@ a318/a319/a320/a321 - regulations.gov

@ A318/A319/A320/A321SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

5 DATE : Oct 08/02 SERVICE BULLETIN No. : A320—22—1103

REVISION No. : 04 — Mar 12/04 Page : 1 of 2

Printed in FRANCE © AIRBUS, 2004 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 FMGC CFM C13043AA01 (EQUIPPED WITH FMS2THALES/SMITH REV 01)

MODIFICATION No. : 32475P7666 32475P7808

This page transmits Revision No. 04 of Service Bulletin No. A320-22-1103

ADDITIONAL WORK

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

REASON

Revision No. 04 issued to add aircraft MSN 1102, 1283 and 1305 for operatorD2F, and aircraft MSN 1048 for operator F2I.

CHANGES

SUMMARY :

— EFFECTIVITY

. Operators updated.

— CONCURRENT REQUIREMENTS

. Service Bulletin A320-22-1148 and NOTE added.

PLANNING INFORMATION :

— EFFECTIVITY

. Para. 1.A. Effectivity updated.

— CONCURRENT REQUIREMENTS

. Para. 1.B. Service Bulletin A320-22-1148 and NOTE added.

— REFERENCES

. Para. 1.J. Service Bulletin A320-22-1148 added.


REVISION TRANSMITTAL SHEET

DATE : Oct 08/02 SERVICE BULLETIN No. : A320—22—1103

REVISION No. : 04 — Mar 12/04 Page :


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.

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to add aircraft for operator AFR and THALES AVIONICSService Bulletin No. B546CAM-22-009.

Revision No. 02 issued to add aircraft for operators AFR, NWA and includesome minor corrections in the test.

Revision No. 03 issued to add aircraft for operators AFR, NWA and S2A.

REVISION SEQUENCE

ORIGINAL : Oct 08/02

REVISION No. : 01 — Apr 01/03REVISION No. : 02 — Aug 28/03REVISION No. : 03 — Oct 15/03REVISION No. : 04 — Mar 12/04

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 published to advise all operators of A319/A320/A321aircraft of the issue of THALES AVIONICS Service Bulletin No. B546CAM-22-009.

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 by two newmechanically interchangeable FMGCs PN C13043AA01, which incorporate the secondgeneration of Flight Management System (FMS), the so-called FMS2 THALES/SMITHSRev1 standard.

EFFECTIVITY

This Service Bulletin is applicable to these operators :

57Y AFR AZA D2F F2I FFT NWA

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

EVALUATION TABLE

COMPLIANCE Optional CANCELS INSPECTION SB No

POTENTIAL AD No A/C OPERATION AFFECTED Yes

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


SUMMARY




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

AIRBUSCUSTOMER SERVICES DIRECTORATEAI/SC Department1 Rond Point Maurice Bellonte31707 BLAGNAC CEDEXFRANCE

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneousaccomplishment of the following Service Bulletin, except for aircraft havingequivalent production Mod. No. 32766P7909 (AUTO FLIGHT - MCDU - INSTALL NEWTHALES MCDU FOR FMS2 (RETROFIT ONLY)) and Mod. No. 32262P5486 (AUTO FLIGHT -MULTIPURPOSE CONTROL AND DISPLAY UNIT (MCDU) - INSTALL MCDU THALES 2NDGENERATION) embodied :

Service Bulletin No. A320-22-1104Service Bulletin No. A320-22-1148

NOTE : Apply either Service Bulletin A320-22-1104 or Service BulletinA320-22-1148 as per effectivity specified in these Service Bulletins.

Accomplishment of this Service Bulletin requires the prior or simultaneousaccomplishment of the following Service Bulletin, except for aircraft havingequivalent production Mod. No. 31365P6987 (AUTO-FLIGHT - FMGC - INSTALL FMGC PNB546CAM0103 (CFM GPS/ACARS)) embodied :

Service Bulletin No. A320-22-1084

Accomplishment of this Service Bulletin requires the prior or simultaneousaccomplishment of the following Service Bulletin, except for aircraft havingequivalent production Mod. No. 28308P5567 (INDICATING RECORDING SYSTEM - DMC -INTRODUCE DMC V40 STANDARD) embodied :


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 (andEnvelope) Computer (FMG(E)C), the various optional and standard functionspurchased by the operator.

