@ A318/A319/A320/A321

@ A318/A319/A320/A321SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

5 DATE : May 05/04 SERVICE BULLETIN No. : A320—22—1152

REVISION No. : 03 — Feb 18/05 Page : 1 of 2

Printed in FRANCE © AIRBUS, 2005 All rights reserved

AIRBUSCUSTOMER SERVICES DIRECTORATE1 Rond Point Maurice Bellonte31707 BLAGNAC CEDEX FRANCETel : (33) 5 61 93 33 33Telex : AIRBU 530526FFax : (33) 5 61 93 42 51

ATA SYSTEM : 22

TITLE : AUTO FLIGHT - FMGC - INSTALL NEW THALES/SMITHS FMS2 (REV1+) C13043AA02WITH CFM ENGINES

MODIFICATION No. : 32475P7666 32475P7808 32997P7977 34078P8518

This page transmits Revision No. 03 of Service Bulletin No. A320-22-1152

ADDITIONAL WORK

No additional work is required by this revision for aircraft modified by anyprevious issue.

REASON

Revision No. 03 issued to remove aircraft MSN 1679 and 1753 for operatorCJG.

CHANGES

SUMMARY :

— EFFECTIVITY

. Operators updated.

— CONCURRENT REQUIREMENTS

. Paragraph updated.

PLANNING INFORMATION :

— EFFECTIVITY

. Para. 1.A. Aircraft model 319-111 deleted. Effectivity updated.

— CONCURRENT REQUIREMENTS

. Para. 1.B. Paragraph updated.

FILING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as acomplete document. Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.


REVISION TRANSMITTAL SHEET

DATE : May 05/04 SERVICE BULLETIN No. : A320—22—1152

REVISION No. : 03 — Feb 18/05 Page :


HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to add aircraft for operator TAR.

Revision No. 02 issued to add aircraft for operator USA.

REVISION SEQUENCE

ORIGINAL : May 05/04

REVISION No. : 01 — Jul 06/04REVISION No. : 02 — Oct 15/04REVISION No. : 03 — Feb 18/05

2


SUMMARY





This summary is for information onlyand is not approved for modification of the aircraft

ATA SYSTEM : 22



REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

This Service Bulletin is issued further to an operator's request in order toinstall new Flight Management and Guidance Computers (FMGCs).

This Service Bulletin replaces the two FMGCs PN B546CAM0103 or PN C13043AA01 bytwo new, mechanically interchangeable FMGCs PN C13043AA02, modified as perTHALES AVIONICS Service Bulletins No. B546CAM-22-009 and No. C13043A-22-002,which incorporate the second generation of Flight Management System (FMS), theso-called FMS2 THALES/SMITHS Rev1 S2C10 standard.

The following new functions have been incorporated in this new FMS2THALES/SMITHS Rev1 standard :

— Temporary F-PLN supporting multiple revisions and undo function

— Improved offset with customized intercept angle

— Wind interpolation

— Improved "DIR TO" activation display.

Furthermore, this new FMS standard is capable of managing Flight Management (FM)operational software and 5 data bases, and of independently data loading orcross loading in order to provide the operator with both flexibility andcustomization capabilities.

The data loading elements are the following :

— Navigation Data Base (NDB)

— FM selected set of options (FM Operational Program Configuration (OPC))

— FM Performance Data Base (PDB)

— Airline Modifiable Information (AMI)


SUMMARY




— Magnetic variation data base

— FM operational software.

As for Flight Guidance (FG) part, compared with pre-mod. standard, the followingevolutions and corrections have been incorporated :

— DIR TO/INTERCEPT capability

— Back beam approach and back course take off

— MACH/SPEED commutation in OPEN mode to avoid some situations of overspeed attransition

— Increase of speed protection authority in forward CG

— Improvement of A320/A321 Altitude (ALT*) and A320 ALT control laws to avoidsurface jerks

— Cancellation of thrust increase in case of overspeed below 150 ft whenAutopilot (AP) off

— Filtering of Localizer (LOC) and Glide/Slope (G/S) deviations to avoidspurious G/S capture in case of perturbation of Instrument Landing System(ILS) beam

— Improvement of G/S capture

— Approach lateral mode kept active upon longitudinal transition

— AP disconnection upon transmitter failure to be more alerting to the crew

— Improvement of speed target management at take off or go around

— Adjustment of A320 AP longitudinal basic loop authority in ALT mode.

