C@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

ATA SYSTEM: 31

TITLE: INDICATING / RECORDING SYSTEMS - FLIGHT WARNING COMPUTER

(FWC) - INSTALL FWC STANDARD T2-0.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 56729S19417

MINOR 51926S17857 58440S30619

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

This Service Bulletin is published to advise all operators of A330 aircraft of the issue of AIRBUS

FRANCE SAS Service Bulletin No. LA2E2-31-007 and the issue of AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008.

This Service Bulletin has been issued to install a new Flight Warning Computer (FWC) standard T2-0

with 486 based Central Processing Unit (CPU) board on A330 aircraft model.

This Service Bulletin proposes the replacement of the following computer :

- Two AIRBUS FRANCE SAS FWCs P/N LA2E0060D8K0000 standard K8-1 (installed by Mod. No.

56069S18891 (INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) -

INSTALL FWC STANDARD K8-1) with 386 based CPU board

- Or two AIRBUS FRANCE SAS FWCs P/N LA2E20202T10000 standard T1-0 (installed by Mod. No.

55982S18817 (INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) -

INSTALL FWC STANDARD T1) with 486 based CPU board

- By two AIRBUS FRANCE SAS FWCs P/N LA2E20202T20000 standard T2-0 with 486 based CPU

board electrically and mechanically interchangeable.

This new standard is obtained either by

- Replacement of the FWCs

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 1

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C@A330

SERVICE BULLETIN

SUMMARY

- Or by replacement or reprogramming of the On-Board Replaceable Modules (OBRMs), from T1-0

standard only.

Accomplishment of this Service Bulletin will improve the operating performance of the FWCs.

From FWC K8-1/386 standard, the main improvements are the following :

- Improvement of the smoke procedure,

- New "PARK BRAKE ON" alert in flight,

- New auto call-outs 60ft and 70ft (activated by separate pin programming),

- New "Air Data Reference (ADR) monitoring" functions and alerts,

- FLS/GLS compatibility,

- PAX system function (activated by separate pin programming),

- CBB or TV system integration,

- Consolidation of slats/flaps configuration monitoring for take off,

- Tail strike detection system capability,

- Head Up Display (HUD) installation capability,

- New audio board with data-loading capability from the OBRM,

- New 486 CPU board,

- Intermediate Pressure Turbine Overspeed System (IPTOS) monitoring for RR engines,

- New Autopilot/Flight Director Traffic "AUTO FLT TCAS MODE FAULT" Alert and Collision

Avoidance System mode (AP/FD TCAS) monitoring capability,

- Landing Gear Well Surveillance System (LGWSS) installation capability with new "L/G SURV

INTRUSION DET" alert,

- Fuel Tank Inerting System (FTIS) installation capability with new "FUEL INERTING SYS FAULT"

alert,

- AOA monitoring with new "NAV AOA DISAGREE" alert (minimum FCDC standard required),

- Cabin Intercommunication Data System with integrated Smoke Detection Function (CIDS-SDF)

installation capability,

- New engine Feedline burst monitoring capability with "ENG 1 (2) FEEDLINE BURST" alert

(requires pin-programming),

- Monitoring of throttles lever position during landing with new "ENG 1 (2) THR LEVER ABV IDLE"

red alert,

- Icing condition procedure for RR engines with new "ENG RISK OF STATOR ICING" alert,

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 2

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C@A330

SERVICE BULLETIN

SUMMARY

- Deletion of procedure linked to "NAV TCAS FAULT" alert to avoid unintentional switching off of

transponder,

- New monitoring for 64CK and 70K PW engine installation capability,

- ALNAv2 network services system installation capability,

- ADS-B/ATSAW function installation capability,

- New "NAV HUD FPV DISCREPANCY" alert linked to HUD monitoring.