REFERENCES/REPERCUSSIONS

TFU : NoneOEB : OEB 144 cancelledAOT : NoneSIL : NoneLIFE LIMIT : NoneLINE MAINTENANCE AFFECTED : No

2


SUMMARY




OTHERS : None

NATURE OF THE WORK

AIRCRAFT : NoEQUIPMENT : YES

HARD : NOSOFT : YESOBRM : NO

MANPOWER

On aircraft

On bench

MATERIAL INFORMATION

AIRCRAFT DATA

None

APPENDICES

None

TOTAL MANHOURS 3.5

ELAPSED TIME (HOURS) 3.5

TOTAL MANHOURS Refer to THALES AVIONICS ServiceBulletin No. B546CAM-22-009

ELAPSED TIME (HOURS) Refer to THALES AVIONICS ServiceBulletin No. B546CAM-22-009

3






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

319-111 319-112 319-113 319-114 320-111 320-211 320-212 320-214321-111 321-211

NOTE : This Service Bulletin is only applicable to aircraftequipped with CFM56 engines.

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft MSN :

0002-0005 0007 0010 0012-0014 0016 0019-0021 0031-0034 00360040 0041 0044 0060-0063 0100-0102 0106-0108 0115 0118 01210125 0128-0131 0133 0144 0145 0152 0153 0155 0156 0160 01710184 0186-0188 0192 0197 0203 0204 0206 0208 0211 0213-02150220 0226-0228 0235-0237 0239 0244 0262 0263 0270 0272 02730278 0281 0282 0285-0287 0297 0298 0306 0307 0318 0319 03290337 0339 0340 0352 0355 0358 0360 0367 0372 0377 0380 03810387 0388 0399 0400 0408 0410 0417 0418 0491 0498 0509 05210529 0544 0598 0600 0608 0618 0625 0637 0644 0647 0660 07660777 0778 0786 0796 0801 0807 0818 0830 0832 0846 0903 09070911 0923 0938 0956 0962 0964 0981 0985 0988 0996 0998 1000





1011 1020 1025 1036 1037 1048 1058 1062 1071 1078 1090 10911102 1126 1129 1131 1133 1149 1151 1164 1167 1169 1176 11901191 1201 1216 1230 1249 1267 1271 1283 1299 1305 1324 13251344 1346 1392 1404 1414 1415 1434 1444 1449 1453 1456 14711476 1483 1488 1494 1498 1501 1502 1505 1515 1520 1524 15351543 1549 1560 1567 1570 1579 1582 1583 1616 1622 1633 16401641 1645 1646 1658 1659 1662 1677 1683-1685 1691 1693 16991709 1714 1722 1733 1738 1740 1743 1745 1746 1752 1759 17611770 1779 1781 1789 1803 1859 1873 1879 1885 1894 1900 19241938 1949

(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.

OPERATOR MSN

57Y 1494

AFR 0002 0003 0004 0005 0007 0010 0012 0013 0014 00160019 0020 0021 0033 0036 0044 0061 0062 0063 01000101 0102 0108 0115 0128 0129 0130 0131 0133 01440145 0155 0156 0184 0186 0187 0188 0203 0204 02110214 0215 0220 0226 0227 0228 0235 0236 0237 02390244 0270 0278 0285 0286 0287 0337 0352 0377 04910498 0509 0521 0529 0544 0598 0600 0608 0618 06250637 0644 0647 0660 0777 0796 0938 0956 0985 09981000 1020 1025 1036 1133 1151 1169 1176 1190 12011216 1267 1271 1299 1344 1404 1415 1444 1449 14711476 1502 1505 1524 1616 1622 1640 1645 1658 16771691 1699 1733 1859 1873 1879 1885 1894 1900 19241938 1949

AZA 1722 1740 1745 1770 1779

D2F 1102 1283 1305

F2I 1048

2





(c) Effectivity by MSN and Kit/Configuration

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

(3) Spares

FMGC B546CAM0103

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior orsimultaneous accomplishment of the following Service Bulletin, exceptfor aircraft having equivalent production Mod. No. 32766P7909 (AUTOFLIGHT - MCDU - INSTALL NEW THALES MCDU FOR FMS2 (RETROFIT ONLY)) andMod. No. 32262P5486 (AUTO FLIGHT - MULTIPURPOSE CONTROL AND DISPLAY UNIT(MCDU) - INSTALL MCDU THALES 2ND GENERATION) embodied :

Service Bulletin No. A320-22-1104Service Bulletin No. A320-22-1148

NOTE : Apply either Service Bulletin A320-22-1104 or Service BulletinA320-22-1148 as per effectivity specified in these ServiceBulletins.