— Flight Mode Annunciator (FMA)enhancement (option).

— Microwave Landing System (MLS) capability (option)

— Derated take-off capability (option).

Accomplishment of this Service Bulletin will satisfy the operator's request.

The operational consequences of this Service Bulletin are the substitution ofOEB 141, 143 and 144, or OEB 154 and 158 by OEB 157 and the modification of theFlight Manual (FM) and Flight Crew Operating Manual (FCOM) Vol. 1, 2, 3 and 4.

EVALUATION TABLE

COMPLIANCE Optional CANCELS INSPECTION SB No

POTENTIAL AD No A/C OPERATION AFFECTED Yes

2


SUMMARY




EFFECTIVITY

This Service Bulletin is applicable to these operators :

88Y ISS LBT TAR USA

NOTE : This Service Bulletin is written for the operators listed above. Themodification in this Service Bulletin can be done by other operators.

If other operators want to do this modification, use the RFC/RMOprocedure and write to :

AIRBUSCUSTOMER SERVICES DIRECTORATESC Department1 Rond Point Maurice Bellonte31707 BLAGNAC CEDEXFRANCE

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneousaccomplishment of the following Service Bulletins or the equivalent productionmodification:

Service Bulletin No. A320-22-1104 Mod. No. 32262P5486Service Bulletin No. A320-22-1148 Mod. No. 32766P7909

NOTE : Apply either Service Bulletin No. A320-22-1104 or Service Bulletin No.A320-22-1148 as per effectivity specified in these Service Bulletins.

Accomplishment of this Service Bulletin requires the prior or simultaneousaccomplishment of the following Service Bulletin(s) or the equivalent productionmodification(s):

Service Bulletin No. A320-22-1103 Mod. No. 32475P7666

Accomplishment of this Service Bulletin requires the prior or simultaneousaccomplishment of the following Service Bulletin or the equivalent productionmodification:


NOTE : Apply either Service Bulletin No. A320-22-1103 or Service Bulletin No.A320-22-1084 as per effectivity specified in these Service Bulletins.

RELIABILITY AFFECTED No PAX COMFORT AFFECTED No

COST SAVING No ETOPS AFFECTED No

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED Yes

KIT PRICE (USD) No kit

EVALUATION TABLE

3


SUMMARY




Accomplishment of this Service Bulletin requires the prior or simultaneousaccomplishment of the following Service Bulletin or the equivalent productionmodification:


NOTE : Accomplishment of this Service Bulletin also requires the simultaneousaccomplishment of the Service Bulletin which installs the appropriate OPCdisk (1CAMD1). The Operational Program Configuration file (OPC) is a disksoftware which activates, in the Flight Management Guidance Computer(FMGC), the various optional and standard functions purchased by theoperator.

REFERENCES/REPERCUSSIONS

TFU : NoneOEB : 141, 143, 144, 154, 157 and 158AOT : NoneSIL : NoneLIFE LIMIT : NoneLINE MAINTENANCE AFFECTED : NoOTHERS : None

NATURE OF THE WORK

AIRCRAFT : NoEQUIPMENT : YES

HARD : NOSOFT : YESOBRM : NO

MANPOWER

On aircraft

On bench

MATERIAL INFORMATION

AIRCRAFT DATA

TOTAL MANHOURS 3.5

ELAPSED TIME (HOURS) 3.5

TOTAL MANHOURS Refer to THALES AVIONICS ServiceBulletins No. B546CAM-22-009 andC13043A-22-002