From FWC T1/486 the main improvements are the following :

- New Autopilot/Flight Director Traffic "AUTO FLT TCAS MODE FAULT" Alert and Collision

Avoidance System mode (AP/FD TCAS) monitoring capability,

- Landing Gear Well Surveillance System (LGWSS) installation capability with new "L/G SURV

INTRUSION DET " alert,

- Fuel Tank Inerting System (FTIS) installation capability with new "FUEL INERTING SYS FAULT"

alert,

- AOA monitoring with new "NAV AOA DISAGREE" alert (minimum FCDC standard required),

- Cabin Intercommunication Data System with integrated Smoke Detection Function (CIDS-SDF)

installation capability,

- New engine feedline burst monitoring capability with "ENG 1 (2) FEEDLINE BURST" alert (requires

pin-programming),

- Monitoring of throttle lever position during landing with new "ENG 1 (2) THR LEVER ABV IDLE" red

alert,

- Icing condition procedure for RR engines with new "ENG RISK OF STATOR ICING" alert,

- Deletion of procedure linked to "NAV TCAS FAULT" alert to avoid unintentional switching off of

transponder,

- New monitoring for 64CK and 70K PW engine installation capability,

- ALNAv2 network services system installation capability,

- ADS-B/ATSAW function installation capability,

- New "NAV HUD FPV DISCREPANCY" alert linked to HUD monitoring.

The operational/maintenance consequence of this Service Bulletin are the modification of the Flight

Crew Operating Manual (FCOM) VOL 1 and 3 and cancels Operating Engineering Bulletin (OEB) No.

61, 68 and 69.

Operators having programmed an OEB reminder should delete the reminder(s) from their system.

NOTE: For a full improvement description, refer to MOI No. 56729.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 3

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C@A330

SERVICE BULLETIN

SUMMARY

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED 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

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

BFE Equipment

BFEA01

See SB See SB FWC

COMP Component

COMPA01

See SB See SB Contacts

**CONF 002

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

BFE Equipment

BFEA01

See SB See SB FWC

COMP Component

COMPA02

See SB See SB Contacts

**CONF 003

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

BFE Equipment

BFEA01

See SB See SB FWC

COMP Component

COMPA01

See SB See SB Contacts

**CONF 004

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

BFE Equipment

BFEA01

See SB See SB FWC

COMP Component

COMPA01

See SB See SB Contacts

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 4

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C@A330

SERVICE BULLETIN

SUMMARY

EFFECTIVITY

**CONF ALL

This Service Bulletin is applicable to this (these) operator(s) :

10V 46W 78V 99Y AAR ACA ACI ADH AEA AFR ALK ASY AVA

BEL BMA CAL CCA CES CHH CPA CRL CSN CYP DAH DLH EDW

EEZ EIN ETD EVA FWI GFA GIA GRL HDA HFY HVN IAC ISR

IWD IYE JAI JST KAL KFR KLM LTU LVG MAS MAU MEA MON

MPD MSR NWA OBS PAL QAF QFA QTR RSF SAS SWR TAM TAP

TCX THA THY TSC UAE UAF USA VKG XAX XLF

CONCURRENT REQUIREMENTS

**CONF 001 thru 002

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin(s) or the equivalent production modification(s) :

Service Bulletin No. A330-31-3104 Mod. No. 55982S18817

A330-31-3106 55982S18817

A330-28-3080 47997S16052

NOTE: Accomplish either Service Bulletin No. A330-31-3104 or Service Bulletin No.

A330-31-3106 in relation with the effectivity given in these Service Bulletins.

**CONF 003 thru 004

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin(s) or the equivalent production modification(s) :

Service Bulletin No. A330-31-3105 Mod. No. 56069S18891

A330-28-3080 47997S16052

REFERENCES / REPERCUSSIONS

**CONF ALL

TFU None

OEB 61

68

69

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHERS None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT YES

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 5

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C@A330

SERVICE BULLETIN

SUMMARY

HARD NO

SOFT NO

OBRM YES

MANPOWER

**CONF 001

Task 313125-831-801-001: MODIFICATION

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 002

Task 313125-831-801-001: MODIFICATION

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 003

Task 313125-831-801-001: MODIFICATION

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2). AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 004

Task 313125-831-801-001: MODIFICATION

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2). AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 6

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C@A330

SERVICE BULLETIN

SUMMARY

APPENDICES

**CONF ALL

None

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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C@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

1WW2

1WW1

800VU

FR20

FR18

A

Z120

A

G_SB_313125_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 8

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C@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 31

TITLE: INDICATING / RECORDING SYSTEMS - FLIGHT WARNING COMPUTER

(FWC) - INSTALL FWC STANDARD T2-0.

