM- ........... ALL

. 034A 20042 ...... LIGHTS - EXTERNAL LIGHTS - INSTALL ........... LOGO LIGHTS ALL

. 034A 20059 ...... AIR CONDITIONING - CARGO COMPARTMENT - ........... VENTILATION - INSTALL SYSTEM IN AFT COMPARTMENT - ALL

. 034A 20067 ...... FIRE PROTECTION - FWD CARGO COMPARTMENT - ........... INSTALL SMOKE DETECTION SYSTEM - ALL

. 034A 20069 ...... FIRE PROTECTION - AFT CARGO COMPARTMENT - ........... INSTALL SMOKE DETECTION SYSTEM - ALL

. 034A 20071 ...... FIRE PROTECTION - CARGO COMPARTMENT ........... FIRE EXTINGUISHING - INSTALL A SINGLE SHOT SYSTEM - ALL

CCM 1.00.8501 DEC 2002 PAGE 1

. 034A 20073 ...... INDICATING/RECORDING SYSTEMS - ........... INSTALL AN AIRCRAFT INTEGRATED DATA SYSTEM - ALL

. 034A 20081 ...... LIGHTS - EXTERIOR LIGHTS - INSTALL ........... SYNCHRONIZED STROBE LIGHTS ALL

. 034A 20109 ...... WATER/WASTE- INSTALL VACUUM TOILET ........... SYSTEM - ALL

. 034A 20137 ...... COMMUNICATIONS - RADIO MANAGEMENT - ........... INSTALL A 3RD RMP - ALL

. 034A 20164 ...... FUEL - REFUEL/DEFUEL SYSTEM - ........... INSTALL A FUEL QUANTITY PRE-SELECTOR IN FLIGHT COMPARTMENT - ALL

. 034A 20167 ...... STRUCTURE - REINFORCE STRUCTURE TO ........... ALLOW MTOW 72T-MLW 63T-MZFW 59T DESIGN WEIGHTS ALL

. 034A 20201 ...... COMMUNICATIONS-INSTALL DATA LINK SYSTEM ........... ALL

. 034A 20230 ...... LIGHTS - NAVIGATION LIGHTS - INSTALL A ........... SECOND NAVIGATION LIGHT SYSTEM - ALL

. 034A 20268 ...... WINGS-WING TIP FENCES-INTRODUCE WING ........... TIPS INCLUDING FENCES- ALL

. 034A 20283 ...... COMMUNICATIONS - PROVIDE >HOT MIKE> ........... RECORDING ALL

. 034A 20319 ...... ICE AND RAIN PROTECTION-WINDSHIELD ........... RAIN PROTECTION - ADD AN INTERMITTENT FUNCTION ALL

CCM 1.00.8501 DEC 2002 PAGE 2

. 034A 20324 ...... FUEL - COUPLING REFUEL/DEFUEL - 28-1030 04 ADD COUPLING ON LH WING (72T MTOW A/C) ALL

. 034A 20327 ...... MINOR IMPROVEMENTS INTRODUCED FROM ........... A/C 60 - AS ZONE - ALL

. 034A 20994 ...... LANDING GEAR-WHEELS AND BRAKES-INSTALL ........... BSCU STD5- ALL

. 034A 21003 ...... WATER/WASTE - RELOCATE POTABLE WATER ........... TANK - ALL

. 034A 21213 ...... ELECTRICAL POWER - DC GENERATION - ........... REVISE >BAT OFF> INDICATION - ALL

. 034A 21230 ...... ELECTRCIAL POWER - DC - IMPROVE BCL - ........... ALL

. 034A 21237 ...... APU - INTRODUCE APU MODE 6 AND ........... ASSOCIATED ECB (GARRETT) ALL

. 034A 21678 ...... ELECTRICAL POWER-AC/DC ESSENTIAL POWER ........... DISTRIBUTION-PROVIDE PROVISIONS FOR ETOPS- ALL

. 034A 21679 ...... HYDRAULIC POWER-MODIFY ELECTRICAL ........... ROUTING OF GREEN LEAKAGE MEASUREMENT ELECTROVALVE CONTROL ALL

. 034A 21964 ...... FLIGHT CONTROLS - ELAC/EFCS SYSTEM - ........... INTRODUCE SOFTWARE L62 ALL

. 034A 22089 ...... ENGINE FUEL AND CONTROL - EIU/CFM - ........... INTRODUCE SOFTWARE 11 ALL

CCM 1.00.8501 DEC 2002 PAGE 3

. 034A 22112 ...... MINOR IMPROVEMENTS INTRODUCED FROM ........... A/C 268 - AS ZONE ALL

. 034A 22238 ...... ENGINE FUEL AND CONTROL - CFM 56 - ........... INTRODUCE EIU VERSION 12 AND ADDITIONAL WIRING ALL

. 034A 22249 ...... AUTO FLIGHT - ACTIVATE WINDSHEAR ........... FUNCTION ALL

. 034A 22311 ...... NAVIGATION - TCAS II - INTRODUCE ........... COMPLETE PROVISIONS ALL

. 034A 22536 ...... NAVIGATION - INSTALL A BENDIX TCAS II ........... COLLISION AVOIDANCE SYSTEM ALL

. 034A 22561 ...... FIRE PROTECTION - LAVATORY SMOKE ........... DETECTION - INTRODUCE AMBIENT SYSTEM ALL

. 034A 22562 ...... AIRBORNE AUXILIARY POWER UNIT - ........... INTRODUCE APIC APS-3200 ALL

. 034A 22567 ...... EQUIPMENT/FURNISHINGS - EMERGENCY ........... EQUIPMENT - INTRODUCE PBE DRAEGER IN THE COCKPIT ALL

N 035 22572 ...... LANDING GEAR - MLG - IMPROVE LOOM ........... SEGREGATION ALL

. 034A 22634 ...... INDICATING/RECORDING SYSTEMS - CENTRAL ........... WARNING SYSTEM - DEFINE STD FWC FOR A321 ALL

CCM 1.00.8501 DEC 2002 PAGE 4

. 034A 22706 ...... INDICATING/RECORDING SYSTEMS - CENTRAL ........... WARNING SYSTEM - INSTALL SDAC A320/321 STANDARD ALL

. 034A 22707 ...... INDICATING RECORDING SYSTEMS - EIS - ........... DEFINE COF A STANDARD FOR A320/A321 DMC ALL

. 034A 22769 ...... NAVIGATION - GPWS - INSTALL GPWC ........... MARK V WITH INTERFACE WITH CFDS ALL

. 034A 22875 ...... ICE AND RAIN PROTECTION - ICE DETECTION - ........... INSTALL DUAL ADVISORY ICE DETECTION SYSTEM ALL

. 034A 22941 ...... EQUIPMENT/FURNISHINGS - COCKPIT SEATS - ........... INTRODUCE TYPE A340 SEATS ALL

. 034A 23099 ...... COMMUNICATIONS - ACARS - INSTALL ........... SUNDSTRAND ACARS MANAGEMENT UNIT BFE ALL

. 034A 23119 ...... HYDRAULIC POWER-BLUE MAIN HYDRAULIC ........... POWER-IMPROVE MAINTENANCE STATUS OF BLUE HYDRAULIC RESERVOIR ALL

. 034A 23124 ...... AIR CONDITIONING - PRESSURIZATION ........... CONTROL - IMPROVE CONTROLLER TO ENABLE USE OF EXTERNAL MODE ALL

. 034A 23208 ...... LANDING GEAR - WHEELS AND BRAKES - ........... INTRODUCE BSCU STD 6 ALL

. 034A 23344 ...... AIR CONDITIONING - IMPROVE CABIN PRESSURIZA- ........... TION CONTROL ON 25VU PANEL. ALL

N 035 23510 ...... NAVIGATION - ADIRS - ADAPT SHELVES ........... FOR 4 MCU ADIRS INSTALLATION ALL

CCM 1.00.8501 DEC 2002 PAGE 5

. 034A 23577 ...... EQUIPMENT/FURNISHINGS-COCKPIT SEATS- ........... INTRODUCE ADDITIONAL BONDING STRIP ON FOURTH CREW MEMBERHS SEAT ALL

. 034A 23585 ...... AUTO FLIGHT - FCU - INTRODUCE FCU ........... M-9 STD ALL

. 034A 23642 ...... LIGHTS - COCKPIT ILLUMINATION - ........... INTRODUCE IMPROVED COCKPIT LIGHTING ALL

. 034A 23672 ...... NAVIGATION - ADIRS - INSTALL LITTON ........... 4MCU ON A321 A/C ALL

. 034A 23742 ...... AUTO FLIGHT - FCU - INTRODUCE FCU ........... STANDARD M10 ALL

. 034A 23795 ...... HYDRAULIC POWER - INDICATING - REMOVE ........... SENSOR AND ASSOCIATED WIRING FOR BLUE RESERVOIR INDICATION ALL

. 034A 23839 ...... FIRE PROTECTION - DETECTION - INTRODUCE ........... MODIFIED ENGINE AND APU FIRE PANEL ALL

. 034A 24035 ...... INDICATING/RECORDING SYSTEMS - ........... GENERAL- DEFINE CPIP3 ALL

. 034A 24064 ...... AUTO FLIGHT-FMS-INTRODUCE FMGC A320/321 ........... B1 STD WITH OPTIONS AND 400 KILOWORDS FOR CFM 56 VERSIONS ALL

. 034A 24077 ...... LANDING GEAR - BSCU - TWIN WHEEL - ........... INTRODUCE A320/A321 STD 6 VERSION 60C ALL

CCM 1.00.8501 DEC 2002 PAGE 6

. 034A 24084 ...... AUTO FLIGHT - A320/A321 FOR IAE AND CFM ........... ENGINES - INSTALL WIRING PROVISION FOR ENERGY MANAGEMENT ACTIVATION ALL

. 034A 24105 ...... FUSELAGE - REAR FUSELAGE - ADAPT ........... SECTION 17/19 STRUCTURE TO A319 DEFINITION ALL

. 034A 24106 ...... FUSELAGE - DEFINE INTERFACES AND ........... ASSEMBLING OF SECTION 14 TO 15/21 TO A319 DEFINITION ALL

. 034A 24136 ...... FLIGHT CONTROLS - ELAC SYSTEM - ........... INTRODUCE A320/A321 ELAC STD ALL

. 034A 24139 ...... AIR CONDITIONING - COCKPIT AND CABIN ........... TEMPERATURE CONTROL - INTRODUCE ZONE TEMPERATURE CONTROLLER -03 ALL

. 034A 24215 ...... AUTO FLIGHT - FAC - INSTALL TWO FACS ........... P/N BAM 0509 ALL

. 034A 24287 ...... INDICATING/RECORDING SYSTEMS - CFDR - ........... INTRODUCE CFDIU STD -7 ALL

. 034A 24351 ...... INDICATING/RECORDING SYSTEMS - ........... ELECTRICAL CLOCK - INSTALL A CLOCK SMITHS TYPE 2610 ALL

. 034A 24414 ...... AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU) ........... DELETE >EXPEDITE> FUNCTION FROM FCU ALL

. 034A 24449 ...... LANDING GEAR - A320/A321 TWIN WHEELS - ........... INTRODUCE BSCU STANDARD 7 (70B VERSION) ALL

CCM 1.00.8501 DEC 2002 PAGE 7

. 034A 24511 ...... FLIGHT CONTROLS -S.E.C. SYSTEM ........... INTRODUCE A320/A321 S.E.C STANDARD P/N BAM0508 ALL

. 034A 24588 ...... AUTO FLIGHT-FAC-INTRODUCE FAC ........... P/N BAM 510 ALL

. 034A 24612 ...... INDICATING/RECORDING SYSTEMS - FWC - ........... INTRODUCE FWC D2 STD ALL

. 034A 24613 ...... FLIGHT CONTROLS - ELAC - INTRODUCE ........... ELAC STD P/N L69 ALL

. 034A 24745 ...... FLIGHT CONTROLS-SEC SYSTEM->PARTIAL ........... LIFT DUMPING> FUNCTION ACTIVATION ALL

. 034A 24805 ...... PNEUMATIC-ENGINE BLEED AIR SUPPLY- ........... INTRODUCE A BLEED AIR MONITORNG COMPUTER STD6 ALL

. 034A 24851 ...... ICE AND RAIN PROTECTION-ICE DETECTION- ........... PROVIDE ICE DETECTOR ILLUMINATION ALL

N 035 24852 ...... NAVIGATION-ADIRU-INTRODUCE ADIRU ........... P/N -307 ALL

. 034A 24917 ...... FLIGHT CONTROLS-INTRODUCE ELAC STD ........... L69J ALL

. 034A 25184 ...... NAVIGATION-TCAS-INSTALL ATC/TCAS ........... CONTROL PANEL SEXTANT P/N 04-AA01. ALL

. 034A 25287 ...... POWERPLANT - GENERAL - INSTALL ON A319 ........... ENGINE RATED VERSION OF CFM 56-5B6 23500 LBS ALL

CCM 1.00.8501 DEC 2002 PAGE 8

. 034A 25293 ...... INDICATING/RECORDING SYSTEM - INSTALL ........... A PORTABLE DATA LOADER CONNECTOR AND DISK STOWAGE ALL

. 034A 25294 ...... NAVIGATION - ADIRS - INSTALL HONEYWELL ........... ADIRS CAPABLE OF A319 A/C ALL

. 034A 25295 ...... AUTOFLIGHT - FMGC - ACTIVATE ACARS ........... INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

. 034A 25296 ...... FLIGHT CONTROLS - FCDC SYSTEM - PROVIDE ........... A VISUAL INDICATION FOR SIMULTANEOUS SIDE STICK ACTION ALL

. 034A 25335 ...... FLIGHT CONTROLS-ELAC-INTRODUCE A319 EIS ........... L77 SOFTWARE STD- ALL

. 034A 25336 ...... NAVIGATION-ADIRS-INTRODUCE AIRU ........... LITTON P/N -308 ALL

. 034A 25345 ...... AUTOFLIGHT-FCU-INTRODUCE F.C.U. ........... STANDARD M11 ALL

. 034A 25346 ...... AUTOFLIGHT-FCU-INTRODUCE FCU ........... STANDARD M11 WITHOUT EXPEDITE FUNCTION ALL

. 034A 25381 ...... AUTOFLIGHT - FMGC - ACTIVATE PRINTER ........... INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

. 034A 25404 ...... EXHAUST-THRUST REVERSER CONTROL AND ........... INDICATING-ACTIVATE ADDITIONAL THRUST REVERSER LOCK CONTROL ALL

CCM 1.00.8501 DEC 2002 PAGE 9

. 034A 25409 ...... INDICATING RECORDING SYSTEMS-DMC- ........... INTRODUCE D.M.C. V31 STANDARD ALL

. 034A 25410 ...... INDICATING RECORDING SYSTEM-FWC- ........... INTRODUCE F.W.C. E1 STANDARD ALL

. 034A 25419 ...... ICE AND RAIN PROTECTION-WINDSHIELD ........... RAIN PROTECTION-DESACTIVATION OF RAIN REPELLENT SYSTEM ALL

. 034A 25440 ...... NAVIGATION - GENERAL - CHANGE ........... EQUIPMENTS TO COMPLY WITH MARCH 95 SPECS. ALL

. 034A 25529 ...... NAVIGATION - WEATHER RADAR SYSTEM - ........... ACTIVATE PREDICTIVE WINDSHEAR FUNCTION ALL

. 034A 25530 ...... ENGINE - COMBUSTION SECTION - ........... INTRODUCE DOUBLE ANNULAR COMBUSTOR ON CFM56-5B6 (CFM56-5B6/2) ALL

. 034A 25863 ...... AUTO FLIGHT - FCU - DEFINE FLIGHT ........... DIRECTOR ENGAGEMENT IN CROSSED BARS AT GO AROUND ALL

. 034A 25871 ...... ENGINE FUEL AND CONTROL-CONTROLLING- ........... INTRODUCE ECU SOFTWARE 5DH FOR CFM56-5B (DAC -DAC/P) ENGINES ALL

. 034A 25894 ...... FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ........... ELAC SOFTWARE STD L78 ALL

. 034A 25901 ...... INDICATING/RECORDING SYSTEMS-ELECTRICAL ........... CLOCK- INSTALL SEXTANT CLOCK IN PLACE OF SMITHS BASIC CLOCK OO-SSB

CCM 1.00.8501 DEC 2002 PAGE 10

. 034A 25999 ...... ELECTRICAL POWER-DC GENERATION- ........... MODIFY TRANSFORMER RECTIFIER OVERHEAT PROTECTION ALL

. 034A 26000 ...... NAVIGATION-ADIRS-INTRODUCE HONEYWELL ........... ADIRU 4 MCU STD WITH HARDWARE P/N AD09 ALL

. 034A 26001 ...... NAVIGATION-ADIRS-INTRODUCE HONEYWELL ........... 4 MCU P/N AC09 ALL

. 034A 26002 ...... NAVIGATION-ADIRS-INTRODUCE LITTON ADIRU ........... 4 MCU STD WITH P/N-309 (AIME FUNCTION) ALL

. 034A 26017 ...... INDICATING/RECORDING SYSTEMS-FLIGHT ........... WARNING COMPUTER (FWC)-INTRODUCE FWC ST2 E2 ALL

. 034A 26018 ...... INDICATING/RECORDING SYSTEMS-DISPLAY ........... MANAGEMENT COMPUTER (DMC)-INTRODCUE DMC V32 STD ALL

. 034A 26194 ...... NAVIGATION - WEATHER RADAR SYSTEM - ........... ALLIED SIGNAL CONFIGURATION AND FULL PROVISION FOR A SECOND TRANSCEIVER ALL

. 034A 26203 ...... COMMUNICATIONS - SSCVR - INSTALL SSCVR ........... ALLIED SIGNAL P/N 980-6022-001 ALL

. 034A 26250 ...... WATER/WASTE-TOILET SYSTEM-INTRODUCE ........... MODIFIED TOILET ASSY ALL

. 034A 26274 ...... NAVIGATION - ADF - INSTALL A SECOND ADF ........... RECEIVERS ALL

CCM 1.00.8501 DEC 2002 PAGE 11

. 034B 26275 ...... NAVIGATION-WEATHER RADAR SYSTEM- ........... INSTALL FULL PROVISION FOR 2ND TRANSCEIVER OO-SSF

. 034B 26358 ...... AUTOFLIGHT-FLIGHT CONTROL UNIT- ........... (FCU) INTRODUCE SEXTANT MODULAR FCU OO-SSF

. 034A 26363 ...... AIR CONDITIONING-AIR COOLING SYSTEM- ........... INTRODUCE MODIFIED RAM AIR OUTLET ALL

. 034A 26497 ...... AUTO FLIGHT-GENERAL-ACTIVATE GLOBAL ........... SPEED PROTECTION AND F/D DISENGAGEMENT UPON SPEED CONSTRAINTS ALL