ELAPSED TIME (HOURS) Refer to THALES AVIONICS ServiceBulletins No. B546CAM-22-009 andC13043A-22-002

4


SUMMARY




None

APPENDICES

None

5


SUMMARY




6






ATA SYSTEM : 22



This document contains AIRBUS PROPRIETARY INFORMATION and shall at all timesremain the property of AIRBUS; no intellectual property right or licence isgranted by AIRBUS in connection with any information contained in it. It isdelivered on the express condition that said document and the informationcontained in it shall be treated as confidential, shall not be used for anypurpose other than that for which it is hereby delivered. It shall not bedisclosed in whole or in part to third parties and shall not be duplicated inany manner (except for the purposes of performing the tasks described hereunderand provided that any recipient of such document shall comply with theconditions herein), without AIRBUS' prior written consent.

1. PLANNING INFORMATION

A. EFFECTIVITY

(1) Models

319-112 319-114 320-211 320-214 321-211

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft MSN :

0119 0123 0124 0205 0370 0390 0402 0511 0844 0861 0863 08680869 0880 0885 0890 0896 0904 0922 0929 0936 0946 0949 09580972 0975 0997 1019 1033 1038 1040 1044 1046 1048 1051 10521055 1061 1065 1069 1077 1084 1089 1095 1097 1102 1109 11121114 1121 1122 1134-1136 1141 1147 1148 1155 1170 1171 11751182 1187 1203 1205 1209 1210 1224 1245 1254 1263-1265 12681269 1275 1277 1283 1286 1287 1289 1294 1297 1298 1301 13051310 1311 1313-1315 1317 1319 1326 1328 1331 1340 1342 13481354 1358 1360 1369 1371 1378 1382 1389 1391 1393 1403 14121417 1425 1431 1436 1442 1447 1455 1462 1465 1472 1479 14811492 1496 1499 1517 1519 1521 1525 1531 1536 1539 1651 16661700 1701 1704 1724 1744 1769





NOTE : This Service Bulletin is only applicable to aircraft onwhich Mod. No. 20141P0115 (POWER PLANT - ENGINE -INSTALL CFM 56-5-A1 ENGINE RATED 25000LBS) is embodied.

(b) Effectivity by Operator

The Operator/MSN relationship is provided for information onlyand is correct at the time of issue in accordance with theinformation available to AIRBUS. Any future changes resultingfrom transfer of an aircraft from one operator to another willnot be reflected in this list unless the Service Bulletin isrevised for another reason.

(c) Effectivity by MSN and Kit/Configuration

No AIRBUS kit is required for the accomplishment of thisService Bulletin.

(3) Spares

FMGC B546CAM0103FMGC C13043AA01

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior orsimultaneous accomplishment of the following Service Bulletins or theequivalent production modification:

Service Bulletin No. A320-22-1104 Mod. No. 32262P5486Service Bulletin No. A320-22-1148 Mod. No. 32766P7909

OPERATOR MSN

88Y 1769

ISS 1048 1102 1283 1305

LBT 1121 1175 1744

TAR 0119 0123 0124 0205 0370 0390 0402 0511 0869 08800958 0975 1187 1479 1700

USA 0844 0861 0863 0868 0885 0890 0896 0904 0922 09290936 0946 0949 0972 0997 1019 1033 1038 1040 10441046 1051 1052 1055 1061 1065 1069 1077 1084 10891095 1097 1109 1112 1114 1122 1134 1135 1136 11411147 1148 1155 1170 1171 1182 1203 1205 1209 12101224 1245 1254 1263 1264 1265 1268 1269 1275 12771286 1287 1289 1294 1297 1298 1301 1310 1311 13131314 1315 1317 1319 1326 1328 1331 1340 1342 13481354 1358 1360 1369 1371 1378 1382 1389 1391 13931403 1412 1417 1425 1431 1436 1442 1447 1455 14621465 1472 1481 1492 1496 1499 1517 1519 1521 15251531 1536 1539 1651 1666 1701 1704 1724

2





NOTE : Apply either Service Bulletin No. A320-22-1104 or ServiceBulletin No. A320-22-1148 as per effectivity specified in theseService Bulletins.