Accomplishment of this Service Bulletin requires the prior orsimultaneous accomplishment of the following Service Bulletin, exceptfor aircraft having equivalent production Mod. No. 31365P6987(AUTO-FLIGHT - FMGC - INSTALL FMGC PN B546CAM0103 (CFM GPS/ACARS))embodied :


Accomplishment of this Service Bulletin requires the prior orsimultaneous accomplishment of the following Service Bulletin, exceptfor aircraft having equivalent production Mod. No. 28308P5567

FFT 1488 1515 1560 1579 1583 1684 1743 1759 1761 17811803

NWA 0031 0032 0034 0040 0041 0060 0106 0107 0118 01210125 0152 0153 0160 0171 0192 0197 0206 0208 02130262 0263 0272 0273 0281 0282 0297 0298 0306 03070318 0319 0329 0339 0340 0355 0358 0360 0367 03720380 0381 0387 0388 0399 0400 0408 0410 0417 04180766 0778 0786 0801 0807 0818 0830 0832 0846 09030907 0911 0923 0962 0964 0981 0988 0996 1011 10371058 1062 1071 1078 1090 1091 1126 1129 1131 11491164 1167 1191 1230 1249 1324 1325 1346 1392 14141434 1453 1456 1483 1498 1501 1520 1535 1543 15491567 1570 1582 1633 1641 1646 1659 1662 1683 16851693 1709 1714 1738 1746 1752 1789

OPERATOR MSN

3





(INDICATING RECORDING SYSTEM - DMC - INTRODUCE DMC V40 STANDARD)embodied :


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 (and Envelope)Computer (FMG(E)C), the various optional and standard functionspurchased by the operator.

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 is published to advise all operators ofA319/A320/A321 aircraft of the issue of THALES AVIONICS ServiceBulletin No. B546CAM-22-009.

This Service Bulletin replaces the two FMGCs PN B546CAM0103 by twonew mechanically interchangeable FMGCs PN C13043AA01, whichincorporate the second generation of Flight Management System(FMS), the so-called FMS2 THALES/SMITHS Rev1 standard.

(3) Advantages

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 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)

4





— 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

— 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.

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

(4) Operational/Maintenance Consequences

The operational consequences of this Service Bulletin are thecancellation of OEB 144, and the modification of Flight CrewOperating Manual (FCOM) Vol. 1, 2, 3 and 4, and of Flight Manual(FM) chapter 2.

5





D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

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

E. COMPLIANCE

(1) Classification

Optional

(2) Accomplishment Timescale

In accordance with operators' maintenance schedule.

F. APPROVAL

The technical content of this Service Bulletin has been approved underthe authority of the DGAC Design Organisation Approval No. F.JA.02.

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.

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

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 --

6





H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES





THALES AVIONICS Service Bulletin No. B546CAM-22-009

K. PUBLICATIONS AFFECTED

This Service Bulletin has an operational impact. You are thereforerequested to inform AIRBUS, at least four weeks in advance, of yourintention to accomplish this Service Bulletin, in order to receiverequired amendments to your operational documentation. For this purpose,please send a fax, telex or mail to :

AI/SE-D, AIRBUS - Customer Services DirectorateFax No. (33) 5 61 93 28 06Sita No. TLSBP7XE-mail [email protected]

TOTAL MANHOURS Refer to THALES AVIONICSService Bulletin No.

B546CAM-22-009

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

B546CAM-22-009

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

Aircraft Wiring Lists (AWL)

Flight Crew Operating Manual (FCOM) : 1-22 1-31 2-04 3-01 3-023-03 4-02 4-03 4-04 4-054-06 4-07

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

Flight Manual (FM) : Chapter 2

7





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(SE-D).

L. INTERCHANGEABILITY/MIXABILITY

NOTE : For definitions of interchangeability codes shown in column INT.refer to ATA 200 Chapter 1A-2.

NOTE (01) Not authorized. Replacement of both 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.

DESCRIPTION OLD PART No. NEW PART No. INT MIXABILITY

FMGC B546CAM0103 C13043AA01 01 NOTES (01)(02)

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 shown in columnINT. refer to ATA 200 Chapter 1A-2.

NOTE (01) Modification of removed equipment should be negotiateddirectly with THALES AVIONICS as written in the ServiceBulletin B546CAM-22-009.

NOTE (02) The operator must get this equipment from :

THALES AVIONICSAir Transport Avionics105, Avenue du General EisenhowerBP 1147 - 31036 TOULOUSE CEDEX 1FRANCE

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

C13043AA01 2 FMGC B546CAM0103 01 (01)F1420033 1 Disk (02)

(03)F1420035 1 Disk (02)

(03)F1420059 1 Disk (02)

(03)

9





NOTE (03) After the uploading, the FMGC software PNs are :

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

— Operational soft PN G2604AAA01 (Disk F1420033)

— 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

— REGULARY 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, CLEANING.

(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 CA2, refer to THALESAVIONICS Service Bulletin No. B546CAM-22-009 .

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

(a) Remove :

(b) Install :

(c) The FMGCs are loaded with these disks :

2 FMGC B546CAM0103

2 FMGC C13043AA01

1 Disk F14200591 Disk F14200351 Disk F1420033

11





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)

— 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)

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 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

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.

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 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.

@ a318/a319/a320/a321 - regulations.gov

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