. 034A 26526 ...... NAVIGATION - GPWS - ACTIVATE ........... ENHANCED FUNCTIONS OF THE EGPWS ALL

. 034A 26540 ...... INDICATING/RECORDING SYSTEMS - FWC - ........... PROVIDE NEW SYNTHETIC VOICE >DUAL INPUT> ALL

. 034A 26923 ...... OXYGEN-PASSENGER OXYGEN-INTRODUCE ........... MODIFIED CHEMICAL OXYGEN CONTAINER (DRAEGER) P/N -0004 ALL

. 034A 26963 ...... ICE AND RAIN PROTECTION-WINSHIELD RAIN ........... PROTECTION-ACTIVATION OF RAIN REPELLENT SYS.(FLUID COMPATIBLE WITH OZONE RULES) ALL

. 034A 26968 ...... AUTO FLIGHT-FMGC-INTRODUCE FMGC CAM0102 ........... FOR A319 AUTOLAND AND GPS/ACARS FOR CFM ENGINES ALL

. 034B 26999 ...... NAVIGATION - MMR - INSTALL COLLINS MMR ........... PROVIDING ILS AND GPS FUNCTION OO-SSF

CCM 1.00.8501 DEC 2002 PAGE 12

. 034A 27014 ...... HYDRAULIC POWER-AUXILIARY HYDRAULIC ........... POWER-INTRODUCE MODIFIED SUNDSTRAND RAM AIR TURBINE ALL

. 034A 27255 ...... OXYGEN - PASSENGER OXYGEN SYSTEM - ........... INTRODUCE OXYGEN CONTAINER DRAGER P/N -0003 ALL

. 034A 27256 ...... AUTO FLIGHT - MULTIPURPOSE CONTROL AND ........... DISPLAY UNIT (MCDU) - INTRODUCE MCDU HONEYWELL 2ND GENERATION (P/N -980) ALL

. 034A 27276 ...... FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ........... ELAC SOFTWARE >L80> ALL

. 034A 27285 ...... NAVIGATION-ATC MODE>S>-INTRODUCE ........... ATC/TCAS CONTROL UNIT P/N C12404AB02 ALL

. 034A 27320 ...... INFORMATION SYSTEM-AIR TRAFFIC AND INFO ........... MANAGEMENT SYS(ATIMS)-COCKPIT-INTRODUCE SYS PROVISIONS FOR FANS >A>(ATSU-2DCDU) ALL

. 034A 27330 ...... INDICATING/RECORDING SYSTEMS - 31-1133 05 ELECTRICAL CLOCK- INSTALL AIR PRECISION P/N APE5100-1 CAPABLE OF GPS TIME ALL

. 034A 27498 ...... ELECTRICAL POWER - GENERAL - AC-DC ........... MAIN DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS ALL

. 034B 27522 ...... INFORMATION SYSTEM - AIR TRAFFIC AND ........... INFORMATION SYSTEM (ATIMS) - INSTALL ATSU COMPUTER FOR ACARS OO-SSF

CCM 1.00.8501 DEC 2002 PAGE 13

. 034A 27541 ...... AUTO FLIGHT - MCDU - INSTALL AN MCDU ........... 2ND GENERATION HONEYWELL FMS (MCDU WITH A340 KEYBOARD) ALL

. 034A 27572 ...... OXYGEN-PASSENGER OXYGEN-INTRODUCE ........... MODIFIED CHEMICAL OXYGEN CONTAINER -15 MIN- PURITAN ALL

. 034A 27646 ...... NAVIGATION - MMR - INSTALL SEXTANT MMR ........... PROVIDING ILS (FM IMMUNE) ALL

. 034A 27698 ...... NAVIGATION - TCAS - INSTALL ALLIED 34-1177 10 SIGNAL TCAS COMPUTER P/N 066-50000-2220 (WITH CHANGE 7.0) ALL

. 034A 27699 ...... COMMUNICATIONS - AUDIO MANAGEMENT ........... SYSTEM - INSTALL SATCOM AMU AND ACP ALL

. 034A 27993 ...... AIR CONDITIONING - PACK COOLING AIR ........... CONTROL - INTRODUCE LOGIC RELAY FOR CONTROL PACK CLOSURE AT ENGINE START ALL

. 034A 28218 ...... NAVIGATION-ADIRS-INTRODUCE LITTON ........... ADIRU 4 MCU STD-312 ALL

. 034A 28244 ...... NAVIGATION-GPWS-INTRODUCE EGPWS 34-1193 17 P/N 206-206 AND INHIBIT AUTOMATIC DEACTIVATION ENHANCED FUNCTIONS ALL

. 034B 28293 ...... NAVIGATION - WEATHER RADAR SYSTEM - ........... REINSTALL A SINGLE WEATHER RADAR CONFIGURATION OO-SSF

. 034B 28308 ...... INDICATING RECORDING SYSTEM-DMC- ........... INTRODUCE DMC V40 STANDARD OO-SSF

CCM 1.00.8501 DEC 2002 PAGE 14

. 034B 28360 ...... INFORMATION SYSTEMS-ATIMS-REMOVE ........... ATSU INSTALLATION BACK TO ACARS PROVISIONS OO-SSF

. 034B 28369 ...... INDICATING/RECORDING SYSTEMS - DMC - ........... DISPLAY ALTITUDE IN METRIC UNITS ON THE PRIMARY FLIGHT DISPLAY (PFD) OO-SSF

. 034A 28382 ...... NAVIGATION - MMR - ACTIVATE GPS PRIMARY ........... FUNCTION (HYBRID) IN SEXTANT MMR (WITH HONEYWELL OR LITTON ADIRU) ALL

. 034A 28482 ...... LANDING GEAR-NOSE LANDING GEAR ........... WHEELS-REMOVE RUBBING STRIPS ALL

. 034B 28495 ...... NAVIGATION - MMR - REMOVE COLLINS MMR ........... PROVIDING ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION (PREVIOUS SPEC.) OO-SSF

CCM 1.00.8501 DEC 2002 PAGE 15

CCM ALL

CCM MSN 1068

CCM MSN 1145

CCM ALL

CCM MSN 1068

CCM MSN 1145

CCM ALL

CCM MSN 1068

CCM MSN 1145

CCM ALL

CCM MSN 1068

CCM MSN 1145

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1068 F-GTFM 1145 F-GYJM

CCM 2.00.70 01 MAR 2003 PAGE : CRT001

318/319/320/321 FCOM VOL. 2 FLIGHT PREPARATION HIGHLIGHTS REV033

2 01 00 001 001 REV033

- TECHNICAL AMENDMENT 1)Table of content is updated.

2 01 30 003 200 REV033 CODE 0033

- TECHNICAL AMENDMENT 1)Procedures for APU start/shutdown during refueling are moved to FCOM 2.01.30 p 10a.

2 01 30 007 100 REV033 M:20024

- TECHNICAL AMENDMENT 1)Procedures for APU start/shutdown during defueling are moved to FCOM 2.01.30 p 10a.

2 01 30 008 100 REV033 20024

- TECHNICAL AMENDMENT 1)Procedures for APU start/shutdown during refueling are moved to FCOM 2.01.30 p 10a.

2 01 30 010A 001 REV033

- TECHNICAL AMENDMENT 1)The policy on APU operation during refueling/defueling is modified to allow APU start attempt and shutdown during refueling/defueling. However : -no start attempt is authorized following an automatic shutdown or a failed start -a manual APU shutdown is requested in the event of a fuel spill during refueling/defueling.

2 01 30 011 100 REV033 MOD:20024

- TECHNICAL AMENDMENT 1)Page modified to clarify use of MMIs.

2 01 30 011A 001 REV033

- TECHNICAL AMENDMENT 1)Page created to clarify use of MMIs.

2 01 30 012 100 REV033 20024

- INCORPORATION OF MOD 20024 - TECHNICAL AMENDMENT 1)Page created to clarify use of MMIs.

2 01 30 013 001 REV033 CODE 0029

- TECHNICAL AMENDMENT 1)Fuel quantities units are added. 2)Table values are updated.

2 01 30 014 001 REV033 CODE 0029

01 MAR 2003 CCM 2.00.75 PAGE 1

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- 1)Fuel quantities units are added. 2)Table values are updated.

2 01 30 015 001 REV033 CODE 0029

2 01 30 016 001 REV033 CODE 0029

2 01 30 017 001 REV033 CODE 0029

2 01 30 018 001 REV033 CODE 0029

2 01 30 019 001 REV033 CODE 0029

2 01 30 020 100 REV033 CODE 0031

- TECHNICAL AMENDMENT 1)Fuel quantities units are added.

2 01 30 021 100 REV033 CODE 0031

- INCORPORATION OF MOD 20024 - TECHNICAL AMENDMENT 1)Fuel quantities units are added.

2 02 14 008 100 REV033 22013=24105

- TECHNICAL AMENDMENT 1)Update of minimum speeds check.

2 02 20 008 100 REV033 22013=24105

- TECHNICAL AMENDMENT 1)To replace the check of V2 only, by the check of all speeds versus minimum speeds (VMC and VMU). To replace the check of all speeds versus minimum speeds (VMC and VMU) by the check of V2 only versus VMU.

2 03 10 001 001 REV026 CODE 0081

2 03 20 001 001 REV033

01 MAR 2003 CCM 2.00.75 PAGE 2

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- 1)Removal of the recommendations for the use of the autobrake system. Refer to FCOM 3.03 S.O.P.

2 04 10 002 100 REV033 22013=24105

- TECHNICAL AMENDMENT 1)To clarify the conditions of use of the performance corrections in the CAUTION note.

2 05 70 001 135 REV033 CODE 0093/56-5-B5/B6

- INCORPORATION OF MOD 25530 - INCORPORATION OF MOD 25800 - INCORPORATION OF MOD 27727 - VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)To provide fuel tankering data for A319-111/-112.

2 05 70 002 135 REV033 CODE 0093/56-5-B5/B6

2 05 70 003 135 REV033 CODE 0093/56-5-B5/B6

2 05 70 004 135 REV033 CODE 0093/56-5-B5/B6

2 05 70 005 135 REV033 CODE 0093/56-5-B5/B6

2 05 70 006 135 REV033 CODE 0093/56-5-B5/B6

- INCORPORATION OF MOD 25530 - INCORPORATION OF MOD 25800 - INCORPORATION OF MOD 27727

01 MAR 2003 CCM 2.00.75 PAGE 3

2 05 70 006 135 REV033 CODE 0093/56-5-B5/B6

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)To provide fuel tankering data for A319-111/-112.