Accomplishment of this Service Bulletin requires the prior orsimultaneous accomplishment of the following Service Bulletin(s) or theequivalent production modification(s):


Accomplishment of this Service Bulletin requires the prior orsimultaneous accomplishment of the following Service Bulletin or theequivalent production modification:


NOTE : Apply either Service Bulletin No. A320-22-1103 or ServiceBulletin No. A320-22-1084 as per effectivity specified in theseService Bulletins.

Accomplishment of this Service Bulletin requires the prior orsimultaneous accomplishment of the following Service Bulletin or theequivalent production modification:


NOTE : Accomplishment of this Service Bulletin also requires thesimultaneous accomplishment of the Service Bulletin whichinstalls the appropriate OPC disk (1CAMD1). The OperationalProgram Configuration file (OPC) is a disk software whichactivates, in the Flight Management Guidance Computer (FMGC), thevarious optional and standard functions purchased by theoperator.

C. REASON

(1) History

This Service Bulletin is issued further to an operator's request inorder to install new Flight Management and Guidance Computers(FMGCs).

(2) Objective/Action

This Service Bulletin replaces the two FMGCs PN B546CAM0103 or PNC13043AA00 by two new, mechanically interchangeable FMGCs PNC13043AA02, modified as per THALES AVIONICS Service Bulletins No.B546CAM-22-009 and No. C13043A-22-002, which incorporate the secondgeneration of Flight Management System (FMS), the so-called FMS2THALES/SMITHS Rev1 S2C10 standard.

(3) Advantages

The following new functions have been incorporated in this new FMS2THALES/SMITHS Rev1 standard :

3





— Temporary F-PLN supporting multiple revisions and undo function

— Improved offset with customized intercept angle

— Wind interpolation

— Improved "DIR TO" activation display.

Furthermore, this new FMS standard is capable of managing FlightManagement (FM) operational software and 5 data bases, and ofindependently data loading or cross loading in order to provide theoperator with both flexibility and customization capabilities.

The data loading elements are the following :

— Navigation Data Base (NDB)

— FM selected set of options (FM Operational Program Configuration(OPC))

— FM Performance Data Base (PDB)

— Airline Modifiable Information (AMI)

— Magnetic variation data base

— FM operational software.

As for Flight Guidance (FG) part, compared with pre-mod. standard,the following evolutions and corrections have been incorporated :

— DIR TO/INTERCEPT capability

— Back beam approach and back course take off

— MACH/SPEED commutation in OPEN mode to avoid some situations ofoverspeed at transition

— Increase of speed protection authority in forward CG

— Improvement of A320/A321 Altitude (ALT*) and A320 ALT controllaws to avoid surface jerks

— Cancellation of thrust increase in case of overspeed below 150 ftwhen Autopilot (AP) off

— Filtering of Localizer (LOC) and Glide/Slope (G/S) deviations toavoid spurious G/S capture in case of perturbation of InstrumentLanding System (ILS) beam

— Improvement of G/S capture

— Approach lateral mode kept active upon longitudinal transition

4





— AP disconnection upon transmitter failure to be more alerting tothe crew

— Improvement of speed target management at take off or go around

— Adjustment of A320 AP longitudinal basic loop authority in ALTmode.

— Flight Mode Annunciator (FMA)enhancement (option).

— Microwave Landing System (MLS) capability (option)

— Derated take-off capability (option).

Accomplishment of this Service Bulletin will satisfy the operator'srequest.

(4) Operational/Maintenance Consequences

The operational consequences of this Service Bulletin are thesubstitution of OEB 141, 143 and 144, or OEB 154 and 158 by OEB 157and the modification of the Flight Manual (FM) and Flight CrewOperating Manual (FCOM) Vol. 1, 2, 3 and 4.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(1) Modify the FMGCs 1CA1 and 1CA2 in the Aft Electronics Rack 80VU.