MODIFICATION No.: 51926S17857 56729S19417 58440S30619

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: Modification No. 56729S19417 (INSTALL FWC STANDARD T2-0) is

embodied before delivery on A330 aircraft MSN 0925 , 0962-0975 ,

0977-0979 , 0982-1031 , 1034-1035 , 1037-1045 , 1047-1078 , 1081 and

subsequent.

NOTE: Modification No. 51926S17857 (DEACTIVATE ALTITUDE ALERT INHIBITED

FUNCTION) is embodied before delivery on A330 aircraft MSN 0558 and

subsequent.

NOTE: Modification No. 58440S30619 (ACTIVATE ON A330 A/C ENGINE FEEDLINE

BURST MONITORING FUNCTION ON FWC T2) is embodied before delivery

on A330 aircraft MSN 0925 ,0962-0975 , 0977-0979 , 0982-1031 , 1034-1035

, 1037-1045 , 1047-1078 , 1081 and subsequent.

(1) Models

330-201 330-202 330-203 330-223 330-243 330-301 330-302 330-303

330-321 330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0059-0060 0062 0064-0067 0069-0073

0077 0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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C@A330

SERVICE BULLETIN

0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211

0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256

0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288

0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320

0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353

0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386

0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423

0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458

0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487

0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522

0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558

0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588

0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618

0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650

0652-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 0690-0693

0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718 0720-0722

0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747 0749-0752

0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782 0784-0786

0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811 0813-0815

0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863 0865-0869

0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901 0903-0909 0911

0913-0916 0918-0920 0922-0923 0926-0928 0930-0932 0934-0937 0939-0952 0954

0956-0959 0961 0964 0976 0980 1033 1036 1046 1080

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

10V 0863

46W 0871

78V 1033 1046

99Y 0747 0951

AAR 0640 0676 0708 0772 0803 0845

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

ADH 0272 0339

AEA 0733 0745 0749 0814 0931 0950

AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657 0660

ALK 0303 0306 0311 0313

ASY 1036

AVA 0948

BEL 0030 0037 0045 0082

BMA 0398 0401 0404

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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SERVICE BULLETIN

OPERATOR MSN

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830

0836 0851 0862 0866 0916 0928 0936 0942

CHH 0875 0881 0906 0919

CPA 0012 0017 0071 0083 0099 0102 0109 0113 0118 0121 0155 0244

0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0669

0673 0679 0776 0850 0855 0895 0915 0959

CRL 0285 0320

CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964

CYP 0505 0526

DAH 0644 0647 0650 0653 0667

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922

EDW 0369

EEZ 0358 0364 0665 0802

EIN 0055 0059 0070 0086 0269 0330 0397 0841 0847

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852

0854 0868

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755

FWI 0240 0253 0758

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HDA 0098 0106 0132 0177 0234 0405 0407 0479 0512 0581 0654 0662

0692 0716 0741 0786

HFY 0096

HVN 0087 0255 0262

IAC 0353 0362

ISR 0822

IWD 0072 0670 0833

IYE 0625 0632

JAI 0751 0807 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956

JST 0506 0508 0513 0522 0842 0853

KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0425 0428 0484 0490 0550

KFR 0874 0891 0927 0939 0946

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900

LTU 0120 0127 0171 0403 0432 0444 0454 0469 0476 0493 0739 0828

0911

LVG 0551 0597 0627

MAS 0067 0069 0073 0077 0095 0100 0107 0110 0116 0119 0143 0290

0296 0300

MAU 0883

MEA 0527 0529 0532 0926

MON 0261 0265

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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SERVICE BULLETIN

OPERATOR MSN

MPD 0205 0211 0943

MSR 0600 0610 0666 0683 0696 0709 0726

NWA 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799

0806 0817 0827 0843 0857 0858 0859 0865

OBS 0461

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887 0892

0898 0940 0945 0976

QTR 0441 0463 0473 0489 0504 0511 0521 0571 0612 0616 0623 0637

0638 0659 0680 0684 0711 0721 0734 0743 0746 0760 0789 0792

0813 0820 0826 0849 0893 0907 0918

RSF 0980

SAS 0496 0497 0515 0568

SWR 0229 0249 0275 0288 0291 0294 0299 0322 0324 0343 0366

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0869 0876

0949 0961

TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934

TCX 0254 0266 0301 0427 0456 0795

THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346

THY 0697 0704 0742 0754 0774

TSC 0111 0250 0271 0480

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0365

0372 0382 0384 0392 0396 0409 0437 0451 0452 0455 0462 0491

0494 0509 0518 0525 0536

UAF 1080

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388

VKG 0309 0349 0356 0357

XAX 0054 0952

XLF 0501 0635

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0050 0054 0060 0062 0064 0065 0066 0067 0069