2 05 70 007 135 REV033 CODE 0093/56-5-B5/B6

2 05 70 008 135 REV033 CODE 0093/56-5-B5/B6

01 MAR 2003 CCM 2.00.75 PAGE 4

318/319/320/321 FCOM VOL.2 (FLIGHT PREPARATION ) -REV 033 LIST OF EFFECTIVE PAGES (LEP) -

2 00 00 001 001 REV021 CONTENTS ALL

2 00 10 001 001 REV031 ORGANIZATION OF THE MANUAL ALL 2 00 10 002 001 REV021 ORGANIZATION OF THE MANUAL

2 00 10 005 001 REV021 ORGANIZATION OF THE MANUAL ALL

2 00 30 001 001 REV028 LIST OF NORMAL REVISIONS ALL 2 00 30 002 001 REV032 LIST OF NORMAL REVISIONS

2 00 35 001 001 REV022 RECORD OF TEMPORARY REVISION ALL

R 2 00 36 001 001 REV033 LIST OF EFFECTIVE TEMPO.REVI ALL

R 2 00 70 001 001 REV033 CROSS REFERENCE TABLE ALL

R 2 00 75 001 001 REV033 HIGHLIGHTS ALL

R 2 00 80 001 001 REV033 LIST OF EFFECTIVE PAGES ALL

R 2 00 85 001 001 REV033 LIST OF MODIFICATIONS ALL

R 2 01 00 001 001 REV033 ALL

2 01 10 001 001 REV031 ALL

2 01 20 001 100 REV021 21103 1145 2 01 20 002 230 REV028 CODE 0061

2 01 20 001 100 REV021 21103 1068 2 01 20 002 303 REV029 CODE 0063

2 01 20 002A 001 REV029 CODE 0065 ALL

2 01 20 003 100 REV020 MOD:21329 ALL 2 01 20 004 100 REV026 M:23320

2 01 20 005 100 REV026 M:23320 ALL 2 01 20 006 100 REV026 M:23320

2 01 30 001 200 REV023 M: 20024+20167 ALL 2 01 30 002 200 REV020 MOD:20024+20164

R 2 01 30 003 200 REV033 CODE 0033 ALLR 2 01 30 004 100 REV028 M:20164

2 01 30 005 100 REV020 MOD:20024 ALL 2 01 30 006 001 REV021

01 MAR 2003 CCM 2.00.80 PAGE 01

R 2 01 30 007 100 REV033 M:20024 ALLR 2 01 30 008 100 REV033 20024

2 01 30 009 100 REV021 MOD:20024 ALL 2 01 30 010 200 REV024 CODE 0024

R 2 01 30 010A 001 REV033 ALL

N 2 01 30 011 100 REV033 MOD:20024 ALL

N 2 01 30 011A 001 REV033 ALL

N 2 01 30 012 100 REV033 20024 ALL

N 2 01 30 021 100 REV033 CODE 0031 ALL

2 01 40 001 001 REV028 ALL 2 01 40 002 230 REV028 M:20268+24105

2 01 40 003 210 REV028 MOD:20268+24105 ALL 2 01 40 004 230 REV030 MOD 20268+24105

2 01 40 005 230 REV030 MOD 20268+24105 ALL 2 01 40 006 001 REV030

2 02 00 001 100 REV025 M:22013 OR 24105 ALL 2 02 00 002 001 REV022

2 02 05 001 001 REV022 ALL

2 02 10 001 001 REV022 ALL 2 02 10 002 100 REV025 M:22013 OR 24105

2 02 10 003 100 REV025 CODE 0011 ALL 2 02 10 004 100 REV025 M:22013 OR 24105

2 02 10 005 100 REV025 M:22013=24105 ALL 2 02 10 006 110 REV026 M:24105

2 02 12 001 110 REV025 M:24105 ALL 2 02 12 002 040 REV025 CFM 56-5-B6

2 02 12 003 110 REV025 M:24105 ALL 2 02 12 004 040 REV025 CFM 56-5-B6

2 02 12 005 040 REV022 CFM 56-5-B6 ALL 2 02 12 006 100 REV022 M:22013 OR 24105

01 MAR 2003 CCM 2.00.80 PAGE 02

2 02 14 001 040 REV022 CFM 56-5-B6 ALL 2 02 14 002 100 REV031 22013=24105

2 02 14 003 110 REV025 M:24105 ALL 2 02 14 004 050 REV030 CFM 56-5-B6

2 02 14 005 110 REV025 M:24105 ALL 2 02 14 006 050 REV030 CFM 56-5-B6

R 2 02 14 007 050 REV031 CFM 56-5-B6 ALLR 2 02 14 008 100 REV033 22013=24105

2 02 16 001 001 REV022 ALL 2 02 16 002 100 REV023 M:22013 OR 24105

2 02 16 003 100 REV025 CODE 0011 ALL 2 02 16 004 100 REV025 M:22013 OR 24105

2 02 16 005 100 REV025 M:22013=24105 ALL 2 02 16 006 105 REV025 M:24105

2 02 18 001 100 REV025 M:22013 OR 24105 ALL 2 02 18 002 100 REV025 M:24105

2 02 18 003 045 REV025 CFM 56-5-B6 ALL 2 02 18 004 100 REV025 M:24105

2 02 18 005 045 REV025 CFM 56-5-B6 ALL 2 02 18 006 045 REV022 CFM 56-5-B6

2 02 18 007 100 REV022 M:22013 OR 24105 ALL

2 02 20 001 050 REV022 CFM 56-5-B6 ALL 2 02 20 002 100 REV022 M:22013 OR 24105

2 02 20 003 100 REV025 M:24105 ALL 2 02 20 004 050 REV030 CFM 56-5-B6

2 02 20 005 100 REV025 M:24105 ALL 2 02 20 006 050 REV030 CFM 56-5-B6

R 2 02 20 007 050 REV031 CFM 56-5-B6 ALLR 2 02 20 008 100 REV033 22013=24105

2 02 25 001 195 REV031 20268/CFM 56-5-B6 ALL 2 02 25 002 165 REV022 M:20268 CFM 56-5-B6

2 02 25 003 165 REV022 M:20268 CFM 56-5-B6 ALL 2 02 25 004 160 REV022 M:20268 CFM 56-5-B6

2 02 40 001 100 REV031 22013=24105=(MXA+24105) ALL 2 02 40 002 110 REV021 M:24105

2 02 40 003 150 REV025 M:20268 CFM 56-5-B6 ALL 2 02 40 004 185 REV025 M:20268/CFM 56-5-B6

01 MAR 2003 CCM 2.00.80 PAGE 03

2 02 40 005 185 REV025 M:20268/CFM 56-5-B6 ALL 2 02 40 006 185 REV025 M:20268/CFM 56-5-B6

2 02 40 009 185 REV025 M:20268/CFM 56-5-B6 ALL 2 02 40 010 001 REV020

2 02 40 013 185 REV025 M:20268/CFM 56-5-B6 ALL 2 02 40 014 001 REV020

2 02 50 001 001 REV032 ALL 2 02 50 002 195 REV022 MOD 20268 CFM 56-5-B6

2 02 50 003 195 REV022 MOD 20268 CFM 56-5-B6 ALL 2 02 50 004 195 REV022 MOD 20268 CFM 56-5-B6

2 02 50 005 195 REV022 MOD 20268 CFM 56-5-B6 ALL 2 02 50 006 195 REV022 MOD 20268 CFM 56-5-B6

2 02 50 007 195 REV022 MOD:20268 CFM 56-5-B6 ALL

2 03 00 001 001 REV031 ALL

2 03 10 001 001 REV026 CODE 0081 ALL 2 03 10 002 001 REV026

2 03 10 003 150 REV031 20268 CFM 56-5-B6 ALL 2 03 10 004 150 REV031 20268 CFM 56-5-B6

2 03 10 005 150 REV031 M:20268/CFM 56-5-B6 ALL 2 03 10 006 001 REV032

R 2 03 20 001 001 REV033 ALLR 2 03 20 002 155 REV031 20268/CFM 56-5-B6

2 04 00 001 001 REV028 ALL 2 04 00 002 001 REV025

R 2 04 10 001 001 REV032 ALLR 2 04 10 002 100 REV033 22013=24105

2 04 10 002A 100 REV030 22013=24105 ALL

2 04 10 003 190 REV028 20268/CFM 56-5-B6 ALL 2 04 10 004 190 REV028 20268/CFM 56-5-B6

2 04 10 005 190 REV026 MOD:20268 CFM 56-5-B6 ALL 2 04 10 006 190 REV026 MOD:20268 CFM 56-5-B6

2 04 10 007 190 REV026 MOD:20268 CFM 56-5-B6 ALL 2 04 10 008 190 REV026 M:20268/CFM 56-5-B6

2 04 10 009 190 REV026 MOD:20268 CFM 56-5-B6 ALL 2 04 10 010 001 REV022

01 MAR 2003 CCM 2.00.80 PAGE 04

2 04 10 011 001 REV021 ALL 2 04 10 012 001 REV025

2 04 10 013 001 REV021 ALL 2 04 10 014 140 REV026 M:20268/CFM 56-5-B6

2 04 10 015 140 REV026 M:20268 CFM 56-5-B6 ALL

2 04 15 001 001 REV020 ALL

2 04 20 001 001 REV021 ALL 2 04 20 002 001 REV020

2 04 20 003 001 REV027 ALL 2 04 20 004 001 REV024

2 04 20 005 001 REV029 ALL 2 04 20 006 235 REV027 M:24105+25800/56-5-B5/B6/B7

2 04 20 007 220 REV027 CODE 0023/CFM 56-5-B5/B6 ALL 2 04 20 008 110 REV023 MOD:24105

2 04 25 001 100 REV030 M:22013=24105=28160 ALL 2 04 25 002 100 REV020 M:22013=24105=28160

2 04 25 003 035 REV023 CODE 0015 ALL 2 04 25 004 050 REV021 CFM 56-5-B5/B6

2 04 25 005 130 REV023 M:20268 CFM 56-5-B5/B6 OR L ALL 2 04 25 006 135 REV027 M:25800/56-5-B5/B6

2 04 25 007 220 REV029 CODE 0023/CFM 56-5-B5/6 ALL 2 04 25 008 220 REV029 CODE 0023/CFM 56-5-B5/6

2 04 25 011 150 REV023 M:20268 CFM 56-5-B5/B6 ALL 2 04 25 012 145 REV031 20268 CFM 56-5-B5/B6

2 04 35 001 001 REV020 ALL 2 04 35 002 001 REV021

2 04 40 001 001 REV025 ALL 2 04 40 002 001 REV020

2 04 40 003 001 REV021 ALL 2 04 40 004 001 REV020

2 04 40 005 001 REV021 ALL 2 04 40 006 001 REV025

2 04 40 007 001 REV025 ALL 2 04 40 008 001 REV025

2 04 40 009 110 REV031 26249 ALL 2 04 40 010 110 REV030 26017/CFM ALL

2 04 40 010A 010 REV031 CFM ALL ALL

01 MAR 2003 CCM 2.00.80 PAGE 05

2 04 40 010B 100 REV031 24105 ALL

2 04 40 011 240 REV031 CODE 0023/CFM 56-5-B5/B6 ALL 2 04 40 012 140 REV027 CODE 0018 CFM 56-5-B5/B6

2 04 40 013 140 REV027 CODE 0018 CFM 56-5-B5/B6 ALL 2 04 40 014 140 REV027 CODE 0018 CFM 56-5-B5/B6

2 04 45 001 025 REV023 CFM 56-5-B1/B2/B3/B4/B5/B6 ALL 2 04 45 002 025 REV023 CFM 56-5-B1/B2/B3/B4/B5/B6

2 04 50 001 001 REV029 ALL 2 04 50 002 105 REV030 23779

2 04 50 003 001 REV027 ALL

2 04 60 001 001 REV030 ALL

2 05 00 001 001 REV021 ALL

2 05 10 001 120 REV024 M:25800/56-5-B ALL 2 05 10 002 103 REV021 M:24105

2 05 10 003 001 REV020 ALL 2 05 10 004 001 REV021

2 05 15 001 001 REV020 ALL 2 05 15 002 001 REV021

2 05 15 003 001 REV020 ALL 2 05 15 004 001 REV022

2 05 15 009 220 REV031 CODE 0023/CFM 56-5-B5/6 ALL

2 05 20 001 220 REV031 CODE 0023/CFM 56-5-B5/6 ALL 2 05 20 002 220 REV031 CODE 0023/CFM 56-5-B5/B6/T=L

2 05 20 003 120 REV021 MOD 24105 ALL

2 05 30 001 120 REV024 M:25800/56-5-B ALL 2 05 30 002 220 REV027 CODE:0023/56-5-B5/B6

2 05 30 003 220 REV027 CODE:0023/56-5-B5/B6 ALL 2 05 30 004 220 REV027 CODE:0023/56-5-B5/B6

01 MAR 2003 CCM 2.00.80 PAGE 06

2 05 30 023 220 REV027 CODE 0023/CFM 56-5-B5/B6 ALL 2 05 30 024 220 REV027 CODE 0023/CFM 56-5-B5/B6

2 05 40 001 235 REV027 M:24105+25800/CFM B5/B6/B7 ALL 2 05 40 002 220 REV027 CODE 0023/CFM 56-5-B5/B6

2 05 50 001 235 REV027 M:24105+25800/56-5-B5/B6/B7 ALL 2 05 50 002 220 REV027 CODE:0023/56-5-B5/B6

2 05 50 003 220 REV027 CODE:0023/56-5-B5/B6 ALL

2 05 60 001 001 REV021 ALL 2 05 60 002 001 REV023

2 05 60 003 150 REV021 MOD:24105 ALL 2 05 60 004 150 REV021 MOD:24105

N 2 05 70 001 135 REV033 CODE 0093/56-5-B5/B6 ALLN 2 05 70 002 135 REV033 CODE 0093/56-5-B5/B6

01 MAR 2003 CCM 2.00.80 PAGE 07

01 MAR 2003 CCM 2.00.80 PAGE 08

318/319/320/321 FCOM VOLUME : 2 FLIGHT PREPARATION LIST OF MOD/MP/SB AFFECTING THE MANUAL REVISION : 033

. 032A 20164 ...... FUEL - REFUEL/DEFUEL SYSTEM - ........... INSTALL A FUEL QUANTITY PRE-SELECTOR IN FLIGHT COMPARTMENT - ALL

. 032A 20167 ...... STRUCTURE - REINFORCE STRUCTURE TO ........... ALLOW MTOW 72T-MLW 63T-MZFW 59T DESIGN WEIGHTS ALL

. 032A 21103 ...... EQUIPMENT/FURNISHINGS - CARGO ........... COMPARTMENT - REARRANGE COMPARTMENT 4 INTO TWO ZONES - ALL

. 032A 21329 ...... DOORS-CARGO COMPT DOORS-MODIFY LOCKING ........... INDICATION ALL

. 032A 21897 ...... EQUIPMENT/FURNISHINGS-FWD CARGO COMPT- ........... INSTALL CLS AND FULL BULK COMPONENTS F-GTFM

. 032A 21898 ...... EQUIPMENT/FURNISHINGS-AFT CARGO COMPT- ........... INSTALL CLS AND FULL BULK COMPONENTS F-GTFM

. 032A 23124 ...... AIR CONDITIONING - PRESSURIZATION ........... CONTROL - IMPROVE CONTROLLER TO ENABLE USE OF EXTERNAL MODE ALL

. 032A 23320 ...... DOORS-CARGO COMPARTMENT DOOR HYDRAULIC ........... SYSTEM-INTRODUCE MODIFIED DOOR SELECTOR VALVE ALL

CCM 2.00.8501 MAR 2003 PAGE 1

. 032A 23779 ...... MINOR IMPROVEMENTS INTRODUCED FROM ........... A/C 508 (ST2) TO A/C 521 (ST2) ALL

. 032A 24373 ...... FUEL - TANK LEVEL SENSING - INTRODUCE ........... MODIFIED LOW FUEL PRESSURE WARNING CONTROL ALL

. 032A 24821 ...... EQUIPMENT/FURNISHINGS : AFT CARGO ........... COMPARTMENT PROVIDE ADDITIONAL CONTAINER CAPABILITY F-GTFM

. 032A 24946 ...... LANDING GEAR - MLG - MESSIER - ........... INTRODUCE BRAKES P/N C202253 ALL

. 032A 25141 ...... NACELLES/PYLONS-PYLON STRUCTURE- ........... ADAPT PRIMARY STRUCTURE TO A321-200 VERSION ALL

. 032A 25800 ...... POWER PLANT-GENERAL-INTRODUCE ........... CFM56-5B/P ALL

CCM 2.00.8501 MAR 2003 PAGE 2

. 032A 26249 ...... AIR CONDITIONING-FLOW CONTROL AND ........... INDICATING INTRODUCE MODIFIED AIR CONDITIONING FLOW CONTROL ALL

. 032A 26645 ...... AUTO-FLIGHT-FAC INTRODUCE FAC STD BAM ........... 0513 ALL

. 032A 27276 ...... FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ........... ELAC SOFTWARE GL80G ALL

. 032A 27727 ...... ENGINE -COMBUSTION SECTION- ........... INTRODUCE CFM56-5B DAC II PIP ENGINES ALL

. 032A 28164 ...... LANDING GEAR - WHEELS AND BRAKES - ........... INSTALL CARBON BRAKES TYPE SEPCARB III PLUS - MESSIER BUGATTI ALL

N 033 31395 ...... FLIGHT CONTROLS - ELAC SYSTEM - 27-1135 02 INTRODUCE ELAC STD L81 ALL

CCM 2.00.8501 MAR 2003 PAGE 3

CCM ALL

CCM MSN 1145

CCM MSN 1068

CCM ALL

1068 F-GTFM 1145 OO-SSF

CCM 3.00.70 01 MAR 2003 PAGE : CRT001

318/319/320/321 FCOM VOL. 3 FLIGHT OPERATIONS HIGHLIGHTS REV036

3 01 20 003 105 REV036 CODE 0358

- TECHNICAL AMENDMENT 1)Page updated to indicate the maximum wind speed for cargo door operation, in order to be consistent with the AMM : Cargo doors must not be opened, if the wind exceeds 40 knots, and must be closed before the wind exceeds 65 knots.

3 01 21 001 001 REV034

- TECHNICAL AMENDMENT 1)Page created to reflect the cabin pressure graphic, when the max operational altitude is 39800 feet.

3 01 22 001 002 REV036 STD=M:24105=US=(24105/US)

- TECHNICAL AMENDMENT 1)The FLIGHT MANAGEMENT FUNCTION item was moved to the next page, for repagination purposes.

3 01 22 002 105 REV036 CODE 0535

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - TECHNICAL AMENDMENT 1)The FLIGHT MANAGEMENT FUNCTION item, which was moved from the previous page, has been reviewed to be in line with the AFM. 2)The FMGS is also certified for navigation within PRNAV airspace. This is now reflected on this page.

3 01 22 002A 100 REV036 CODE 0538

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - TECHNICAL AMENDMENT 1)The USE OF NAV AND FINAL APP MODES FOR NON PRECISION APPROACH item has been reviewed to be in line with the AFM, and this page has been created for repagination purposes.

3 01 22 003 108 REV036 M:24105/CFM/IAE

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)No technical change. The sequence

01 MAR 2003 CCM 3.00.75 PAGE 1

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- number was changed to ensure the correct validation for all customers.

3 01 22 004 115 REV036 24105/CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)Additional information to precise the required VAPP in autoland. 2)Automatic landing in CAT1 or better conditions is moved to p 4a.

3 01 22 004A 100 REV036 24105=22013

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change. The sequence number has changed to ensure the correct validity for all customers.

3 01 32 001 040 REV035 STD OR (25951+32239)CFM ENG

3 01 34 001 100 REV036 CODE 0427

- TECHNICAL AMENDMENT 1)EGPWS limitations updated to be in accordance with the existing Flight Manual.

3 01 70 001 050 REV033 STD OR US/CFM 56-5-B

3 02 00 003 001 REV036

- TECHNICAL AMENDMENT 1)Page revised to reflect the correct pagination for the fire protection chapter.

3 02 00 007 001 REV036

- TECHNICAL AMENDMENT 1)The Table of Contents has been updated to reflect FCOM revisions and take into account various pagination changes.

3 02 00 009 025 REV030 CFM ALL

3 02 10 002 100 REV036 M:26017

- INCORPORATION OF MOD 26017 - TECHNICAL AMENDMENT 1)Introduction of the FWC E2 : With this standard, the DENG REV UNLOCKEDD message is only inhibited in flight phase 8. It may appear at takeoff.

01 MAR 2003 CCM 3.00.75 PAGE 2

3 02 10 003 001 REV036

- TECHNICAL AMENDMENT 1)PA call information revised for standardization purposes, and to be in accordance with training.

3 02 10 005 200 REV036 CODE 0396

- TECHNICAL AMENDMENT 1)Recommendations for rotation technique have been harmonized with the 3.02.10 P4 : At VR, rotate the aircraft to 12.5 deg. and, after lift off, follow Speed Reference System (SRS) orders.

3 02 21 004 001 REV036

- TECHNICAL AMENDMENT 1)Deletion of DFWD CRG HEATD from the inoperative system list, as forward cargo heating is not installed.

3 02 21 006 110 REV036 MOD:22561

- TECHNICAL AMENDMENT 1)Deletion of DFWD CRG HEATD, from the inoperative system list, as forward cargo heating is not installed. 2)LAV DET is removed from the DLAV+ GALLEY FAN FAULTD INOP SYS list because the ambient lavatory detectors (Mod 22561) are not lost in case of DLAV+GALLEY FAN FAULTD failure.

3 02 22 002 001 REV036

- TECHNICAL AMENDMENT 1)Addition of information to indicate that following a RUD TRV LIM SYS fault at slatsF extension, full rudder travel authority may be recovered, depending on the cause of the failure.

3 02 22 004 240 REV036 CODE 0589

- TECHNICAL AMENDMENT 1)Addition of information to indicate that following a FAC 1 + 2 FAULT at slatsF extension, full rudder travel authority is recovered.

3 02 23 001 001 REV036

- TECHNICAL AMENDMENT 1)Page revised to reflect the fact that, in case of continuous emission, the onside ACP must not be used for emission. A part of the note has been removed since the recommendation appeared not to be appropriate.

01 MAR 2003 CCM 3.00.75 PAGE 3

3 02 24 003 008 REV029 CFM ALL

3 02 24 005 108 REV032 CODE 0008/CFM ALL

3 02 24 006 205 REV036 M:21678+26377

- TECHNICAL AMENDMENT 1)Page revised to delete the DANTI ICE CAPT AOAD line, since this alarm is not triggered by an DAC ESS BUS FAULTD.

3 02 24 006 215 REV036 CODE:0554

- TECHNICAL AMENDMENT 1)Page revised to delete the DANTI ICE CAPT AOAD line, since this alarm is not triggered by an DAC ESS BUS FAULTD.

3 02 24 009 205 REV036 CODE:0555

- INCORPORATION OF MOD 27646 - TECHNICAL AMENDMENT 1)If installed, the CDLS (Cockpit Door Locking System) is inoperative, in case of a DC BUS 2 FAULT. The list of inoperative systems has been updated accordingly. 2)The sequence number was changed to ensure the correct page validation for all customers.

3 02 24 013 205 REV036 21678+24105

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers.

3 02 24 014 400 REV036 CODE 0426

- TECHNICAL AMENDMENT 1)SDCU2 has been removed from the list of INOP SYS displayed on the ECAM. 2)The inoperative system list has been updated to reflect the fact that, if installed, the Cockpit Door Locking System (CDLS) is inoperative, in case of a DC BUS 1+2 FAULT.

3 02 24 018 215 REV036 24105+25404 CFM=IAE

- TECHNICAL AMENDMENT 1)The sequence number was changed to correct validation problems on the page.

01 MAR 2003 CCM 3.00.75 PAGE 4

3 02 24 019 100 REV036 M:22013=24105=28160

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 28160 - TECHNICAL AMENDMENT 1)Modification of the DELEC ESS BUSES ON BATD note for improved technical understanding. 2)The sequence number has been changed to ensure the correct page validation for all customers.

3 02 24 026 110 REV030 M:24105=28160=30020

3 02 24 027 100 REV030 M:22013=24105=28160=30020

3 02 26 005 100 REV036 20057=20059=30067

- INCORPORATION OF MOD 20057 - INCORPORATION OF MOD 20059 - INCORPORATION OF MOD 30067 - TECHNICAL AMENDMENT 1)When both BLOWER and EXTRACT pushbuttons are in the OVRD position, a single pack may not be able to keep the cabin pressure. So, to avoid depressurization, it is asked to switch the BLOWER and the EXTRACT pushbuttons to the AUTO position before setting the single pack operation of the smoke procedure. If smoke still persists after the single - ADDITIONAL INFORMATION pack operation, once both packs are switched back ON, BLOWER and EXTRACT pushbuttons should be set to OVRD again.

3 02 26 007 300 REV036 CODE 0475

- TECHNICAL AMENDMENT 1)Page modified to reflect the exact aircraft definition : Aircraft not powered by IAE engines.

3 02 26 008 300 REV032 24105+25410+26017

3 02 26 010 001 REV036

- TECHNICAL AMENDMENT 1)The procedure has been harmonized with the Long Range family. In order to open the cockpit window (if necessary), the differential pressure should be zero (no residual pressure). Consequently, it is requested, at FL100 or MEA, to switch both packs OFF, set the pressure MODE SEL to MAN, and set the MAN V/S CTL to FULL UP.

01 MAR 2003 CCM 3.00.75 PAGE 5

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- 2)Fwd (aft) cargo smoke warning (if - ADDITIONAL INFORMATION previously contained on this page) has been moved to next page for standardization purposes.

3 02 26 011 400 REV036 CODE:0357

- TECHNICAL AMENDMENT 1)The DFWD (AFT) CARGO SMOKED warning has been moved from the previous page for standardization purposes. 2)The DLAV + CRG DET FAULTD warning has been moved to 3.02.26, page 12, for standardization purposes. 3)Introduction of the C/BsF panel location in the FWD (AFT) CARGO SMOKE procedure.

3 02 26 012 210 REV036 CODE 0530

- INCORPORATION OF MOD 20059 - INCORPORATION OF MOD 20067 - INCORPORATION OF MOD 20069 - TECHNICAL AMENDMENT 1)The DLAV + CRG DET FAULTD warning has been moved from page 11 to this page, for standardization purposes.

3 02 27 002 405 REV032 CODE 0415

3 02 27 008 410 REV036 24105+24511+25410+26017

- TECHNICAL AMENDMENT 1)Correction of the landing coefficient, when two SECs are affected, to be in accordance with the DLDG CONF-APPR SPD-LDG DIST CORRECTIONS FOR FAILURESD table (FCOM 3.02.80).

3 02 28 006 100 REV026 CODE 0359/CFM ALL

3 02 28 008 001 REV036

- TECHNICAL AMENDMENT 1)The Fuel leak section has been updated to : a) Indicate an additional method of detecting a fuel leak. b) Specify that, in case of leak from an engine, the crossfeed valve may be used, as required.