(2) Put the disk in the storage box.

E. COMPLIANCE

(1) Classification

Optional

(2) Accomplishment Timescale

In accordance with operators' maintenance schedule.

F. APPROVAL

Approved under the EASA Design Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repairembodied that is not of AIRBUS origin, and which affects the content ofthis Service Bulletin, the operator is responsible for obtainingapproval by its airworthiness authority for any adaptation necessarybefore incorporation of the Service Bulletin.

5





G. MANPOWER

The manpower estimates given in this Service Bulletin are based on thedirect labor cost to do the work. These estimates assume that the workwill be done by experienced personnel, and may need to be revisedupwards to suit operator's circumstances. The estimates do not includethe time to prepare, plan or inspect the work. Manufacture andprocurement of parts and tools, drying times for paints, sealants, etc,and general administration work are also not included.

On aircraft

On bench

H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

Service Bulletin No. A320-22-1084



Get access 0.5

Replace the FMGCs 0.5

Tests 2.0

Close-up 0.5

TOTAL MANHOURS 3.5

ELAPSED TIME (HOURS) 3.5

Modify the FMGCs --

TOTAL MANHOURS Refer to THALES AVIONICSService Bulletins No.

B546CAM-22-009 andC13043A-22-002

ELAPSED TIME (HOURS) Refer to THALES AVIONICSService Bulletins No.

B546CAM-22-009 andC13043A-22-002

Aircraft Maintenance Manual (AMM) : 22-10-00 22-83-34 22-96-0022-97-00 24-41-00

Elec. Std. Practices Manual (ESPM) : 20-55-00

6







THALES AVIONICS Service Bulletin No. B546CAM-22-009

THALES AVIONICS Service Bulletin No. C13043A-22-002

K. PUBLICATIONS AFFECTED

This Service Bulletin has an operational impact. Please inform AIRBUS,at least four weeks in advance, in case you need your operationaldocumentation to be amended by an intermediate revision prior to SBembodiment. For this purpose, please request the intermediate revisionby fax, telex or mail to :

SDC3, AIRBUS - Customer Services DirectorateFax No. 33 (0) 5 61 93 28 06Sita No. TLSBP7XE-mail [email protected]

These amendments will be confirmed by the next normal revision ofoperational documentation, once your Service Bulletin accomplishmentreport has been sent, as usual, to our Customer Services Directorate(SDC3).

L. INTERCHANGEABILITY/MIXABILITY

NOTE : For definitions of interchangeability codes in column INT. referto ATA Common Support Data Dictionary (CSDD), chapter 2.

NOTE (01) Not authorized. Replacement of the two FMGCs has to be donesimultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph B.of this Service Bulletin.

NOTE (02) Only the mixability configuration(s) and condition (s) statedin this Service Bulletin are approved.

Aircraft Wiring Lists (AWL)

Flight Crew Operating Manual (FCOM) : Vol. 1 Vol. 2 Vol. 3Vol. 4

Illustrated Parts Catalog (IPC) : 22-83-34 22-84-08

Flight Manual (FM)

DESCRIPTION OLD PART No. NEW PART No. INT MIXABILITY

FMGC B546CAM0103C13043AA01

C13043AA02 03 NOTES (01)(02)

7





This Page Intentionally Left Blank

8





2. MATERIAL INFORMATION

A. MATERIAL — PRICE AND AVAILABILITY

(1) Material

See list of Materials - Operator Supplied.

(2) Price and Availability

Sales terms must be agreed between the Customers and AIRBUS inaccordance with the RFC (or RFC/RMO) procedure.

B. INDUSTRY SUPPORT INFORMATION

Refer to paragraph 2.A.(2): Price and Availability.

C. LIST OF COMPONENTS

None

D. LIST OF MATERIALS — OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

NOTE : For definitions of interchangeability codes in column INT.refer to ATA Common Support Data Dictionary (CSDD), chapter2.