0071 0073 0077 0083 0087 0095 0098 0099 0100 0102 0106

0107 0109 0110 0111 0112 0113 0116 0118 0119 0121 0122

0132 0143 0155 0162 0172 0177 0209 0224 0231 0244 0346

003

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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SERVICE BULLETIN

MSN CONFIGURATION

0030 0037 0045 0055 0059 0070 0082 0086 0120 0127 0181

0183 0184 0188 0189 0191 0195 0198 0200 0203 0205 0206

0211 0219 0222 0223 0226 0229 0230 0232 0234 0238 0240

0241 0247 0248 0249 0250 0251 0253 0254 0255 0256 0258

0259 0261 0262 0265 0266 0267 0269 0271 0272 0275 0276

0277 0279 0281 0283 0284 0285 0286 0287 0288 0290 0291

0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308

0309 0311 0312 0313 0314 0315 0316 0317 0320 0322 0323

0324 0326 0328 0330 0333 0334 0337 0338 0339 0340 0342

0343 0344 0345 0348 0349 0350 0351 0353 0356 0357 0358

0361 0362 0364 0365 0366 0368 0369 0370 0372 0375 0380

0382 0384 0386 0388 0389 0392 0393 0396 0397

001

0072 0138 0140 0144 0148 0153 0165 004

0096 0171 001 003

0398 0400 0401 0403 0404 0405 0407 0408 0409 0412 0418

0419 0420 0421 0422 0423 0425 0427 0428 0432 0437 0439

0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461

0462 0463 0465 0466 0469 0472 0473 0476 0477 0479 0480

0481 0484 0486 0487 0489 0490 0491 0493 0494 0496 0497

0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509

0510 0511 0512 0513 0515 0516 0518 0519 0521 0522 0524

0525 0526 0527 0529 0530 0532 0533 0535 0536 0539 0542

0548 0549 0550 0551 0552 0553 0555 0558 0564 0565 0567

0568 0570 0571 0573 0574 0576 0578 0579 0581 0584 0587

0588 0591 0593 0595 0597 0600 0602 0603 0605 0607 0609

0610 0612 0614 0616 0618 0620 0621 0623 0625 0627 0629

0631 0632 0633 0634 0635 0636 0637 0638 0640 0641 0642

0644 0645 0647 0648 0649 0650 0652 0653 0654 0655 0656

0657 0658 0659 0660 0661 0662 0663 0664 0665 0666 0667

0669 0670 0671 0673 0674 0675 0676 0678 0679 0680 0682

0683 0684 0686 0687 0688 0690 0691 0692 0693 0695 0696

0697 0699 0700 0701 0703 0704 0705 0707 0708 0709 0711

0712 0713 0714 0716 0717 0718 0720 0721 0722 0724 0725

0726 0728 0729 0730 0732 0733 0734 0735 0737 0738 0739

0741 0742 0743 0745 0746 0747 0749 0750 0751 0752 0754

0755 0756 0758 0759 0760 0769 0770 0772 0773 0774 0776

0777 0778 0780 0781 0782 0784 0785 0786 0788 0789 0791

0792 0795 0796 0797 0799 0801 0802 0803 0805 0806 0807

0809 0810 0811 0813 0814 0815 0817 0818 0819 0820 0821

0822 0823 0824 0825 0826 0827 0828 0830 0831 0832 0833

0834 0836 0838 0839 0840 0841 0842 0843 0845 0847 0849

0850 0851 0852 0853 0854 0855 0857 0858 0859 0860 0861

0862 0863 0865 0866 0867 0868 0869 0871 0873 0874 0875

0876 0877 0879 0881 0882 0883 0884 0885 0887 0888 0889

0890 0891 0892 0893 0895 0896 0898 0899 0900 0901 0903

0904 0905 0906 0907 0908 0909 0911 0913 0914 0915 0916

0918 0919 0920 0922 0923 0926 0927 0928 0930 0931 0932

0934 0935 0936 0937 0939 0940 0941 0942 0943 0944 0945

0946 0947 0948 0949 0950 0951 0952 0954 0956 0957 0958

0959 0961 0964 0976 0980 1033 1036 1046 1080

002

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(5) Configuration definition