3 02 28 009 110 REV036 20024

- TECHNICAL AMENDMENT 1)The presentation of the procedure has been changed to clarify that, except in the case of leak from an engine, the crossfeed valve must remain closed.

01 MAR 2003 CCM 3.00.75 PAGE 6

3 02 28 010 100 REV036 20024

- TECHNICAL AMENDMENT 1)Procedure modified to prevent opening the crossfeed valve, in case of fuel leak.

3 02 29 001 105 REV036 M:22013=24105

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers.

3 02 29 011 310 REV034 CODE 0464

3 02 29 016 105 REV036 M:22013=24105

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers.

3 02 32 003 110 REV036 24645

- TECHNICAL AMENDMENT 1)Reference to DBRAKES SYS 1(2) FAULTD has been corrected to read : DBRAKES BSCU CH 1(2) FAULTD to reflect the actual ECAM wording.

3 02 32 010 110 REV036 M:24105=(22013+24044)

- INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change, the sequence number was changed to ensure correct page validation for all customers.

3 02 34 005 001 REV036

- TECHNICAL AMENDMENT 1)Addition of information to further enhance the ADR 1 + 2 + 3 FAULT paper procedure : Since the Rudder Travel Limiter is lost, DRUD WITH CARE ABV 160 KTD will be displayed on the ECAM. 2)Minor editorial change for improved technical understanding.

3 02 34 009 300 REV036 CODE 0198

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all

01 MAR 2003 CCM 3.00.75 PAGE 7

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

3 02 34 010 100 REV036 CODE:0382

- TECHNICAL AMENDMENT 1)Information moved to improve technical understanding.

3 02 34 012 001 REV036

- TECHNICAL AMENDMENT 1)Page modified to clarify that the LOC mode is available via the FCU LOC pushbutton, in case of a double Radio Altimeter fault.

3 02 34 015 100 REV036 M:26526

- TECHNICAL AMENDMENT 1)The heading has been shaded to indicate that this is not an ECAM procedure (for some batches of printed pages, the shading was inadvertently omitted).

3 02 36 003 001 REV036

- TECHNICAL AMENDMENT 1)Deletion of the note advising that the forward cargo isolation valve should be closed to minimize the rate at which the cabin altitude increase is removed, since forward cargo ventilation is not installed.

3 02 36 005 200 REV036 MOD:22562+24105

- TECHNICAL AMENDMENT 1)FCOM page amended to specify that the crossbleed valve must be opened, when wing anti-ice is used, and if one bleed is inoperative.

3 02 70 001 120 REV030 M:28307=27725/CFM 56-5-B

3 02 70 002 130 REV030 CODE:0046/56-5-B

3 02 70 003 035 REV024 CFM 56-5-B

3 02 70 004 150 REV028 CODE 0020

3 02 70 005 020 REV024 CFM ALL

3 02 70 006 010 REV026 CFM ALL

01 MAR 2003 CCM 3.00.75 PAGE 8

3 02 70 006 010 REV026 CFM ALL

3 02 70 007 020 REV032 CFM

3 02 70 008 010 REV032 CFM

3 02 70 009 020 REV030 CFM ALL

3 02 70 010 110 REV029 CODE 0145/CFM 56-5-B

3 02 70 011 035 REV032 CFM ALL

3 02 70 016 230 REV034 CODE 0312/CFM ALL

3 02 70 018 020 REV024 CODE 0361 CFM ALL

3 02 70 019 030 REV024 CFM ALL

3 02 70 022 130 REV024 CODE 0106

3 02 70 023 120 REV033 CODE 0314/CFM ALL

3 02 70 024 120 REV024 M:24035=24160=24189 CFM ALL

3 02 70 025 020 REV026 CFM ALL

3 02 70 026 020 REV024 CFM ALL

3 02 80 003 001 REV036

- TECHNICAL AMENDMENT 1)The DDITCHINGD procedure has been revised to recommend that bleed sources be switched OFF, before setting the DITCHING pushbutton ON, in order to be in accordance with the DON GROUND DE-ICINGD procedure. 2)Rewording of the ditching pushbutton

01 MAR 2003 CCM 3.00.75 PAGE 9

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- description to be in line with the FCOM 1.21.20 p 7.

3 02 80 005 100 REV036 26526

- TECHNICAL AMENDMENT 1)Procedure enhanced to specify that, if the engines are not running, the landing gear is extended by gravity.

3 02 80 016 025 REV027 CFM ALL

3 02 80 018 302 REV036 23208+24077+24105

- TECHNICAL AMENDMENT 1)Addition of the Ddelta VREFD and landing coefficient when there is a DREVERSE UNLOCKEDD warning, and when the landing is performed in CONF 3.

3 02 90 005 001 REV036

- TECHNICAL AMENDMENT 1)Page revised to reflect the fact that the described procedure is applicable to aircraft fitted with the slide, not the slide-raft. 2)Addition of a note to clarify that doors, equipped with slides, should be given priority for use in case of evacuation.

3 03 04 005 001 REV036

- TECHNICAL AMENDMENT 1)Due to several cases of activation of autobrake at taxi, the crew should check that the SPEED BRAKE lever is retracted and disarmed. 2)Addition of information to warn pilots that, before turning ON the APU bleed, they should check with the ground crew and should also check the ECAM BLEED page to ensure that HP ground air unit is not connected.

3 03 04 007 110 REV030 M:22013=24105=24701/CFM ALL

3 03 05 003 105 REV036 22199=24105

- INCORPORATION OF MOD 22199 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)Page created to remove the DWing leading edge ventilation intakeD item, as it is not applicable.

3 03 06 002 100 REV036 CODE 0435

- INCORPORATION OF MOD 21946 - TECHNICAL AMENDMENT 1)No technical change. The sequence

01 MAR 2003 CCM 3.00.75 PAGE 10

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- number was changed to ensure the correct page validation for all customers.

3 03 06 006 100 REV036 MOD 22031=25440

- INCORPORATION OF MOD 22031 - INCORPORATION OF MOD 25440 - TECHNICAL AMENDMENT 1)A note has been added to highlight the fact that the Flight Number should be exactly entered on the MCDU INIT page, with the same syntax as the one shown in the ICAO flight plan. Indeed, an inexactly entered flight number can cause the communication and identification with the ATC to fail.

3 03 07 002 001 REV036

- TECHNICAL AMENDMENT 1)The check of the red circle on the window handle has been removed, since this feature is not necessarily installed on all A320 family aircraft.

3 03 08 002 020 REV032 CFM ALL

3 03 09 001 020 REV029 CFM ALL

3 03 09 002 025 REV030 CFM ALL

3 03 10 006 105 REV036 24105

- TECHNICAL AMENDMENT 1)The schematic and wording have been clarified to reflect that the 2 meters of reference, are before the runway edge.

3 03 11 001 040 REV024 CODE:0187

- DELETION OF MOD 25530 - VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE

3 03 11 001 040 REV036 CODE:0504/CFM

- TECHNICAL AMENDMENT 1)The benefits of bleed selections for takeoff are clarified and standardized to be in accordance with the A330 SOP.

3 03 12 002 120 REV025 CODE 0189 CFM ALL

3 03 12 003 001 REV036

- TECHNICAL AMENDMENT 1)Modification of the pilot rotation

01 MAR 2003 CCM 3.00.75 PAGE 11

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- technique to achieve a continuous rotation rate. The aim is to avoid pitch PIO (Pilot Induced Oscillations) and obtain a similar aircraft rotation for all the Airbus fly-by-wire aircraft family. Recommendations regarding lateral inputs on ground and during the rotation have also been amended.

3 03 13 001 001 REV036

- TECHNICAL AMENDMENT 1)FCOM page amended to clarify that icing conditions may be expected, when temperatures are at (or below) 10 deg. C, in order to be in accordance with the Flight Manual.

3 03 15 002 001 REV036

- TECHNICAL AMENDMENT 1)Page modified to include an additional recommendation, in case the cockpit oxygen mask has been used. The mask should be stowed, as per the FCOM 1.35.20, in order to avoid potential risk of oxygen depletion.

3 03 16 002 001 REV036

- TECHNICAL AMENDMENT 1)Page modified to reflect that the correct QRH page reference is 2.31, not 2.41.

3 03 17 003 100 REV036 CODE:0189

- TECHNICAL AMENDMENT 1)The recommendation concerning the use of the EGPWS TERR on ND display has been modified : Depending on operational conditions, the EGPWS TERR display or the weather radar display may be selected on both sides. However, if both weather radar and EGPWS TERR displays are needed, it is recommended to select the weather radar display on the PF side and the - ADDITIONAL INFORMATION EGPWS TERR display on the PNF side.

3 03 18 001 200 REV027 M:26018+26398

3 03 18 002 210 REV036 CODE:0578

- TECHNICAL AMENDMENT 1)The legends of the NAV accuracy table have been clarified for improved technical understanding.

3 03 18 003 100 REV036 CODE:0511

01 MAR 2003 CCM 3.00.75 PAGE 12

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- 1)Page revised to introduce ALAR program recommendations.

3 03 18 006 001 REV036

- TECHNICAL AMENDMENT 1)Information has been moved to the FCOM 3.03.18, page 7, for pagination purposes.

3 03 18 007 001 REV036

- TECHNICAL AMENDMENT 1)Information has been moved from the previous page, and some information has been moved to the next page, for pagination purposes. 2)Page modified to add the recommendations given in OIT/FOT 999.0108/02/BB. After landing gear extension, additional guidelines are given to prevent undue flight crew action, in case of brakesF residual - ADDITIONAL INFORMATION pressure. Particularly, the antiskid and nosewheel steering must be kept ON.

3 03 18 008 001 REV036

- TECHNICAL AMENDMENT 1)Information has been moved from the previous page, for pagination purposes.

3 03 18 009 001 REV036

- TECHNICAL AMENDMENT 1)Information has been moved from the previous page, for pagination purposes.

3 03 19 001 105 REV036 CODE 0535

- INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 30631 - TECHNICAL AMENDMENT 1)DNON RNAVD approaches has been included in the title. RNAV approaches are described further in this chapter. 2)Additional references to Airbus operational documentation, regarding NAV database validation, is included. 3)Now, it is requested to check the lateral and vertical F-PLN against the IAP approach, before starting the approach. - ADDITIONAL INFORMATION 4)New indications are given on how to deal with a GPS PRIMARY loss, or a FM/GPS POS DISAGREE caution.

3 03 19 002 001 REV036

- TECHNICAL AMENDMENT 1)Addition of information on approach

01 MAR 2003 CCM 3.00.75 PAGE 13

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- guidance for RNAV approaches.

3 03 19 003 120 REV036 CODE 0543

- INCORPORATION OF MOD 24105 - INCORPORATION OF MOD 25294 - TECHNICAL AMENDMENT 1)Addition of information on approach guidance for RNAV approaches.

3 03 19 004 105 REV036 CODE 0546

- INCORPORATION OF MOD 26398 - TECHNICAL AMENDMENT 1)Page created to include information that was moved from a previous page, for repagination purposes. 2)Introduction of the ALAR program recommendations.

3 03 19 005 001 REV036

- TECHNICAL AMENDMENT 1)Information was moved from a previous page, for repagination purposes.

3 03 19 006 200 REV036 CODE 0549

- INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28244 - INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 - TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)The legends of the NAV accuracy table have been clarified for improved technical understanding. 3)A note is added to advise that, if during an overlay approach to a conventional radio procedure, the raw data indicates that the managed guidance is unsatisfactory, the crew - ADDITIONAL INFORMATION must revert to selected guidance.

3 03 19 007 100 REV036 CODE 0538

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631

3 03 19 007 100 REV032 CODE 0042

- DELETION OF MOD 24064 - DELETION OF MOD 24065 - DELETION OF MOD 24066 - DELETION OF MOD 24067

01 MAR 2003 CCM 3.00.75 PAGE 14

3 03 19 007 100 REV036 CODE 0538

- TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)Specific procedure lines for RNAV approaches have been added to ensure the required navigation accuracy for the approach. It is also reminded that the RNAV approaches without GPS are subject to specific operational approval.

3 03 19 008 001 REV036

- TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)Page modified to add the recommendations given in OIT/FOT 999.0108/02/BB. After landing gear extension, additional guidelines are given to prevent undue flight crew action in case of brakes residual pressure. Particularly, the antiskid and nose wheel steering must be kept - ADDITIONAL INFORMATION ON.

3 03 19 009 001 REV036 STD=M:24105

- INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)New indications for the POSITION and FLIGHT PATH monitoring and adjusting, regarding the RNAV approaches and approaches overlay to a conventional radio navaid procedure.

3 03 19 010 001 REV036

- TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes.

3 03 19 011 100 REV036 M:24064=24065=24066=24067

- INCORPORATION OF MOD 24064 - INCORPORATION OF MOD 24065 - INCORPORATION OF MOD 24066 - INCORPORATION OF MOD 24067 - TECHNICAL AMENDMENT 1)Information was moved from page 7 for repagination purposes.

3 03 19 012 100 REV036 M:23742

- INCORPORATION OF MOD 23742 - TECHNICAL AMENDMENT 1)Information was moved from page 8 for repagination purposes.

01 MAR 2003 CCM 3.00.75 PAGE 15

3 03 19 013 001 REV036

- TECHNICAL AMENDMENT 1)Information was moved from page 9 for repagination purposes.

3 03 20 001 100 REV035 26398

3 03 22 004 105 REV036 M:24105

- TECHNICAL AMENDMENT 1)Page modified to include attitude monitoring during flare. Attitude monitoring is done by the PNF and its aim is to avoid tailstrike, or wingtip or engine scrape during the flare maneuver.

3 03 23 001 110 REV036 25863

- TECHNICAL AMENDMENT 1)Information has been moved to the next page for pagination and standardization purposes.

3 03 23 002 001 REV036

- TECHNICAL AMENDMENT 1)- Information has been moved from page 1. - Addition of a conditional procedure, to manually disengage GO-Around SRS Mode by pulling the FCU ALT knob, should the target speed not automatically increase when climbing through GO Acceleration Altitude.

3 03 23 004 100 REV036 M:25863

- INCORPORATION OF MOD 25863 - TECHNICAL AMENDMENT 1)Blank page moved from previous page to this page for pagination and standardization purposes.

3 03 25 001 020 REV035 CODE 0186/CFM ALL

3 03 25 003 170 REV035 22013=23119/CFM ALL

3 04 00 001 203 REV036 CODE 0501

- TECHNICAL AMENDMENT 1)The title of the SUPPLEMENTARY TECHNIQUESF FLIGHT CONTROLS chapter has been modified to indicate that it also contains flying techniques. 2)AIRCRAFT TRIMMING is moved to page 12.

01 MAR 2003 CCM 3.00.75 PAGE 16

3 04 10 002 115 REV028 M:24105/CFM ALL=IAE ALL

3 04 23 001 001 REV036

- TECHNICAL AMENDMENT 1)Simplification of the note concerning noisy frequencies.

3 04 23 001A 001 REV036

- TECHNICAL AMENDMENT 1)Page created to harmonize pagination changes.

3 04 24 004 103 REV036 24771

- INCORPORATION OF MOD 24771 - TECHNICAL AMENDMENT

1)Addition of a CIDS reset procedure in case of uncommanded EVAC horn actuation. 2)Some information has been moved to the next page, to accommodate additional information on page 4, and ensure the correct page validation for all customers.

3 04 24 005 101 REV036 24613=22013+24613

- INCORPORATION OF MOD 24613 - TECHNICAL AMENDMENT 1)Some information has been moved from page 4 to this page, and some information has been moved to page 6, to accommodate additional information page 4 and ensure the correct page validation for all customers.

3 04 24 006 001 REV036

- TECHNICAL AMENDMENT 1)Page created to accommodate additional information on page 4 and ensure the correct page validation for all customers.

3 04 27 002 001 REV036

- TECHNICAL AMENDMENT 1)Sidestick position indication on PFD may be monitored by the crew, not only when in crosswind condition. References to crosswind conditions have consequently been removed from our recommendations regarding the use of the sidestick position indication. 2)A crossreference to the SOP 3.03.12 has been added, since this chapter contains some additional information - ADDITIONAL INFORMATION on takeoff technique.

01 MAR 2003 CCM 3.00.75 PAGE 17

3 04 27 003 001 REV036

- TECHNICAL AMENDMENT 1)Recommendations regarding lateral inputs on ground and during the rotation have been amended : Lateral inputs on ground and during the rotation should be minimized to avoid spoiler extension. Spoiler deflection starts to become significant with more than one third sidestick deflection.

3 04 27 004 001 REV036

- TECHNICAL AMENDMENT 1)Recommendations for crosswind landing technique, have been harmonized with the SOP 3.03.22.

3 04 27 005 001 REV036

- TECHNICAL AMENDMENT 1)Introduction of recommendations, in case of bounce at landing. 2)Some text has been moved to page 6.

3 04 27 006 001 REV036

- TECHNICAL AMENDMENT 1)The DBACKUP CONTROLD chapter has been renamed DMECHANICAL BACKUPD for improved understanding of the meaning of this term. 2)Some text has been moved from page 5, and the illustration to page 7, to accomodate additional info on page 5.

3 04 27 007 001 REV036

- TECHNICAL AMENDMENT 1)Some text has been moved from page 6, and some to page 8, to accomodate additional info on page 5.

3 04 27 008 001 REV036

3 04 27 009 001 REV036

3 04 27 010 001 REV036

01 MAR 2003 CCM 3.00.75 PAGE 18

3 04 27 011 001 REV036

3 04 27 012 001 REV036

- TECHNICAL AMENDMENT 1)New page created : Some text has been moved from page 11, to accomodate info on page 5.

3 04 70 003 020 REV026 CFM ALL

3 04 70 005 100 REV029 CODE 0145/CFM ALL

3 04 70 006 020 REV033 CFM ALL

3 04 70 007 020 REV028 CFM ALL

3 04 70 008 007 REV030 CFM ALL

3 04 90 001 020 REV024 CFM ALL

3 04 90 002 020 REV035 CFM ALL

3 04 91 004 001 REV036

- TECHNICAL AMENDMENT 1)No technical change. Information has been moved to the next page for pagination purposes.

3 04 91 005 001 REV036

- TECHNICAL AMENDMENT 1)No technical change. Information has been moved from the previous page for pagination purposes.

3 04 91 007 001 REV036

- TECHNICAL AMENDMENT 1)Introduction of the Doutflow valve check ditchingD Temporary Revision : A recommendation has been added to check that no external air is supplied to the aircraft via the low or high pressure ground connectors, before

01 MAR 2003 CCM 3.00.75 PAGE 19

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- starting the de-icing procedure. 2)Minor editorial changes have been made to reflect the fact that the aircraft can be de-iced with the APU and the - ADDITIONAL INFORMATION engines running. 3)The note concerning the DITCHING pushbutton has been updated to reflect the fact that the avionic ventilation inlet valve is also closed.