NOTE (01) Modification of removed equipment should be negotiateddirectly with THALES as per instructions given in ServiceBulletins No. B546CAM-22-009 and No. C13043B-22-002.

NOTE (02) After the uploading, the FMGC software PNs are :

— Perf database PN 553167-02-01 (Disk F1420035)

— Operational soft PN G2604AAA02 (Disk F1420265)

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

C13043AA02 2 FMGC B546CAM0103C13043AA01

03 (01)

F1420035 1 Disk (01)(02)

F1420059 1 Disk (01)(02)

F1420265 1 Disk (01)(02)

9





— Mag var database PN G1748AAA01 (Disk F1420059)

— Basic PN G8274AAA01 for OPC.

E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR

None

F. TOOLING — PRICE AND AVAILABILITY

None

G. SPECIAL TOOLS

None

10





3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.

CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY ANDMECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK,REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICALY WIRING,COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS:

— PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., ASNECESSARY ON WIRING AND COMPONENTS

— REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHERCONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

(1) Preparation

(a) Do the preparation procedure as specified in theremoval/installation of the FMGCs (1CA1, 1CA2), (Refer to AMM22-83-34 Page block 401).

(2) Standard Practices

None

B. MODIFICATION

NOTE : For the modification of the FMGCs 1CA1 and 1CA2, refer to THALESAVIONICS Service Bulletin No. B546CAM-22-009 and ServiceBulletin No. C13043A-22-002 .

(1) Modify the FMGCs 1CA1 and 1CA2 in the Aft Electronics Rack 80VU(Refer to AMM 22-83-34 Page block 401)

(a) Remove :

or

(b) Install :

2 FMGC B546CAM0103

2 FMGC C13043AA01

2 FMGC C13043AA02

11





NOTE : The FMGCs are preloaded with the softwares embodied inthese disks :

(2) Put the disk in the storage box.

C. TEST

(1) Job Set-up

(a) Energize the aircraft electrical circuits, (Refer to AMM24-41-00 Page block 201).

(b) Make sure that this(these) circuit breaker(s) is(are) closed :

(c) Make sure that the aircraft is in the ground configuration.

(d) On the MCDU, on the applicable PN status page(s), do a checkof the PN of the element(s) (pre-loaded in the related FMGC)(use the line select key adjacent to the NEXT PAGE or PREVPAGE indication)

NOTE : You must do this check because if the elements that youcan load are not correct, the FMGC will not accept theloading.

On the applicable PN STATUS page, make sure that theseelements are in the FMGC :

— The FM operational software with the FMS operationalprogram disk (1CAMD3) (Page 2 : FMS SOFTWARE)

NOTE : If the FMS software does not agree with the FGsoftware, the INCOMPATIBLE message is shown.

— The navigation data base with the active nav database disk (Page 3: NAV DATA BASE)

1 Disk F14200591 Disk F14200351 Disk F1420265

PANEL DESIGNATION FIN LOCATION

49VU AUTO FLT/FMGC/1 10CA1 02 B121VU AUTO FLT/FMGC/2 10CA2 17 M49VU AUTO FLT/MCDU/1 11CA1 01 B121VU AUTO FLT/MCDU/2 11CA2 20 N121VU AUTO FLT/MCDU/2 11CA2 19 N49VU L/G/LGCIU/SYS1/NORM 1GA 11 C49VU L/G/LGCIU/SYS1/NORM 1GA 09 C121VU DATA/LOADER/SPLY 3TD 16 J121VU DLS&/DLRB/SPLY 5TD 15 J

12





— The AMI file with the applicable disk (Page 4 : FMAIRLINE CONFIG (AMI))

— The OPC file with FMS option configuration disk(1CAMD1) (Page 5 : FM OPTION CONFIG (OPC))

— The performance data base with the FMS performancedata base disk (1CAMD2) (Page 6 : PERF DATA BASE)

— The magnetic variation data base with the applicabledisk (1CAMD4) (Page 7 : MAG VAR DATA BASE).