**CONF 001

Config. 01 is valid for aircraft on which :

- Modification No. 45509S13661 (INSTALL COLLINS MULTI-MODE RECEIVERS)

is embodied or Service Bulletin No. A330-34-3102 (Mod. No. 45509S13661) is

accomplished

- Modification No. 47653S15129 (STANDARDIZE ELECTRONICS RACK 800VU) is not

embodied

- Altitude alert chord function is not activated (wires 3152-0715 and 3152-0784 are

connected to a dummy connector or are not installed).

**CONF 002

Config. 02 is valid for aircraft on which :

- Modification No. 45509S13661 (INSTALL COLLINS MULTI-MODE RECEIVERS)

is embodied or Service Bulletin No. A330-34-3102 (Mod. No. 45509S13661) is

accomplished

- Modification No. 47653S15129 (STANDARDIZE ELECTRONICS RACK 800VU) is

embodied

- Altitude alert chord function is not activated (wires 3152-0715 and 3152-0784 are

connected to a dummy connector or are not installed).

**CONF 003

Config. 03 is valid for aircraft on which :

- Modification No. 45509S13661 (INSTALL COLLINS MULTI-MODE RECEIVERS) is

not embodied and Service Bulletin No. A330-34-3102 (Mod. No. 45509S13661) is not

accomplished

- Modification No. 47653S15129 (STANDARDIZE ELECTRONICS RACK 800VU) is not

embodied

- Altitude alert chord function is not activated (wires 3152-0715 and 3152-0784 are

connected to a dummy connector or are not installed).

**CONF 004

Config. 04 is valid for aircraft on which :

- Modification No. 45509S13661 (INSTALL COLLINS MULTI-MODE RECEIVERS) is

not embodied and Service Bulletin No. A330-34-3102 (Mod. No. 45509S13661) is not

accomplished

- Modification No. 47653S15129 (STANDARDIZE ELECTRONICS RACK 800VU) is not

embodied

- Altitude alert chord function is activated (wire 3152-0715 is connected to connector

2828VC and wire 3152-0784 is connected to 2824VC).

(6) Material Effectivity

**CONF 001, 003 thru 004

MATERIAL QTY PER A/C REMARK

Equipment BFEA01 1

Component COMPA01 1

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**CONF 002

MATERIAL QTY PER A/C REMARK

Equipment BFEA01 1

Component COMPA02 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

**CONF 001 thru 002

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin(s) or the equivalent production modification(s) :

Service Bulletin No. A330-31-3104 Mod. No. 55982S18817

A330-31-3106 55982S18817

A330-28-3080 47997S16052

NOTE: Accomplish either Service Bulletin No. A330-31-3104 or Service Bulletin No.

A330-31-3106 in relation with the effectivity given in these Service Bulletins.

**CONF 003 thru 004

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin(s) or the equivalent production modification(s) :

Service Bulletin No. A330-31-3105 Mod. No. 56069S18891

A330-28-3080 47997S16052

**CONF ALL

C. REASON

(1) History

This Service Bulletin is published to advise all operators of A330 aircraft of the issue of

AIRBUS FRANCE SAS Service Bulletin No. LA2E2-31-007 and the issue of AIRBUS

FRANCE SAS Service Bulletin No. LA2E2-31-008.

This Service Bulletin has been issued to install a new Flight Warning Computer (FWC)

standard T2-0 with 486 based Central Processing Unit (CPU) board on A330 aircraft

model.

(2) Objective/Action

This Service Bulletin proposes the replacement of the following computer :

- Two AIRBUS FRANCE SAS FWCs P/N LA2E0060D8K0000 standard K8-1

(installed by Mod. No. 56069S18891 (INDICATING/RECORDING SYSTEMS -

FLIGHT WARNING COMPUTER (FWC) - INSTALL FWC STANDARD K8-1) with

386 based CPU board

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- Or two AIRBUS FRANCE SAS FWCs P/N LA2E20202T10000 standard T1-0

(installed by Mod. No. 55982S18817 (INDICATING/RECORDING SYSTEMS -

FLIGHT WARNING COMPUTER (FWC) - INSTALL FWC STANDARD T1) with 486

based CPU board

- By two AIRBUS FRANCE SAS FWCs P/N LA2E20202T20000 standard T2-0 with

486 based CPU board electrically and mechanically interchangeable.