3 04 91 008 001 REV036

- TECHNICAL AMENDMENT 1)Introduction of TR 734-1 : A recommendation has been added within the de-icing procedure, to check that the outflow valve is indicated open, after completion of this procedure. 2)The sequence number was changed to ensure the correct page validation for all customers.

3 04 92 001 001 REV036

- TECHNICAL AMENDMENT Page revised : 1)To indicate that pilots must check the version of F.O.V.E. installed on their PCs, not the version of each module, as previously stated. 2)For improved technical understanding and standardization.

3 04 92 002 001 REV036

- TECHNICAL AMENDMENT Page revised to indicate that : 1)Pilots must check the version of F.O.V.E. installed on their PCs, not the version of each module, as previously stated. 2)The DAircraft LoadingD module has been replaced by the DWeight and BalanceD module.

3 04 92 004 001 REV036

- TECHNICAL AMENDMENT Page revised to : 1)Replace the DAircraft LoadingD module by the DWeight and BalanceD module. 2)Introduce the description of the LPCFs Weight and Balance (W & B) module. 3)Delete the reference to the ECAM CG, as there is no ECAM CG on the A320 aircraft family.

3 04 92 005 001 REV036

- TECHNICAL AMENDMENT 1)Page created to introduce the description of the LPCFs Weight and Balance (W & B) module.

01 MAR 2003 CCM 3.00.75 PAGE 20

3 04 92 006 001 REV036

- TECHNICAL AMENDMENT 1)Page created to introduce the description of the LPCFs Weight and Balance (W & B) module.

3 05 35 001 100 REV036 M:22013=24105

- TECHNICAL AMENDMENT 1)In note 2, replace VLS by VREF for CONF FULL. VLS is for CONF 3.

01 MAR 2003 CCM 3.00.75 PAGE 21

318/319/320/321 FCOM VOL.3 (FLIGHT OPERATIONS ) -REV 036 LIST OF EFFECTIVE PAGES (LEP) -

3 00 00 001-2 001 REV024 CONTENT ALL

N 3 00 20 017 001 REV036 LIST OF CODES ALL

R 3 00 30 001 001 REV027 LIST OF NORMAL REVISION ALLR 3 00 30 002 001 REV036 LIST OF NORMAL REVISION

3 01 00 001 001 REV032 CONTENTS ALL 3 01 00 002 001 REV028 CONTENTS

3 01 10 001 105 REV024 M:24105 OR (24105 US) ALL

3 01 20 001 116 REV032 CODE 0140 ALL 3 01 20 002 209 REV029 M:24105+27276

01 MAR 2003 CCM 3.00.80 PAGE 01

3 01 20 005 105 REV027 MOD:24105 ALL 3 01 20 006 070 REV034 CFM 56-5-B6

3 01 20 007 100 REV031 M:24105 ALL 3 01 20 008 105 REV026 MOD:24105

3 01 20 009 020 REV025 V2530=V2533=B1/B2/B3 = 24105 ALL 3 01 20 010 105 REV025 M:22013 = 24105

3 01 21 001 001 REV034 ALL 3 01 21 002 001 REV024

N 3 01 22 001 002 REV036 STD=M:24105=US=(24105/US) ALLN 3 01 22 002 105 REV036 CODE 0535

N 3 01 22 002A 100 REV036 CODE 0538 ALL

N 3 01 22 003 108 REV036 M:24105/CFM/IAE ALLN 3 01 22 004 115 REV036 24105/CFM ALL

N 3 01 22 004A 100 REV036 24105=22013 ALL

3 01 24 001 001 REV024 ALL 3 01 24 002 001 REV024

3 01 27 001 001 REV024 ALL 3 01 27 002 001 REV024

3 01 28 001 001 REV026 ALL 3 01 28 002 100 REV024 MOD:20024

3 01 29 001 001 REV024 ALL 3 01 29 002 001 REV024

3 01 32 001 040 REV035 STD OR (25951+32239)CFM ENG ALL

R 3 01 34 001 100 REV036 CODE 0427 ALL

3 01 35 001 105 REV024 CODE 0137 ALL

3 01 49 001 110 REV034 22562=(22562+25888+27609) ALL 3 01 49 002 230 REV033 CODE:0254

3 01 49 003 105 REV024 CODE 0223 ALL

3 01 70 001 050 REV033 STD OR US/CFM 56-5-B ALL 3 01 70 002 064 REV032 CFM 56-5-B6/B7

3 02 00 001 001 REV032 ALL 3 02 00 002 001 REV027

R 3 02 00 003 001 REV036 ALLR 3 02 00 004 001 REV028

3 02 00 005 001 REV026 ALL 3 02 00 006 100 REV035 22875

01 MAR 2003 CCM 3.00.80 PAGE 02

R 3 02 00 007 001 REV036 ALLR 3 02 00 008 001 REV024 CODE 0531

3 02 00 009 025 REV030 CFM ALL ALL 3 02 00 010 100 REV035 25529

3 02 01 001 001 REV024 ALL 3 02 01 002 001 REV030

3 02 01 003 001 REV033 ALL 3 02 01 004 001 REV032

N 3 02 10 001 001 REV024 ALLN 3 02 10 002 100 REV036 M:26017

R 3 02 10 005 200 REV036 CODE 0396 ALLR 3 02 10 006 100 REV030 M:23742

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3 02 21 001 001 REV028 ALL 3 02 21 002 320 REV035 26363+26792+28488

R 3 02 21 003 001 REV024 CODE 0032 ALLR 3 02 21 004 001 REV036

R 3 02 21 005 100 REV024 20059=30067 ALLR 3 02 21 006 110 REV036 MOD:22561

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3 02 21 013 110 REV029 M:21899 ALL 3 02 21 014 001 REV025 CODE 0089

R 3 02 22 001 100 REV035 26645=27846=28703=30439 ALLR 3 02 22 002 001 REV036

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01 MAR 2003 CCM 3.00.80 PAGE 03

3 02 24 001 002 REV034 STD=24105 ALL 3 02 24 002 100 REV031 CODE:0072

3 02 24 003 008 REV029 CFM ALL ALL 3 02 24 004 305 REV031 21678+24105+26017

N 3 02 24 005 108 REV032 CODE 0008/CFM ALL 1068N 3 02 24 006 205 REV036 M:21678+26377

N 3 02 24 005 108 REV032 CODE 0008/CFM ALL 1145N 3 02 24 006 215 REV036 CODE:0554

3 02 24 007 100 REV027 M:21678 ALL 3 02 24 008 400 REV032 CODE 0426

N 3 02 24 009 205 REV036 CODE:0555 ALLN 3 02 24 010 001 REV028

3 02 24 011 200 REV030 24105+26017 ALL 3 02 24 012 370 REV026 21678+24105+26017

N 3 02 24 013 205 REV036 21678+24105 ALLN 3 02 24 014 400 REV036 CODE 0426

N 3 02 24 017 250 REV033 CODE:0350 ALLN 3 02 24 018 215 REV036 24105+25404 CFM=IAE

N 3 02 24 019 100 REV036 M:22013=24105=28160 ALLN 3 02 24 020 210 REV033 MOD 21678+21706

3 02 24 021 100 REV035 21678 ALL 3 02 24 022 230 REV027 CODE 0476

3 02 24 023 310 REV031 M:21285+21678+25404/CFM ALL 3 02 24 024 200 REV032 CODE 0239

3 02 24 025 303 REV029 CODE 0552 ALL 3 02 24 026 110 REV030 M:24105=28160=30020

3 02 24 027 100 REV030 M:22013=24105=28160=30020 ALL 3 02 24 028 001 REV032

3 02 26 001 001 REV032 ALL 3 02 26 002 001 REV033

3 02 26 003 001 REV033 ALL 3 02 26 004 100 REV035 27498=31891

N 3 02 26 005 100 REV036 20057=20059=30067 ALLN 3 02 26 006 001 REV035

R 3 02 26 007 300 REV036 CODE 0475 ALLR 3 02 26 008 300 REV032 24105+25410+26017

N 3 02 26 009 001 REV032 ALLN 3 02 26 010 001 REV036

01 MAR 2003 CCM 3.00.80 PAGE 04

3 02 27 001 200 REV024 24612+26017 ALL 3 02 27 002 405 REV032 CODE 0415

3 02 27 003 110 REV028 CODE 0183 ALL 3 02 27 004 400 REV032 20024+24105+25410+26017

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R 3 02 27 007 220 REV027 CODE 0392 ALLR 3 02 27 008 410 REV036 24105+24511+25410+26017

3 02 27 009 100 REV026 MOD:26017 ALL 3 02 27 010 215 REV032 CODE 0229

3 02 27 011 110 REV031 25410 ALL 3 02 27 012 100 REV025 MOD:26017

3 02 27 013 300 REV028 24105+25410+26017 ALL 3 02 27 014 200 REV024 MOD 24105+26017

3 02 27 015 310 REV024 24105+25410+26017 ALL 3 02 27 016 240 REV033 M:21964+22087

3 02 27 017 110 REV025 26017=(25410+26017) ALL 3 02 27 018 001 REV024

3 02 27 019 001 REV024 ALL 3 02 27 020 200 REV028 CODE 0045

3 02 27 021 001 REV024 ALL 3 02 27 022 001 REV024

3 02 28 001 100 REV033 M:20024 ALL 3 02 28 002 002 REV033

3 02 28 003 100 REV028 MOD 20024 ALL 3 02 28 004 001 REV024

3 02 28 005 001 REV026 ALL 3 02 28 006 100 REV026 CODE 0359/CFM ALL

R 3 02 28 007 100 REV024 MOD 20024 ALLR 3 02 28 008 001 REV036

R 3 02 28 009 110 REV036 20024 ALLR 3 02 28 010 100 REV036 20024

N 3 02 29 001 105 REV036 M:22013=24105 ALLN 3 02 29 002 001 REV024

3 02 29 003 110 REV032 MOD:26017 ALL 3 02 29 004 001 REV024

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01 MAR 2003 CCM 3.00.80 PAGE 05

3 02 29 007 002 REV024 ALL 3 02 29 008 230 REV024 CODE 0355

3 02 29 009 001 REV024 ALL 3 02 29 010 001 REV024

3 02 29 011 310 REV034 CODE 0464 ALL 3 02 29 012 001 REV024

3 02 29 013 200 REV034 24105+26017 ALL 3 02 29 014 100 REV034 26017

N 3 02 29 015 100 REV033 26017 ALLN 3 02 29 016 105 REV036 M:22013=24105

3 02 30 001 100 REV030 25410=26017 ALL 3 02 30 002 001 REV024

3 02 30 003 001 REV027 ALL 3 02 30 004 001 REV024

3 02 30 005 100 REV025 MOD:22875 ALL 3 02 30 006 001 REV027

3 02 30 007 001 REV024 ALL 3 02 30 008 205 REV028 M:24105+26017

3 02 31 001 001 REV024 ALL 3 02 31 002 001 REV032

3 02 31 003 001 REV024 ALL 3 02 31 004 001 REV033

3 02 32 001 001 REV030 STD=31897=31896 ALL 3 02 32 002 001 REV034

R 3 02 32 003 110 REV036 24645 ALLR 3 02 32 004 002 REV033 STD=(20139+22129)

3 02 32 005 001 REV024 ALL 3 02 32 006 001 REV032

3 02 32 007 001 REV031 ALL 3 02 32 008 001 REV035

N 3 02 32 009 105 REV035 24105 ALLN 3 02 32 010 110 REV036 M:24105=(22013+24044)

3 02 32 011 001 REV033 STD=27979 ALL

3 02 34 003 100 REV033 26526 ALL 3 02 34 004 205 REV033 M:26017+26526

R 3 02 34 005 001 REV036 ALLR 3 02 34 006 105 REV033 26017=(25410+26017)

01 MAR 2003 CCM 3.00.80 PAGE 06

N 3 02 34 009 300 REV036 CODE 0198 ALLN 3 02 34 010 100 REV036 CODE:0382

R 3 02 34 011 100 REV033 MOD:26017 ALLR 3 02 34 012 001 REV036

3 02 34 013 105 REV035 CODE 0614 ALL 3 02 34 014 105 REV035 22769

R 3 02 34 015 100 REV036 M:26526 ALLR 3 02 34 016 100 REV025 M:26526

3 02 34 017 105 REV033 CODE:0205 ALL 3 02 34 018 100 REV035 26017

3 02 34 019 001 REV035 ALL 3 02 34 020 001 REV035

3 02 34 021 001 REV035 ALL 3 02 34 022 001 REV035

3 02 34 023 035 REV035 56-5-B5/B6/B7 ALL 3 02 34 024 035 REV035 56-5-B5/B6/B7

3 02 34 025 035 REV035 56-5-B5/B6/B7 ALL

3 02 36 001 001 REV024 ALL 3 02 36 002 001 REV034

R 3 02 36 003 001 REV036 ALLR 3 02 36 004 200 REV028 M:22562+24105

R 3 02 36 005 200 REV036 MOD:22562+24105 ALLR 3 02 36 006 001 REV024

3 02 36 007 100 REV025 M:24105 ALL

3 02 49 001 001 REV024 ALL

3 02 52 001 001 REV024 CODE 0188 ALL

3 02 70 001 120 REV030 M:28307=27725/CFM 56-5-B ALL 3 02 70 002 130 REV030 CODE:0046/56-5-B

3 02 70 003 035 REV024 CFM 56-5-B ALL 3 02 70 004 150 REV028 CODE 0020

3 02 70 007 020 REV032 CFM ALL 3 02 70 008 010 REV032 CFM

3 02 70 009 020 REV030 CFM ALL ALL 3 02 70 010 110 REV029 CODE 0145/CFM 56-5-B

01 MAR 2003 CCM 3.00.80 PAGE 07

3 02 70 011 035 REV032 CFM ALL ALL 3 02 70 012 200 REV030 M:25404+26017

3 02 70 013 100 REV033 MOD:25410 ALL 3 02 70 014 105 REV035 MOD 24105

3 02 70 015 040 REV035 CFM ENG:ALL ALL 3 02 70 016 230 REV034 CODE 0312/CFM ALL

3 02 70 017 220 REV026 CODE 0050 ALL 3 02 70 018 020 REV024 CODE 0361 CFM ALL

3 02 70 019 030 REV024 CFM ALL ALL 3 02 70 020 150 REV028 M:26017 CFM 56-5-B4/B5/B6/B7

3 02 70 021 020 REV034 CFM 56-5-A4/A5/B5/B6/B7 ALL 3 02 70 022 130 REV024 CODE 0106

3 02 70 023 120 REV033 CODE 0314/CFM ALL ALL 3 02 70 024 120 REV024 M:24035=24160=24189 CFM ALL

3 02 80 001 001 REV035 ALL 3 02 80 002 100 REV031 M:26526

R 3 02 80 003 001 REV036 ALLR 3 02 80 004 001 REV024

R 3 02 80 005 100 REV036 26526 ALLR 3 02 80 006 001 REV035

3 02 80 007 001 REV034 ALL 3 02 80 008 065 REV029 CODE:0109/T=L

3 02 80 009 001 REV025 ALL 3 02 80 010 001 REV034

3 02 80 010A 001 REV031 ALL

3 02 80 011 001 REV035 ALL

3 02 80 011A 001 REV034 ALL

3 02 80 012 001 REV034 ALL

3 02 80 013 001 REV030 ALL 3 02 80 014 001 REV033

3 02 80 015 100 REV032 MOD:22562 ALL 3 02 80 016 025 REV027 CFM ALL

N 3 02 80 017 110 REV035 24105 ALLN 3 02 80 018 302 REV036 23208+24077+24105

3 02 80 019 100 REV035 22249 ALL 3 02 80 020 100 REV035 25529=25819=26117=26270

01 MAR 2003 CCM 3.00.80 PAGE 08

3 02 90 001 001 REV028 ALL 3 02 90 002 105 REV030 24105=30203

3 02 90 003 001 REV033 ALL 3 02 90 004 001 REV028

R 3 02 90 005 001 REV036 ALL

3 03 00 001-2 001 REV027 ALL

3 03 01 001 001 REV035 ALL 3 03 01 002 001 REV035

3 03 01 003 001 REV034 ALL 3 03 01 004 001 REV034

3 03 01 005 001 REV024 ALL

3 03 02 001 001 REV034 ALL 3 03 02 002 001 REV025

3 03 03 001 001 REV024 ALL

3 03 04 001 001 REV024 ALL 3 03 04 002 001 REV025

3 03 04 003 100 REV028 22373=(22373+25072+28897) ALL 3 03 04 004 001 REV033

R 3 03 04 005 001 REV036 ALLR 3 03 04 006 100 REV025 MOD 22013 OR 24105 OR 24701

3 03 04 007 110 REV030 M:22013=24105=24701/CFM ALL ALL 3 03 04 008 001 REV024 CODE 0462

3 03 05 001 001 REV024 ALL 3 03 05 002 001 REV024

N 3 03 05 003 105 REV036 22199=24105 ALLN 3 03 05 004 001 REV024

3 03 05 005 001 REV033 ALL 3 03 05 006 001 REV032

3 03 06 003 100 REV033 24852=25336=27917=28218 ALL 3 03 06 004 105 REV032 M:24373

N 3 03 06 005 001 REV031 ALLN 3 03 06 006 100 REV036 MOD 22031=25440

3 03 06 007 001 REV025 ALL 3 03 06 008 001 REV033 STD=31896=31897

3 03 06 009 001 REV024 STD=31896=31897 ALL 3 03 06 010 001 REV024

01 MAR 2003 CCM 3.00.80 PAGE 09

3 03 06 011 001 REV035 ALL 3 03 06 012 100 REV034 21946

3 03 06 013 001 REV030 STD OR 24588 OR(24215+24588) ALL 3 03 06 014 001 REV030

3 03 06 015 001 REV028 ALL 3 03 06 016 001 REV029

R 3 03 07 001 001 REV033 ALLR 3 03 07 002 001 REV036

3 03 07 003 001 REV033 ALL

3 03 08 001 020 REV034 CFM56-5-A1/A3/A4/A5/B5/B6/B7 ALL 3 03 08 002 020 REV032 CFM ALL

3 03 08 003 040 REV030 CFM56-5-B1/B2/B3/B4/B5/B6/B7 ALL

3 03 10 001 001 REV034 ALL 3 03 10 002 001 REV034

3 03 10 003 200 REV024 MOD:21964+22087 ALL 3 03 10 004 001 REV033 STD=31896=31897

R 3 03 10 005 001 REV026 STD=31896=31897 ALLR 3 03 10 006 105 REV036 24105

R 3 03 11 001 040 REV036 CODE:0504/CFM ALLR 3 03 11 002 100 REV035 20081

3 03 12 001 001 REV030 ALL 3 03 12 002 120 REV025 CODE 0189 CFM ALL

3 03 12 005 001 REV033 CODE 0092 ALL 3 03 12 006 001 REV035

R 3 03 13 001 001 REV036 ALL

3 03 14 001 100 REV027 CODE 0189 ALL 3 03 14 002 100 REV027 MOD:24035 OR 24160 OR 24211

R 3 03 16 001 001 REV024 STD OR M:28238+28719 ALLR 3 03 16 002 001 REV036

3 03 16 003 001 REV035 CODE 0230 ALL

3 03 17 001 100 REV025 CODE 0036 ALL 3 03 17 002 001 REV024 STD=CODE 0211

01 MAR 2003 CCM 3.00.80 PAGE 10

R 3 03 17 003 100 REV036 CODE:0189 ALLR 3 03 17 004 100 REV034 24404=24405=25416=25530

N 3 03 18 001 200 REV027 M:26018+26398 ALLN 3 03 18 002 210 REV036 CODE:0578

R 3 03 18 003 100 REV036 CODE:0511 ALLR 3 03 18 004 100 REV030 CODE 0001

R 3 03 18 005 001 REV030 ALLR 3 03 18 006 001 REV036

R 3 03 18 007 001 REV036 ALLR 3 03 18 008 001 REV036

N 3 03 18 009 001 REV036 ALL

N 3 03 19 009 001 REV036 STD=M:24105 ALLN 3 03 19 010 001 REV036

N 3 03 19 011 100 REV036 M:24064=24065=24066=24067 ALLN 3 03 19 012 100 REV036 M:23742

N 3 03 19 013 001 REV036 ALL

N 3 03 20 001 100 REV035 26398 ALLN 3 03 20 002 001 REV024

3 03 21 001 001 REV024 ALL

3 03 22 001 035 REV032 56-5-B5/B6/B7 ALL 3 03 22 002 035 REV032 56-5-B5/B6/B7

R 3 03 22 003 105 REV035 24105 ALLR 3 03 22 004 105 REV036 M:24105

3 03 22 005 001 REV033 ALL 3 03 22 006 001 REV027

N 3 03 23 001 110 REV036 25863 ALLN 3 03 23 002 001 REV036

N 3 03 23 003 100 REV036 MOD:25863=(ACA/25863) ALLN 3 03 23 004 100 REV036 M:25863

3 03 24 001 100 REV035 20081 ALL 3 03 24 002 001 REV034 STD=(25951+32239)