NOTE : The loading of the FM operational software erases theother elements.

NOTE : The selection of an MCDU FM mode key on the side of theMCDU is ignored and results in the display of NOTALLOWED scratchpad message while it is necessary toload the mandatory elements or the FM software does notagree with the FG software.

1 Do the check of the PN of the elements

(2) TestsIf an uploading procedure is necessary to modify the pre-loadedelements, do this procedure. If not, refer to ACCOMPLISHMENTINSTRUCTIONS paragraph C.(2)(b).

(a) Procedure

1 Uploading of the FMGC

ACTION RESULT

1. On the MCDU :— Adjust the display intensity withthe BRT control

— Push the DATA mode key.

2. On the MCDU :— Push the line key adjacent to theA/C STATUS indication.

On the MCDU :— The A/C STATUS page comes into view.

3. On the A/C STATUS page :— Push the line key adjacent to theSOFTWARE STATUS/XLOAD indication.

On the MCDU :— The PN STATUS page comes into view.

4. Before you do the uploadingprocedure, on the PN STATUS page :— Read the PN of the element that youcan load

— Make sure that this PN is not thesame as the PN reference on thedisk. If it is the same, theuploading is not necessary.

13





NOTE : The uploading time for one full disk is ten minutesapproximately.

NOTE : After the uploading operations, you must do a checkof the reference of the data loaded in the FMGC, onthe MCDU.

NOTE : The uploading procedure that follows is for theFMGC1. For the FMGC2 procedure, which is the same,refer to the data in parentheses.

ACTION RESULT

1. On the overhead panel, on the dataloading selector :

On the display of the data loadingselector :

— Set the ON/OFF switch to ON. — DB/NPUSH NEXT/PREVindication is shown.

On the MDDU :

— The "MDDU READY" indication isshown.

2. On the overhead panel :

— Open the circuit breakers 10CA1 and10CA2.

3. On the data loading selection : On the display of the data loadingselector :

— Push the PREV or NEXT key until youget the indication of the FMGC thatyou can load

— FMGC1 (2)NOT SELECTEDindication is shown.

— Push the SEL CTL key. — FMGC1 (2)SELECTEDindication is shown.

4. Use the applicable disk(s) from thedisk storage box.

5. On the MDDU : On the MDDU :

— Put the disk into the disk drive. — The READY indication comes into view— Then, the WAIT RESPONSE indicationcomes into view.

6. On the overhead panel : On the MDDU :

— Close the circuit breaker 10CA1(10CA2).

— The READY indication comes into view— Then, the WAIT RESPONSE indicationcomes into view and, immediatelyafter, the TRANSF IN PROG indicationcomes into view

— The BUS n : xxxxxxx indication isshown after the FMGC safety test.

14





2 Do a check of the reference of the software loaded in theFMGC, on the MCDU :

a Make sure that the PN XLOAD 1/7 page is shown on theMCDU :

NOTE : "n" is the number of the bus (1to 8) in transfer."xxxxxx" is the number ofremaining bytes.The uploading is completed onlywhen TRANSF COMPLETE indicationis shown.

NOTE : If more than one disk isnecessary for the uploading,the EJECT DISK and INSERT NEXTDISK indications show one afterthe other. They tell theoperator to put a new disk intothe MDDU.

— When all the disks are loaded in theFMGC, the TRANSF COMPLETE indicationcomes into view.

7. On the MDDU : On the MDDU :

— Eject the disk from the disk drive. — The "MDDU READY" indication comesinto view.

8. On the overhead panel, on the dataloading selector :

On the display of the data loadingselector :

— Push the SEL CTL key. — FMGC1 (2)NOT SELECTEDindication is shown.

9. Open (for more than 5 seconds) thecircuit breaker 10CA1 (10CA2).

10. Do the procedure again (step 3 to9) for the FMGC2 with the data betweenparentheses.

11. On the data loading selector :

— Set the ON/OFF switch to OFF.