01 MAR 2003 CCM 3.00.80 PAGE 11

3 03 25 001 020 REV035 CODE 0186/CFM ALL ALL 3 03 25 002 001 REV035

3 03 25 003 170 REV035 22013=23119/CFM ALL ALL

3 03 26 001 100 REV030 CODE 0213 ALL

3 03 90 001 001 REV035 ALL 3 03 90 002 001 REV034

3 03 90 003 001 REV027 ALL 3 03 90 004 001 REV027

3 03 90 005 001 REV027 ALL 3 03 90 006 001 REV030

3 03 90 007 001 REV033 ALL

3 04 00 003 001 REV033 ALL

3 04 10 001 001 REV024 ALL 3 04 10 002 115 REV028 M:24105/CFM ALL=IAE ALL

3 04 10 003 001 REV024 ALL 3 04 10 004 100 REV024 MOD:22013 OR 24105

3 04 21 001 001 REV032 ALL 3 04 21 002 001 REV024

N 3 04 23 001 001 REV036 ALL

N 3 04 23 001A 001 REV036 ALL

N 3 04 23 002 100 REV024 20137=(20137+28360+30239) ALL

3 04 23 003 100 REV024 CODE 0317 ALL

3 04 24 001 001 REV035 ALL 3 04 24 002 001 REV033

N 3 04 24 003 001 REV033 ALLN 3 04 24 004 103 REV036 24771

N 3 04 24 005 101 REV036 24613=22013+24613 ALLN 3 04 24 006 001 REV036

R 3 04 27 001 001 REV028 ALLR 3 04 27 002 001 REV036

R 3 04 27 003 001 REV036 ALLR 3 04 27 004 001 REV036

R 3 04 27 005 001 REV036 ALLR 3 04 27 006 001 REV036

01 MAR 2003 CCM 3.00.80 PAGE 12

R 3 04 27 007 001 REV036 ALLR 3 04 27 008 001 REV036

R 3 04 27 009 001 REV036 ALLR 3 04 27 010 001 REV036

N 3 04 27 011 001 REV036 ALLN 3 04 27 012 001 REV036

3 04 28 001 100 REV024 MOD:20024 ALL

3 04 30 001 100 REV034 22013=24105 ALL 3 04 30 002 001 REV024

3 04 31 001 001 REV024 ALL 3 04 31 002 001 REV024

3 04 32 001 001 REV031 ALL 3 04 32 002 001 REV031 STD OR (25951 + 32239)

3 04 32 003 001 REV034 ALL

3 04 34 001 001 REV030 ALL 3 04 34 002 100 REV032 CODE:0317

3 04 34 003 001 REV031 ALL 3 04 34 004 001 REV035

3 04 34 005 001 REV026 ALL 3 04 34 006 001 REV032

3 04 34 007 001 REV031 CODE 0058 ALL 3 04 34 008 001 REV034

3 04 34 009 100 REV034 23672=24581=24785=25108 ALL 3 04 34 010 001 REV024

3 04 34 015 120 REV024 CODE 0063 ALL 3 04 34 016 001 REV029

3 04 34 017 001 REV026 ALL 3 04 34 018 001 REV026

3 04 34 019 001 REV028 CODE 0258 ALL 3 04 34 020 001 REV028

3 04 34 021 100 REV031 M:26526 ALL

3 04 70 001 001 REV024 ALL 3 04 70 002 110 REV024 M:22013=24035=24160=24189

3 04 70 003 020 REV026 CFM ALL ALL 3 04 70 004 100 REV033 CODE 0145 CFM ALL

01 MAR 2003 CCM 3.00.80 PAGE 13

3 04 70 005 100 REV029 CODE 0145/CFM ALL ALL 3 04 70 006 020 REV033 STD=M:30439+31040/CFM

3 04 70 009 001 REV030 ALL 3 04 70 010 001 REV030

3 04 80 001 001 REV030 ALL 3 04 80 002 001 REV032

3 04 80 003 001 REV032 ALL

N 3 04 90 001 020 REV024 CFM ALL ALLN 3 04 90 002 020 REV035 CFM ALL

3 04 91 001 110 REV033 24105=(20268+24105) ALL 3 04 91 002 265 REV028 M:20268+24917 CFM 56-5-B5/B6

R 3 04 91 003 100 REV025 M:24917 ALLR 3 04 91 004 001 REV036

R 3 04 91 005 001 REV036 ALLR 3 04 91 006 001 REV026

N 3 04 91 007 001 REV036 ALLN 3 04 91 008 001 REV036

3 04 91 008A 001 REV033 ALL

3 04 91 009 001 REV035 ALL 3 04 91 010 001 REV028

3 04 91 011 001 REV028 ALL 3 04 91 012 001 REV028

3 04 91 013 100 REV028 M:21729 ALL 3 04 91 014 001 REV028

3 04 91 015 001 REV028 ALL

R 3 04 92 001 001 REV036 ALLR 3 04 92 002 001 REV036

R 3 04 92 003 001 REV033 ALLR 3 04 92 004 001 REV036

N 3 04 92 005 001 REV036 ALLN 3 04 92 006 001 REV036

3 05 00 001 001 REV025 ALL 3 05 00 002 001 REV024

3 05 05 001 001 REV024 ALL 3 05 05 002 001 REV025

3 05 05 003 001 REV024 ALL 3 05 05 004 001 REV024

01 MAR 2003 CCM 3.00.80 PAGE 14

3 05 05 005 001 REV032 ALL 3 05 05 006 001 REV024

3 05 06 001 020 REV024 CODE:0517 ALL 3 05 06 002 080 REV025 CFM 56-5-B6

3 05 06 003 080 REV025 CFM 56-5-B6 ALL 3 05 06 004 001 REV024

3 05 06 007 075 REV025 CFM 56-5-B5/B6 ALL 3 05 06 008 075 REV025 CFM 56-5-B5/B6

3 05 06 009 075 REV025 CODE:0513/56-5-B5/B6 ALL 3 05 06 010 020 REV025 STD=M:28238/CFM ALL/T=L

3 05 10 001 115 REV027 M:25800/CFM 56-5-B1 TO B7 ALL 3 05 10 002 280 REV031 CODE:0380/56-5-B5/B6

3 05 10 009 280 REV031 CODE:0380/56-5-B5/B6 ALL

3 05 15 005 280 REV035 CODE:0380/56-5-B5/B6 ALL 3 05 15 006 280 REV030 CODE:0380/56-5-B5/B6/T=L

3 05 15 007 280 REV030 CODE:0380/56-5-B5/B6 ALL 3 05 15 008 110 REV025 MOD:24105

01 MAR 2003 CCM 3.00.80 PAGE 15

3 05 20 001 250 REV030 M:24105+25800/56-5-B5/B6/B7 ALL 3 05 20 002 280 REV030 CODE:0380 56-5-B5/B6

3 05 20 003 280 REV030 CODE:0380 56-5-B5/B6 ALL 3 05 20 004 280 REV030 CODE:0380 56-5-B5/B6

3 05 20 017 280 REV030 CODE:0380 56-5-B5/B6 ALL

3 05 25 001 140 REV027 M:25800/56-5-B1 TO B7 ALL 3 05 25 002 280 REV031 CODE:0380/56-5-B5/B6

3 05 25 005 280 REV031 CODE:0380/56-5-B5/B6 ALL

3 05 30 001 120 REV027 M:25800/56-5-B ALL 3 05 30 002 280 REV030 CODE:0380 56-5-B5/B6

3 05 30 003 280 REV030 CODE 0380/CFM 56-5-B5/B6 ALL

R 3 05 35 001 100 REV036 M:22013=24105 ALLR 3 05 35 002 135 REV025 M:20268/CFM 56-5-B6

3 05 35 003 135 REV025 MOD:20268 CFM 56-5-B6 ALL 3 05 35 004 001 REV026

3 05 35 005 145 REV026 MOD 20268 CFM 56-5-B6 ALL 3 05 35 006 001 REV026

3 05 35 007 145 REV026 MOD 20268 CFM 56-5-B6 ALL 3 05 35 008 001 REV026

3 05 35 009 001 REV029 ALL 3 05 35 010 001 REV029

3 05 35 011 001 REV029 ALL 3 05 35 012 001 REV029

01 MAR 2003 CCM 3.00.80 PAGE 16

3 05 40 001 250 REV030 M:24105+25800/56-5-B5/B6/B7 ALL 3 05 40 002 280 REV030 CODE:0380 56-5-B5/B6

3 05 40 003 280 REV030 CODE:0380 56-5-B5/B6 ALL

3 05 50 001 001 REV025 ALL 3 05 50 002 001 REV026

3 05 50 003 110 REV025 MOD 24105 ALL 3 05 50 004 110 REV025 MOD 24105

3 06 00 001 001 REV024 ALL

3 06 10 001 125 REV027 M:25800/56-5-B ALL 3 06 10 002 001 REV024

3 06 20 001 225 REV035 CODE 0380 CFM 56-5-B5/B6 ALL

3 06 30 001 125 REV027 M:25800/56-5-B1 TO B7 ALL 3 06 30 002 280 REV030 CODE 0380 CFM 56-5-B5/B6

3 06 30 003 280 REV030 CODE 0380/CFM 56-5-B5/B6 ALL 3 06 30 004 280 REV030 CODE 0380 CFM 56-5-B5/B6

3 06 30 011 280 REV030 CODE 0380 CFM 56-5-B5/B6 ALL 3 06 30 012 235 REV030 M:24105+25800/56-5-B5/B6/B7

3 06 40 001 125 REV032 M:25800/56-5-B1 TO B7 ALL 3 06 40 002 280 REV030 CODE 0380/CFM 56-5-B5/B6

3 06 40 007 001 REV024 ALL

3 06 50 001 125 REV027 M:25800/56-5-B ALL 3 06 50 002 280 REV030 CODE 0380/CFM 56-5-B5/B6

3 06 50 003 280 REV030 CODE 0380/CFM 56-5-B5/B6 ALL 3 06 50 004 280 REV030 CODE 0380/CFM 56-5-B5/B6

01 MAR 2003 CCM 3.00.80 PAGE 17

3 06 50 013 235 REV030 M:24105+25800/56-5-B5/B6/B7 ALL 3 06 50 014 280 REV030 CODE 0380 CFM 56-5-B5/B6

3 06 70 001 002 REV024 ALL 3 06 70 002 110 REV024 MOD:24105

3 06 70 003 001 REV026 ALL

3 07 00 001-2 001 REV024 ALL

3 07 10 001-2 001 REV024 ALL

3 07 20 001 001 REV030 LIST OF EFFECTIVE OEBS ALL

3 07 30 001 001 REV025 ALL 3 07 30 002 001 REV025

01 MAR 2003 CCM 3.00.80 PAGE 18

318/319/320/321 FCOM VOLUME : 3 FLIGHT OPERATIONS LIST OF MOD/MP/SB AFFECTING THE MANUAL REVISION : 036

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

. 035A 20059 ...... AIR CONDITIONING - CARGO COMPARTMENT - ........... VENTILATION - INSTALL SYSTEM IN AFT COMPARTMENT - ALL

. 035A 20063 ...... OXYGEN - FLIGHT CREW SYSTEM - INSTALL ........... A 77.1 CU/FT BOTTLE IN COMPOSITE MATERIAL - ALL

. 035A 20067 ...... FIRE PROTECTION - FWD CARGO COMPARTMENT - ........... INSTALL SMOKE DETECTION SYSTEM - ALL

. 035A 20069 ...... FIRE PROTECTION - AFT CARGO COMPARTMENT - ........... INSTALL SMOKE DETECTION SYSTEM - ALL

. 035A 20071 ...... FIRE PROTECTION - CARGO COMPARTMENT ........... FIRE EXTINGUISHING - INSTALL A SINGLE SHOT SYSTEM - ALL

. 035A 20081 ...... LIGHTS - EXTERIOR LIGHTS - INSTALL ........... SYNCHRONIZED STROBE LIGHTS ALL

. 035A 20137 ...... COMMUNICATIONS - RADIO MANAGEMENT - ........... INSTALL A 3RD RMP - ALL

N 036 21206 ...... NAVIGATION - ADIRU - PROVIDE ........... COMMUNITY FOR CFM AND IAE ENGINES - ALL

CCM 3.00.8501 MAR 2003 PAGE 1

. 035A 21285 ...... ENGINE CONTROLS-MODIFY POWER SUPPLY ........... FOR HP FUEL SOLENOID ALL

. 035A 21678 ...... ELECTRICAL POWER-AC/DC ESSENTIAL POWER ........... DISTRIBUTION-PROVIDE PROVISIONS FOR ETOPS- ALL

. 035A 21706 ...... AIR CONDITIONING - VENTILATION CONT. ........... ISOLATION VALVES - CHANGE POWER SUPPLY FOR ETOPS - ALL

. 035A 21729 ...... AIR CONDITIONING -AVIONICS VENTILATION- ........... IMPROVE ACCURANCY OF SKIN TEMPERATURE READING ALL

. 035A 21812 ...... ICE AND RAIN PROTECTION - ........... WING ANTI-ICING - INSTALL MODIFIED VALVES ALL

. 035A 21899 ...... AIR CONDITIONING-AVIONICS VENTILATION- ........... INSTALL A NRV AT AIR INLET ALL

. 035A 21946 ...... OXYGENE - COCKPIT - INSTALL MODIFIED ........... LP OXYGEN SUPPLY SOLENOID VALVE ALL

. 035A 21964 ...... FLIGHT CONTROLS - ELAC/EFCS SYSTEM - ........... INTRODUCE SOFTWARE L62 ALL

. 035A 21988 ...... FUEL - IMPROVE LOW LEVEL WARNING ........... ALL

. 035A 21992 ...... INDICATING/RECORDING SYSTEMS - ........... INTRODUCE CFDIU BATCH 2 ALL

N 036 22031 ...... NAVIGATION - INSTALL BENDIX TYPE TRA ........... 67A ATC TRANSPONDERS (BFE) ALL

CCM 3.00.8501 MAR 2003 PAGE 2

. 035A 22087 ...... FLIGHT CONTROLS - FCDC - INSTALL ........... SOFTWARE L45 ALL

N 036 22199 ...... WINGS - REMOVE LEADING EDGE VENTILATION ........... SYSTEM ALL

. 035A 22249 ...... AUTO FLIGHT - ACTIVATE WINDSHEAR ........... FUNCTION ALL

. 035A 22373 ...... ELECTRICAL POWER - DC GENERATION - ........... INTRODUCE IMPROVED BCL ALL

. 035A 22450 ...... ICE AND RAIN PROTECTION - WING ICE ........... PROTECTION - INTRODUCE AN IMPROVED LOW PRESSURE WARNING SWITCH ALL

. 035A 22536 ...... NAVIGATION - INSTALL A BENDIX TCAS II ........... COLLISION AVOIDANCE SYSTEM ALL

. 035A 22561 ...... FIRE PROTECTION - LAVATORY SMOKE ........... DETECTION - INTRODUCE AMBIENT SYSTEM ALL

. 035A 22562 ...... AIRBORNE AUXILIARY POWER UNIT - ........... INTRODUCE APIC APS-3200 ALL

. 035A 22707 ...... INDICATING RECORDING SYSTEMS - EIS - ........... DEFINE COF A STANDARD FOR A320/A321 DMC ALL

. 035A 22769 ...... NAVIGATION - GPWS - INSTALL GPWC ........... MARK V WITH INTERFACE WITH CFDS ALL

. 035A 22875 ...... ICE AND RAIN PROTECTION - ICE DETECTION - ........... INSTALL DUAL ADVISORY ICE DETECTION SYSTEM ALL

CCM 3.00.8501 MAR 2003 PAGE 3

. 035A 23119 ...... HYDRAULIC POWER-BLUE MAIN HYDRAULIC ........... POWER-IMPROVE MAINTENANCE STATUS OF BLUE HYDRAULIC RESERVOIR ALL

. 035A 23208 ...... LANDING GEAR - WHEELS AND BRAKES - ........... INTRODUCE BSCU STD 6 ALL

. 035A 23661 ...... ENGINE FUEL AND CONTROL - CFM 56 - ........... EIU - INTRODUCE VERSION 13 ALL

. 035A 23672 ...... NAVIGATION - ADIRS - INSTALL LITTON ........... 4MCU ON A321 A/C ALL

. 035A 23698 ...... AUXILIARY POWER UNIT - CONTROL AND ........... MONITORING - INTRODUCE A NEW ECB ALL

. 035A 23699 ...... AUXILIARY POWER UNIT - CONTROL AND ........... MONITORING - MODIFY WIRE HARNESSES FOR NEW ECB 817-1 ALL