12. Close the circuit breakers 10CA1and 10CA2, and wait for the FMGCsafety test.

13. When the safety test of the FMGCsis completed, do the check thatfollows.

ACTION RESULT

15





(b) Do these tests

1 On the center pedestal, on the MCDU related to the replacedFMGC :

— Adjust the intensity of the MCDU screen

— Push the DATA mode key to obtain the DATA INDEX page

— Push the line key adjacent to the A/C STATUS indication

— Make sure that the IDLE/PERF value is the same as thevalue you wrote during the removal. If not :

. Record ARM into brackets in the CHG CODE line (5L),

. Write the IDLE/PERF value in the scratchpad,

. Record this value in line (6L).

2 Do the AFS test, (Refer to AMM 22-96-00 Page block 501).

NOTE : As an alternative, you can do this operational testwithout the CFDS, (Refer to AMM 22-10-00 Page block501).

NOTE : If the aircraft is operated in CAT3 conditions, youmust also do the LAND CAT3 capability test, (Referto AMM 22-97-00 Page block 501).

(3) Close-up

(a) Put the aircraft back to its initial configuration.

(b) On the MCDU, push the MCDU MENU key to get the MCDU MENU page.

(c) Put the disk in the storage box.

D. CLOSE UP

(1) Do the close-up procedure as specified in the removal/installationof the FMGCs (1CA1, 1CA2), (Refer to AMM 22-83-34 Page block 401).

ACTION RESULT

1. On the MCDU : On the MCDU :

— Get the page related to the loadedelement (use the line select keyadjacent to the NEXT PAGE or PREVPAGE indication).

— Make sure that the reference (PN)shown is the same as the referenceon the disk(s).

16





E. DOCUMENTATION

Write in the applicable aircraft records that you have done all the workgiven in the Service Bulletin.

17

@ A318/A319/A320/A321SERVICE BULLETINREPORTING SHEET






Please complete the appropriate item (A or B):

A - SB WILL BE embodied . . . . . . . . . . . . . YES/NO (if NO please comment)If YES, aircraft concerned (as per SB effectivity by default) and planned dates(month/year) of embodiment: . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

B - SB HAS BEEN embodied on aircraft: . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Operator comments: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

From Airline: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Name/Title: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Signature: . . . . . . . . . . . . . . Date: . . . . . . . . . . . . .

If operational documentation is affected (see Paragraph 1.K of this SB): Ifinformation is needed prior to next normal revision or prior to SB embodiment,please indicate required service(s):Either: Advance Data . . . . . . . . . . . . . . . . . . . . . YES/NOOr : Intermediate/Temporary revision. . . . . . . . . . . . YES/NO

Important Information: This SB will only be incorporated in your maintenance andoperational documentation if this sheet is returned to Airbus and signed by aduly authorised representative. With the next feasible revision, this willresult in

- updating of maintenance documentation to show pre and post SB data.- updating of maintenance and operational documentation to show post SB dataafter embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs,Airbus shall automatically include them in the manual revisions. Refer to SIL00-037 for detailed information.

Please return this completed sheet to:

AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.


QUALITY PERCEPTION FORM




Use this form to tell us what is your perception of the quality of this ServiceBulletin. The reported data that you provide us will be used to analyse areas ofdifficulties and to take corrective action to further improve the quality of ourService Bulletins.We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- Is this SB easy to understand ? Y / N

If you have had difficulties in the accomplishment of this SB please quote belowthe area(s) and give a short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X PreparationX Reason X List of Materials X Mod/InspectionX Manpower Operator Supplied X TestX References X Re-identification X Close-UpX Publication X Tooling X Illustrations

Comments :

Operator : Date:

Name/Title :

Please return this form to :

AIRBUSCUSTOMER SERVICES DIRECTORATE1 Rond Point Maurice Bellonte31707 BLAGNACAttn : SET1 Service Bulletins ManagementFAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

Documents

@ A318/A319/A320/A321