. 035A 23779 ...... MINOR IMPROVEMENTS INTRODUCED FROM ........... A/C 508 (ST2) TO A/C 521 (ST2) ALL

. 035A 23901 ...... LANDING GEAR - WHEELS AND BRAKES - ........... INTRODUCE MODIFIED ALTERNATE BRAKE DISTRIBUTION DUAL VALVE ALL

CCM 3.00.8501 MAR 2003 PAGE 4

. 035A 24077 ...... LANDING GEAR - BSCU - TWIN WHEEL - ........... INTRODUCE A320/A321 STD 6 VERSION 60C ALL

. 035A 24215 ...... AUTO FLIGHT - FAC - INSTALL TWO FACS ........... P/N BAM 0509 ALL

. 035A 24373 ...... FUEL - TANK LEVEL SENSING - INTRODUCE ........... MODIFIED LOW FUEL PRESSURE WARNING CONTROL ALL

. 035A 24440 ...... LANDING GEAR-NOSE LANDING GEAR- ........... SHOCK ABSORBER-INTRODUCE MODIFIED THROTTLING ROD GUIDE ALL

. 035A 24449 ...... LANDING GEAR - A320/A321 TWIN WHEELS - ........... INTRODUCE BSCU STANDARD 7 (70B VERSION) ALL

. 035A 24498 ...... APU - STORAGE AND DISTRIBUTION - ........... MODIFY APU COMMON LUBRICATION SYSTEM ALL

. 035A 24511 ...... FLIGHT CONTROLS -S.E.C. SYSTEM ........... INTRODUCE A320/A321 S.E.C STANDARD P/N BAM0508 ALL

. 035A 24588 ...... AUTO FLIGHT-FAC-INTRODUCE FAC ........... P/N BAM 510 ALL

CCM 3.00.8501 MAR 2003 PAGE 5

. 035A 24612 ...... INDICATING/RECORDING SYSTEMS - FWC - ........... INTRODUCE FWC D2 STD ALL

. 035A 24613 ...... FLIGHT CONTROLS - ELAC - INTRODUCE ........... ELAC STD P/N L69 ALL

. 035A 24642 ...... ELECTRICAL POWER - AC AUXILIARY ........... GENERATION (APU GENERATOR) - INTRODUCE MODIFIED GENERATOR ALL

. 035A 24645 ...... LANDING GEAR-MLG-LGCIU-INTRODUCTION ........... OF STANDARD UNIT P/N A4C ALL

N 036 24771 ...... COMMUNICATIONS-CIDS-INTRODUCE ........... MODIFIED DIRECTOR POWER SUPPLY PRINCIPLE ALL

. 035A 24783 ...... ENGINE FUEL AND CONTROL-FUNCTIONAL ........... INTERFACE-INTRODUCE EIU VERSION 14 ON CFM56 ENGINES ALL

. 035A 24794 ...... AIR CONDITIONING-COCKPIT AND CABIN ........... TEMPERATURE CTRL-INTRODUCE MODIFIED TEMPERATURE SENSOR P/N-02.ON MIXER UNIT ALL

. 035A 24805 ...... PNEUMATIC-ENGINE BLEED AIR SUPPLY- ........... INTRODUCE A BLEED AIR MONITORNG COMPUTER STD6 ALL

. 035A 24852 ...... NAVIGATION-ADIRU-INTRODUCE ADIRU ........... P/N -307 ALL

. 035A 24917 ...... FLIGHT CONTROLS-INTRODUCE ELAC STD ........... L69J ALL

CCM 3.00.8501 MAR 2003 PAGE 6

. 035A 24946 ...... LANDING GEAR - MLG - MESSIER - ........... INTRODUCE BRAKES P/N C202253 ALL

. 035A 24955 ...... AIRBORNE AUXILIARY POWER-ENGINE- ........... APIC APS 3200-INTRODUCE MODIFIED PRESS REGULATOR ON FCU ALL

. 035A 25199 ...... FLIGHT MANAGEMENT AND GUIDANCE SYSTEM- ........... INSTALL FMGC ON A320/321 (CFM 56-5A/5B) ALL

. 035A 25241 ...... COMMUNICATIONS - RADIO MANAGEMENT - ........... INSTALL A NEW STD RMP1 AND RMP2 WITH VHS SPACING 8, 33KHZ ALL

. 035A 25242 ...... COMMUNICATIONS - RADIO MANAGEMENT - ........... INSTALL A NEW STD RMP3 (3⁰) WITH VHF SPACING 8, 33KHZ ALL

. 035A 25294 ...... NAVIGATION - ADIRS - INSTALL HONEYWELL ........... ADIRS CAPABLE OF A319 A/C ALL

. 035A 25335 ...... FLIGHT CONTROLS-ELAC-INTRODUCE A319 EIS ........... L77 SOFTWARE STD- ALL

. 035A 25336 ...... NAVIGATION-ADIRS-INTRODUCE AIRU ........... LITTON P/N -308 ALL

. 035A 25360 ...... FLIGHT CONTROLS-SLATS/FLAPS-ELECTRICAL ........... CONTROL AND MONITORING INTRODUCE SFCC P/N 07 ON A319 A/C AND A321 AIRCRAFT ALL

CCM 3.00.8501 MAR 2003 PAGE 7

. 035A 25404 ...... EXHAUST-THRUST REVERSER CONTROL AND ........... INDICATING-ACTIVATE ADDITIONAL THRUST REVERSER LOCK CONTROL ALL

. 035A 25410 ...... INDICATING RECORDING SYSTEM-FWC- ........... INTRODUCE F.W.C. E1 STANDARD ALL

. 035A 25419 ...... ICE AND RAIN PROTECTION-WINDSHIELD ........... RAIN PROTECTION-DESACTIVATION OF RAIN REPELLENT SYSTEM ALL

N 036 25440 ...... NAVIGATION - GENERAL - CHANGE ........... EQUIPMENTS TO COMPLY WITH MARCH 95 SPECS. ALL

. 035A 25529 ...... NAVIGATION - WEATHER RADAR SYSTEM - ........... ACTIVATE PREDICTIVE WINDSHEAR FUNCTION ALL

. 035A 25800 ...... POWER PLANT-GENERAL-INTRODUCE ........... CFM56-5B/P ALL

. 035A 25871 ...... ENGINE FUEL AND CONTROL-CONTROLLING- ........... INTRODUCE ECU SOFTWARE 5DH FOR CFM56-5B (DAC -DAC/P) ENGINES ALL

N 036 26000 ...... NAVIGATION-ADIRS-INTRODUCE HONEYWELL ........... ADIRU 4 MCU STD WITH HARDWARE P/N AD09 ALL

CCM 3.00.8501 MAR 2003 PAGE 8

. 035A 26001 ...... NAVIGATION-ADIRS-INTRODUCE HONEYWELL ........... 4 MCU P/N AC09 ALL

. 035A 26187 ...... NAVIGATION - VOR - INSTALL VOR ........... RECEIVERS ALLIED SIGNAL QUANTUM LINE P/N 066-50012-0202 ALL

. 035A 26363 ...... AIR CONDITIONING-AIR COOLING SYSTEM- ........... INTRODUCE MODIFIED RAM AIR OUTLET ALL

. 035A 26377 ...... NAVIGATION - ILS - INSTALL ADDITIONAL ........... WIRING PROVISIONS FOR MMR INSTALLATION ALL

N 036 26398 ...... ADDITIONAL CERTIFICATION ITEMS - 00-1043 06 LANDING WITH A 15 KNOT TAILWIND ALL

. 035B 26443 ...... NAVIGATION - VOR/MARKER - INSTALL TWO ........... VOR/MARKER RECEIVERS 900 COLLINS P/N 822-0297-020 OO-SSF

. 035A 26457 ...... GENERAL - DESIGN WEIGHTS - INCREASE ........... MAXIMUM TAKE-OFF WEIGHT (MTOW) TO 68T ALL

CCM 3.00.8501 MAR 2003 PAGE 9

. 035A 26526 ...... NAVIGATION - GPWS - ACTIVATE ........... ENHANCED FUNCTIONS OF THE EGPWS ALL

. 035A 26642 ...... ENGINE -CONTROLLING-CFM56-5B/2 ........... FADEC SYSTEM-INTRODUCE ECU STD 5DK ALL

. 035A 26645 ...... AUTO-FLIGHT-FAC INTRODUCE FAC STD BAM ........... 0513 ALL

. 035A 26726 ...... INDICATING/RECORDING SYSTEM-SDAC- ........... INTRODUCE SDAC (NEW TECHNOLOGY ) ALL

. 035A 26785 ...... PNEUMATIC-ENG BLEED AIR SYS-INTRODUCE ........... A TEMP THERMOSTAT WITH MODIFIED LIMITATION SETTINGS (P/N 341E020000) ALL

. 035A 26792 ...... AIR CONDITIONING-PACK TEMPERATURE CTRL- ........... INTRODUCE MODIFIED PACK TEMPERATURE CONTROLLER ALL

. 035A 26963 ...... ICE AND RAIN PROTECTION-WINSHIELD RAIN ........... PROTECTION-ACTIVATION OF RAIN REPELLENT SYS.(FLUID COMPATIBLE WITH OZONE RULES) ALL

. 035A 27276 ...... FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ........... ELAC SOFTWARE DL80D ALL

CCM 3.00.8501 MAR 2003 PAGE 10

. 035A 27498 ...... ELECTRICAL POWER - GENERAL - AC-DC ........... MAIN DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS ALL

. 035A 27572 ...... OXYGEN-PASSENGER OXYGEN-INTRODUCE ........... MODIFIED CHEMICAL OXYGEN CONTAINER -15 MIN- PURITAN ALL

. 035A 27646 ...... NAVIGATION - MMR - INSTALL SEXTANT MMR ........... PROVIDING ILS (FM IMMUNE) ALL

. 035A 27698 ...... NAVIGATION - TCAS - INSTALL ALLIED 34-1177 10 SIGNAL TCAS COMPUTER P/N 066-50000-2220 (WITH CHANGE 7.0) ALL

. 035A 27723 ...... PNEUMATIC-ENGINE BLEED AIR SUPPLY ........... SYSTEM-INTRODUCE NEW TEMPERATURE CTL THERMOSTATS (SERIAL AND RETROFIT) ALL

. 035A 27725 ...... ENGINE FUEL AND CONTROL-FADEC SYSTEM- ........... INTRODUCE ECU SOFTWARE 5DM FOR CFM56-5B DAC ENGINE ALL

. 035A 27727 ...... ENGINE -COMBUSTION SECTION- ........... INTRODUCE CFM56-5B DAC II PIP ENGINES ALL

. 035A 27866 ...... NAVIGATION - WEATHER RADAR SYSTEM - 34-1178 06 INSTALL ALLIED SIGNAL WEATHER RADAR TRANSCEIVER P/N 066-50008-0405 ALL

CCM 3.00.8501 MAR 2003 PAGE 11

. 035A 27952 ...... PNEUMATIC-ENGINE BLEED AIR SYSTEM- ........... INTRODUCE TLT P/N 341E030000 ALL

. 035A 28009 ...... AIR CONDITIONING-PRESSURE CONTROL AND 21-1116 04 MONITORING-INTRODUCE PRESSURE CONTROLLER P/N 9022-15702-10 ALL

. 035A 28164 ...... LANDING GEAR - WHEELS AND BRAKES - ........... INSTALL CARBON BRAKES TYPE SEPCARB III PLUS - MESSIER BUGATTI ALL

. 035A 28244 ...... NAVIGATION-GPWS-INTRODUCE EGPWS 34-1193 18 P/N 206-206 AND INHIBIT AUTOMATIC DEACTIVATION ENHANCED FUNCTIONS ALL

. 035A 28284 ...... NAVIGATION-ILS-INSTALL SEXTANT MMR ........... PROVIDING ILS (FM IMMUNE) P/N TLS 755.01.0101B ALL

. 035A 28377 ...... ICE AND RAIN PROTECTION-WINSHIELD- ........... RAIN PROTECTION-INTRODUCE MODIFIED GAGE ASSY -P/N 4020W35-2 ALL

CCM 3.00.8501 MAR 2003 PAGE 12

. 035A 28488 ...... AIR CONDITIONING-PACK TEMP.CTRL ........... INTRODUCE MODIFIED PACK TEMP. CTRL P/N 759D0000-02 ALL

. 035B 28495 ...... NAVIGATION - MMR - REMOVE COLLINS MMR ........... PROVIDING ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION (PREVIOUS SPEC.) OO-SSF

. 035A 28667 ...... ICE AND RAIN PROTECTION-WINDSHIELD RAIN ........... PROTECTION-INTRODUCE MODIFIED GAGE ASSY WITH INPUT VALUE FUNCTION SUPPRESSED ALL

. 035B 28669 ...... NAVIGATION-VOR/MARKER-REINTRODUCE ........... COLLINS 700 VOR/MARKER RECEIVERS (PREVIOUS A/C STANDARD SPECIFICATION) OO-SSF

. 035B 30239 ...... INFORMATION SYSTEM - ATIMS - MODIFY 46-1009 06 ATSU AIRCRAFT INTERFACE SOFTWARE ACCORDING TO SERVICE PROVIDERS LIST OO-SSF

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

CCM 3.00.8501 MAR 2003 PAGE 13

CCM ALL

CCM MSN 1068

CCM MSN 1145

CCM ALL

1068 OO-SSB 1145 OO-SSF

CCM 4.00.70 01 DEC 2002 PAGE : CRT001

318/319/320/321 FCOM VOL. 4 PILOT)S GUIDE HIGHLIGHTS REV014

4 02 20 002 100 REV014 CODE:0101

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - TECHNICAL AMENDMENT 1)+Required+ and +Estimated+ navigation accuracy values have be revised to reflect more realistic Enroute values on the MCDU, in accordance with the EFIS ND display.

4 02 20 003 100 REV008 CODE:0101

- INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635

4 02 20 006 100 REV011 CODE 0056

- INCORPORATION OF MOD 31364 - INCORPORATION OF MOD 31365 - DELETION OF MOD 25240 - DELETION OF MOD 25274

4 02 20 007 100 REV011 CODE 0056

- INCORPORATION OF MOD 31364 - INCORPORATION OF MOD 31365 - DELETION OF MOD 25240 - DELETION OF MOD 25274

4 02 20 009 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)The missing reference to the LATERAL FUNCTIONS chapter 4.04 has been added.

4 02 20 011 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)Switching conditions from the CRUISE phase to the DESCENT phase are modified to reflect the actual behavior of the A320 FMS Legacy.

4 02 20 014 100 REV006 CODE 0002

- DELETION OF MOD 25240 - DELETION OF MOD 25274

4 02 20 014 100 REV014 CODE 0056

- TECHNICAL AMENDMENT 1)The CG is not considered for the BEST TARGET SPEED computation.

01 DEC 2002 CCM 4.00.75 PAGE 1

4 02 20 015 100 REV007 CODE 0002

4 02 20 015 100 REV014 CODE 0056

- TECHNICAL AMENDMENT 1)Addition of a note regarding the OPTIMUM FLIGHT LEVEL (OPT FL) computed by the FMS : differences between the FCOM/QRH and the FMS value may be observed, and wind entries made at different altitudes may affect the FMS-computed OPTIMUM FLIGHT LEVEL. .

4 02 20 016 100 REV012 CODE 0056

- INCORPORATION OF MOD 26968 - INCORPORATION OF MOD 27831 - INCORPORATION OF MOD 28283 - INCORPORATION OF MOD 28711 - INCORPORATION OF MOD 31364 - INCORPORATION OF MOD 31365

4 02 20 018 001 REV014 CODE 0055

4 02 20 022 001 REV014

- TECHNICAL AMENDMENT 1)Reference to required distance to land and direct distance to destination have been removed, as they are already described in the corresponding MCDU DES PROG page description section.

4 02 30 002 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)Addition of a note for selecting the LOC* and LOC modes by using the FCU)s LOC pushbutton, rather than the APPR pushbutton, in case of a LOC only approach.

4 02 30 007 100 REV006 CODE 0002

4 02 30 007 100 REV014 CODE 0056

- TECHNICAL AMENDMENT 1)Page revised to clarify the DESCENT SPEED PROFILE definition.

01 DEC 2002 CCM 4.00.75 PAGE 2

4 02 30 010 001 REV014

- TECHNICAL AMENDMENT 1)When in a holding pattern, the aircraft will respect the altitude constraints as well as the FCU selected altitude.

4 02 30 012 001 REV014

- TECHNICAL AMENDMENT 1)The APPROACH MODES have been clarified to introduce the precision and non-precision approach concept. Furthermore, the LOC and LOC B/C approach types are clarified to highlight that the APPR pushbutton is not used to arm the LOC guidance mode, but the LOC pushbutton is.

4 03 00 001 001 REV014 CODE:0055

- TECHNICAL AMENDMENT 1)Contents update.

4 03 10 002 110 REV014 CODE 0033

- TECHNICAL AMENDMENT 1)Addition of information to reflect that the PFD)s altitude display in metric units is an +as installed+ item.

4 03 20 003 100 REV011 CODE 0002

4 03 20 004 100 REV006 CODE 0002

4 03 20 005 100 REV011 CODE 0002

4 03 20 008 100 REV006 CODE 0002

4 03 20 009 100 REV011 CODE 0002

4 03 20 010 100 REV006 CODE 0002

01 DEC 2002 CCM 4.00.75 PAGE 3

4 03 20 011 100 REV008 CODE 0002

4 03 20 012 001 REV014 CODE:0055

- TECHNICAL AMENDMENT 1)After first engine start, the FMGS computes predictions based on the FQI FOB (FAC as backup), and not on the BLOCK entry.

4 03 20 014 100 REV008 CODE 0002

4 03 20 015 100 REV006 CODE 0002

4 03 20 026 001 REV014 CODE:0055

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensured correct page validation for all customers.

4 03 20 032 105 REV011 CODE 0096

- INCORPORATION OF MOD 28283 - DELETION OF MOD 25240 - DELETION OF MOD 25274

4 03 20 033 100 REV007 CODE 0002

4 03 20 052 100 REV014 CODE:0101

- INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - TECHNICAL AMENDMENT 1)Page updated to further specify the aircraft definition : GPS PRIMARY Function is installed.

4 03 20 053 100 REV011 CODE:0101

- INCORPORATION OF MOD 25025 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - DELETION OF MOD 23885 - DELETION OF MOD 24075 - DELETION OF MOD 25205

01 DEC 2002 CCM 4.00.75 PAGE 4

4 03 20 054 100 REV014 CODE:0101

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - TECHNICAL AMENDMENT 1)Page created to further specify the aircraft definition : The +DESELECT/ SELECT GPS 5L+ key is installed.

4 03 20 055 105 REV009 CODE:0102

- INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30631

4 03 20 056 100 REV014 CODE 0082

4 03 20 060 100 REV014 CODE 0082

- TECHNICAL AMENDMENT 1)Information has been moved to the next page for pagination purposes.

4 03 20 061 100 REV014 CODE 0082

- TECHNICAL AMENDMENT 1)Information has been moved from the previous page for pagination purposes. 2)If the uplinked TOW/TOCG differs from an already existing TOW/TOCG, the INSERT UPLINK* prompt is not displayed.

4 03 20 071 001 REV014 CODE:0055

- TECHNICAL AMENDMENT 1)Clarification of the conditions for displaying or blanking the MCDU PERF fields.

4 03 20 072 100 REV006 CODE 0002

4 03 20 073 100 REV006 CODE 0002

01 DEC 2002 CCM 4.00.75 PAGE 5

4 03 20 080 100 REV014 CODE:0101

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - TECHNICAL AMENDMENT 1)The +Required+ and +Estimated+ navigation accuracy values have been changed on the PROG CRUISE and PROG DES pages to be consistent with the current navigation mode (GPS PRIMARY) in the Enroute area.

4 03 20 081 100 REV014 CODE:0056

- INCORPORATION OF MOD 27831 - INCORPORATION OF MOD 28283 - INCORPORATION OF MOD 28711 - INCORPORATION OF MOD 31364 - INCORPORATION OF MOD 31365 - TECHNICAL AMENDMENT 1)Page revised to indicate that the maximum REC MAX value is FL391 instead of FL390.

4 03 20 082 100 REV014 CODE:0101

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - TECHNICAL AMENDMENT 1)The +Required+ navigation accuracy field has been revised to reflect more realistic TERMINAL area values on the MCDU PROG page.

4 03 20 083 100 REV014 CODE:0101

- INCORPORATION OF MOD 25205 - INCORPORATION OF MOD 26111 - INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 26999 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30241 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - TECHNICAL AMENDMENT 1)Reference to the FCOM Volume 1 replaces previous reference to the FCOM Volume 4.

4 03 20 084 100 REV006 CODE:0114

- INCORPORATION OF MOD 24105 - INCORPORATION OF MOD 25294

01 DEC 2002 CCM 4.00.75 PAGE 6

4 03 20 084 100 REV006 CODE:0114

- INCORPORATION OF MOD 28495 - DELETION OF MOD 25205 - DELETION OF MOD 30241

4 03 20 085 100 REV006 CODE:0114

- INCORPORATION OF MOD 24105 - INCORPORATION OF MOD 25294 - INCORPORATION OF MOD 28495 - DELETION OF MOD 25205 - DELETION OF MOD 30241

4 03 20 089 105 REV006 CODE 0002

4 03 30 001 001 REV014 CODE:0055

- TECHNICAL AMENDMENT 1)The conditions for displaying the +ALIGN IRS+ message have been clarified.

4 04 00 001 001 REV006 CODE 0055

- TECHNICAL AMENDMENT 1)Index tailored to FMS2 Thales/Smiths (rev 1).

4 04 10 014 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)The MCDU screens have been changed to reflect the actual holding pattern and correct display. Text has also been modified for improved technical understanding.

4 04 10 015 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)When in a holding pattern, the aircraft will respect the altitude constraints as well as the FCU selected altitude.

4 04 10 021 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)Page modified for better technical understanding.

4 04 10 022 001 REV014 CODE 0055

4 04 10 030 001 REV014

- TECHNICAL AMENDMENT 1)The PROG page displayed as an

01 DEC 2002 CCM 4.00.75 PAGE 7

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- example was amended to show a more realistic situation.

4 04 20 003 100 REV006 CODE 0002

4 04 20 004 100 REV006 CODE 0002

4 04 20 005 100 REV006 CODE 0002

4 04 20 006 100 REV011 CODE 0002

4 04 20 007 100 REV006 CODE 0002

4 04 20 008 100 REV006 CODE 0002

4 04 30 003 001 REV014

- TECHNICAL AMENDMENT 1)+PROCEDURES+ item has been modified : if there is an AMSL Altitude constraint above the transition altitude in the departure procedure, the crew must convert it into STD before insertion in the MCDU. 2)The sequence number was changed to ensure the correct page validation for all customers.

4 04 30 010 001 REV014 CODE 0055

4 04 30 017 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)The reference to +Multifunction Control and Display Unit+ has been amended to read +MCDU+.

4 04 30 018 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the

01 DEC 2002 CCM 4.00.75 PAGE 8

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- correct page validation for all customers.

4 04 30 021 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)The reference to +Multifunction Control and Display Unit+ has been amended to read +MCDU+.

4 05 10 003 100 REV006 CODE 0002

4 05 10 004 100 REV006 CODE 0002

4 05 10 007 100 REV006 CODE 0002

4 05 10 008 100 REV006 CODE 0002

4 05 10 010 100 REV007 CODE 0002

4 05 10 010 100 REV014 CODE 0056

- TECHNICAL AMENDMENT 1)The note about altitude constraint entries has been clarified.

4 05 10 014 001 REV014 CODE 0055

4 05 10 021 100 REV014 CODE 0058

- TECHNICAL AMENDMENT 1)During cockpit preparation, the PERF CLB page is accessed by pressing the +NEXT PHASE+ prompt on the PERF TAKEOFF page, not by the MCDU +NEXT PAGE+ key.

4 05 10 022 100 REV014 CODE 0058

- TECHNICAL AMENDMENT 1)Access to the PERF CRZ page has been clarified.

4 05 30 006 001 REV014

- TECHNICAL AMENDMENT 1)No technical change. The sequence

01 DEC 2002 CCM 4.00.75 PAGE 9

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- number was changed to ensure the correct page validation for all customers.

4 05 40 001 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)Page modified for better technical understanding. 2)Addition of missing information on the PERF CLB screen.

4 05 50 003 100 REV014 CODE:0101

- INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30631 - INCORPORATION OF MOD 30635 - TECHNICAL AMENDMENT 1)FCOM page revised to reflect the correct MCDU display corresponding to the procedure.

4 05 50 011 100 REV006 CODE 0002

4 05 60 008 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)No technical change. The sequence number has changed to ensure correct validity for all customers.

4 05 70 001 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)The PERF DES page has been revised to add missing information : Time/Distance predictions to FL025 are also available for the ECON mode.

4 05 70 007 110 REV008 CODE 0010

4 05 70 009 001 REV014 CODE 0055

- TECHNICAL AMENDMENT 1)The CAUTION has been slightly modified to provide the correct message +CHECK APPR GUIDANCE+.

4 05 70 015 001 REV014 CODE 0055

4 05 70 027 001 REV014

- TECHNICAL AMENDMENT 1)A caution is added to advise the crew not to select the APPR pushbutton for

01 DEC 2002 CCM 4.00.75 PAGE 10

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA----- -----------------------REASONS OF CHANGE--------------------------------------------------------------------------------------------------------- a LOC only approach.

4 06 20 006 001 REV014 CODE 0055

4 06 20 007 001 REV014 CODE 0064

- TECHNICAL AMENDMENT 1)No technical change. The sequence number has been changed to ensure correct validity for all customers.

4 06 20 008 001 REV014 CODE:0055

01 DEC 2002 CCM 4.00.75 PAGE 11

318/319/320/321 FCOM VOL.4 (PILOT)S GUIDE ) -REV 014 LIST OF EFFECTIVE PAGES (LEP) -

4 00 00 001-2 001 REV007 ALL

R 4 00 30 001 001 REV014 LIST OF NORMAL REVISIONS ALL

4 01 00 001 001 REV006 ALL

4 01 10 001 001 REV006 ALL 4 01 10 002 001 REV006

4 02 00 001 001 REV006 ALL

4 02 10 001 001 REV006 ALL

N 4 02 20 001 001 REV006 ALLN 4 02 20 002 100 REV014 CODE:0101

4 02 20 005 001 REV006 ALL 4 02 20 006 100 REV011 CODE 0056

01 DEC 2002 CCM 4.00.80 PAGE 01

4 02 20 019 001 REV006 ALL 4 02 20 020 001 REV006

N 4 02 20 021 001 REV006 ALLN 4 02 20 022 001 REV014

4 02 30 003 100 REV006 M:24035 OR 24160 OR 24211 ALL 4 02 30 004 100 REV006 M:24035 OR 24160 OR 24211

4 02 30 005 100 REV006 CODE 0059 ALL 4 02 30 006 001 REV006

N 4 02 30 009 001 REV006 ALLN 4 02 30 010 001 REV014

R 4 02 30 011 100 REV006 M:24035 OR 24160 OR 24211 ALLR 4 02 30 012 001 REV014

4 02 30 013 100 REV008 M:24035=24160=24211 ALL

R 4 03 00 001 001 REV014 CODE:0055 ALLR 4 03 00 002 001 REV006 CODE:0055

R 4 03 10 001 105 REV008 M:27541=(27256+27541) ALLR 4 03 10 002 110 REV014 CODE 0033

4 03 10 003 001 REV013 ALL 4 03 10 004 120 REV006 M.24035=24160=(24189+24211)

4 03 10 005 001 REV006 ALL

01 DEC 2002 CCM 4.00.80 PAGE 02

N 4 03 20 025 001 REV011 CODE:0055 ALLN 4 03 20 026 001 REV014 CODE:0055

01 DEC 2002 CCM 4.00.80 PAGE 03

01 DEC 2002 CCM 4.00.80 PAGE 04

4 03 30 011 100 REV008 CODE:0086 1145

4 03 40 001 001 REV006 ALL 4 03 40 002 001 REV011

4 03 40 003 001 REV011 ALL 4 03 40 004 001 REV011

4 03 40 005 001 REV011 ALL 4 03 40 006 001 REV011

4 03 40 007 001 REV011 ALL 4 03 40 008 001 REV011

4 03 40 009 001 REV011 ALL 4 03 40 010 001 REV011

4 04 00 001 001 REV006 CODE 0055 ALL

01 DEC 2002 CCM 4.00.80 PAGE 05

4 04 10 031 001 REV006 CODE 0055 ALL

4 04 30 001 001 REV006 ALL 4 04 30 002 001 REV013

N 4 04 30 003 001 REV014 ALLN 4 04 30 004 001 REV006

4 04 30 005 001 REV006 ALL 4 04 30 006 001 REV006 CODE 0055

01 DEC 2002 CCM 4.00.80 PAGE 06

4 04 30 011 001 REV010 ALL 4 04 30 012 001 REV006

4 04 30 013 100 REV008 M:23742 ALL 4 04 30 014 110 REV008 M:26497=(23742+26497)

4 04 30 015 001 REV011 ALL 4 04 30 016 100 REV011 M:26497

4 04 30 019 001 REV006 CODE 0055 ALL 4 04 30 020 001 REV006

R 4 04 30 021 001 REV014 CODE 0055 ALL

4 04 40 001 100 REV006 M:25295=27522 ALL 4 04 40 002 100 REV006 M:25295=27522

4 04 40 003 100 REV006 M:25295=27522 ALL 4 04 40 004 100 REV006 M:25295=27522

4 04 40 005 100 REV006 M:25295=27522 ALL 4 04 40 006 100 REV006 M:25295=27522

4 04 40 007 100 REV006 M:25295=27522 ALL 4 04 40 008 100 REV006 M:25295=27522

4 05 00 001 001 REV011 ALL 4 05 00 002 100 REV010 M:25863

4 05 05 001 001 REV006 ALL

4 05 10 005 001 REV006 CODE 0055 ALL 4 05 10 006 001 REV006

4 05 10 011 001 REV006 ALL 4 05 10 012 001 REV006 CODE 0055

4 05 10 015 001 REV011 ALL 4 05 10 016 001 REV006 CODE 0088

01 DEC 2002 CCM 4.00.80 PAGE 07

4 05 10 019 001 REV011 ALL 4 05 10 020 001 REV011

4 05 10 023 001 REV011 ALL

4 05 15 001 001 REV007 CODE 0055 ALL 4 05 15 002 001 REV006

4 05 20 001 200 REV006 M:(23742+24035)=(23742+24189 ALL 4 05 20 002 100 REV007 M:24035 OR 24189

4 05 30 007 001 REV011 CODE 0055 ALL

R 4 05 40 001 001 REV014 CODE 0055 ALLR 4 05 40 002 100 REV006 M:24035 OR 24160 OR 24211

4 05 40 005 001 REV006 ALL 4 05 40 006 100 REV006 M:24035 OR 24160 OR 24211

4 05 50 001 001 REV008 ALL 4 05 50 002 001 REV006

R 4 05 50 003 100 REV014 CODE:0101 ALLR 4 05 50 004 001 REV006

4 05 50 005 001 REV011 ALL 4 05 50 006 001 REV006 CODE 0055

4 05 50 006A 001 REV011 CODE 0055 ALL

4 05 50 007 001 REV011 ALL 4 05 50 008 001 REV006

4 05 50 009 001 REV006 ALL 4 05 50 010 001 REV007 CODE 0055

01 DEC 2002 CCM 4.00.80 PAGE 08

4 05 50 013 001 REV006 ALL 4 05 50 014 001 REV006

4 05 60 001 001 REV010 ALL 4 05 60 002 100 REV006 M:24035 OR 24160 OR 24211

4 05 60 003 100 REV006 M:24035 OR 24160 OR 24211 ALL 4 05 60 004 100 REV006 CODE 0058

4 05 60 005 100 REV011 M:24035 OR 24160 OR 24211 ALL 4 05 60 006 001 REV008

4 05 60 009 001 REV006 ALL 4 05 60 010 001 REV010

4 05 70 003 001 REV006 ALL 4 05 70 004 001 REV011

4 05 70 005 001 REV006 ALL 4 05 70 006 110 REV006 M:24035=24160=(24189+24211)

4 05 70 007 110 REV008 M: 26497 ALL 4 05 70 008 001 REV006

4 05 70 008A 100 REV010 CODE 0054 ALL

4 05 70 011 001 REV008 ALL 4 05 70 012 001 REV008

4 05 70 013 001 REV008 ALL 4 05 70 014 001 REV007

4 05 70 017 001 REV011 ALL 4 05 70 018 001 REV011

4 05 70 019 001 REV011 ALL 4 05 70 020 001 REV006 CODE 0055

4 05 70 023 100 REV011 M:24035=24160=24211 ALL 4 05 70 024 100 REV008 M:24035=24160=24211

4 05 70 025 200 REV009 CODE:0016 ALL 4 05 70 026 001 REV007

01 DEC 2002 CCM 4.00.80 PAGE 09

R 4 05 70 027 001 REV014 ALLR 4 05 70 028 100 REV006 M:24035=24160=24211

4 05 70 029 001 REV006 ALL 4 05 70 030 001 REV006

4 05 80 001 100 REV008 M:26497 ALL 4 05 80 002 200 REV007 CODE:0006

4 05 80 003 110 REV007 M:25863 ALL 4 05 80 004 100 REV008 M:25863

4 05 80 005 100 REV006 M:24035 OR 24160 OR 24211 ALL

4 06 00 001 001 REV013 CODE:0055 ALL

4 06 10 001 001 REV012 ALL 4 06 10 002 001 REV012

4 06 20 001 001 REV006 ALL 4 06 20 002 001 REV013

4 06 20 003 001 REV013 CODE 0071 ALL 4 06 20 004 001 REV013

R 4 06 20 005 001 REV013 STD=31579=31580=31896=31897 ALLR 4 06 20 006 001 REV014 CODE 0055

N 4 06 20 007 001 REV014 CODE 0064 ALLN 4 06 20 008 001 REV014 CODE:0055

4 06 40 001 001 REV012 ALL 4 06 40 002 001 REV010

4 07 00 001 001 REV006 CODE 0055 ALL

01 DEC 2002 CCM 4.00.80 PAGE 10

4 07 10 015 001 REV006 CODE 0055 ALL

01 DEC 2002 CCM 4.00.80 PAGE 11

318/319/320/321 FCOM VOLUME : 4 PILOT)S GUIDE LIST OF MOD/MP/SB AFFECTING THE MANUAL REVISION : 014

. 013A 23353 ...... AUTO FLIGHT - FMS - PROVIDE FMS CROSS ........... LOAD ALL

N 014 23593 ...... AUTO FLIGHT - MCDU 1 AND 2 - SOFTWARE ........... UPGRADED (CI-20) ALL

. 013A 24309 ...... AUTO FLIGHT - FMGC - PROVIDE TIME ........... CONSTRAINT AND TEN CHARACTERS RTE IDENT FUNCTIONS ALL

. 013A 24414 ...... AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU) ........... DELETE +EXPEDITE+ FUNCTION FROM FCU ALL

. 013A 24735 ...... AUTOFLIGHT-FCU- INTRODUCE MODIFIED ........... PIN/SOCKET CONNECTOR ON FCU WITH EXPEDITE FUNCTION DELETED (FCU BBM10) ALL

N 014 25025 ...... COMMUNICATIONS-INTERPHONE- ........... INTRODUCE IDENTIFICATION LABEL FOR INTERPHONE JACKS 1RJ/2RJ ALL

CCM 4.00.8501 DEC 2002 PAGE 1

N 014 25294 ...... NAVIGATION - ADIRS - INSTALL HONEYWELL ........... ADIRS CAPABLE OF A319 A/C ALL

. 013A 25295 ...... AUTOFLIGHT - FMGC - ACTIVATE ACARS ........... INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

. 013A 25345 ...... AUTOFLIGHT-FCU-INTRODUCE F.C.U. ........... STANDARD M11 ALL

. 013A 25346 ...... AUTOFLIGHT-FCU-INTRODUCE FCU ........... STANDARD M11 WITHOUT EXPEDITE FUNCTION ALL

. 013A 25381 ...... AUTOFLIGHT - FMGC - ACTIVATE PRINTER ........... INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

N 014 26495 ...... WINGS-INBOARD FLAP-MODIFY SLIDING PANEL ........... DRIVING MECHANISM ALL

. 013A 26497 ...... AUTO FLIGHT-GENERAL-ACTIVATE GLOBAL ........... SPEED PROTECTION AND F/D DISENGAGEMENT UPON SPEED CONSTRAINTS ALL

CCM 4.00.8501 DEC 2002 PAGE 2

. 013A 27256 ...... AUTO FLIGHT - MULTIPURPOSE CONTROL AND ........... DISPLAY UNIT (MCDU) - INTRODUCE MCDU HONEYWELL 2ND GENERATION (P/N -980) ALL

. 013A 27541 ...... AUTO FLIGHT - MCDU - INSTALL AN MCDU ........... 2ND GENERATION HONEYWELL FMS (MCDU WITH A340 KEYBOARD) ALL

N 014 28381 ...... ELECTRIC/ELECTRONIC COMMON INSTALLATION ........... - MODIFY CONNECTOR INTERFACE PLATE FOR ELECTRICAL CONVERTIBLE SEATS ALL

N 014 28495 ...... NAVIGATION - MMR - REMOVE COLLINS MMR ........... PROVIDING ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION (PREVIOUS SPEC.) OO-SSF

CCM 4.00.8501 DEC 2002 PAGE 3

CCM ALL

CCM MSN 1145

CCM ALL

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