This new standard is obtained either by

- Replacement of the FWCs

- Or by replacement or reprogramming of the On-Board Replaceable Modules

(OBRMs), from T1-0 standard only.

(3) Advantages

Accomplishment of this Service Bulletin will improve the operating performance of the

FWCs.

From FWC K8-1/386 standard, the main improvements are the following :

- Improvement of the smoke procedure,

- New "PARK BRAKE ON" alert in flight,

- New auto call-outs 60ft and 70ft (activated by separate pin programming),

- New "Air Data Reference (ADR) monitoring" functions and alerts,

- FLS/GLS compatibility,

- PAX system function (activated by separate pin programming),

- CBB or TV system integration,

- Consolidation of slats/flaps configuration monitoring for take off,

- Tail strike detection system capability,

- Head Up Display (HUD) installation capability,

- New audio board with data-loading capability from the OBRM,

- New 486 CPU board,

- Intermediate Pressure Turbine Overspeed System (IPTOS) monitoring for RR

engines,

- New Autopilot/Flight Director Traffic "AUTO FLT TCAS MODE FAULT" Alert and

Collision Avoidance System mode (AP/FD TCAS) monitoring capability,

- Landing Gear Well Surveillance System (LGWSS) installation capability with new

"L/G SURV INTRUSION DET" alert,

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- Fuel Tank Inerting System (FTIS) installation capability with new "FUEL INERTING

SYS FAULT" alert,

- AOA monitoring with new "NAV AOA DISAGREE" alert (minimum FCDC standard

required),

- Cabin Intercommunication Data System with integrated Smoke Detection Function

(CIDS-SDF) installation capability,

- New engine Feedline burst monitoring capability with "ENG 1 (2) FEEDLINE

BURST" alert (requires pin-programming),

- Monitoring of throttles lever position during landing with new "ENG 1 (2) THR

LEVER ABV IDLE" red alert,

- Icing condition procedure for RR engines with new "ENG RISK OF STATOR ICING"

alert,

- Deletion of procedure linked to "NAV TCAS FAULT" alert to avoid unintentional

switching off of transponder,

- New monitoring for 64CK and 70K PW engine installation capability,

- ALNAv2 network services system installation capability,

- ADS-B/ATSAW function installation capability,

- New "NAV HUD FPV DISCREPANCY" alert linked to HUD monitoring.

From FWC T1/486 the main improvements are the following :

- New Autopilot/Flight Director Traffic "AUTO FLT TCAS MODE FAULT" Alert and

Collision Avoidance System mode (AP/FD TCAS) monitoring capability,

- Landing Gear Well Surveillance System (LGWSS) installation capability with new

"L/G SURV INTRUSION DET " alert,

- Fuel Tank Inerting System (FTIS) installation capability with new "FUEL INERTING

SYS FAULT" alert,

- AOA monitoring with new "NAV AOA DISAGREE" alert (minimum FCDC standard

required),

- Cabin Intercommunication Data System with integrated Smoke Detection Function

(CIDS-SDF) installation capability,

- New engine feedline burst monitoring capability with "ENG 1 (2) FEEDLINE BURST"

alert (requires pin-programming),

- Monitoring of throttle lever position during landing with new "ENG 1 (2) THR LEVER

ABV IDLE" red alert,

- Icing condition procedure for RR engines with new "ENG RISK OF STATOR ICING"

alert,

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- Deletion of procedure linked to "NAV TCAS FAULT" alert to avoid unintentional

switching off of transponder,

- New monitoring for 64CK and 70K PW engine installation capability,

- ALNAv2 network services system installation capability,

- ADS-B/ATSAW function installation capability,

- New "NAV HUD FPV DISCREPANCY" alert linked to HUD monitoring.

(4) Operational/Maintenance Consequences

The operational/maintenance consequence of this Service Bulletin are the modification

of the Flight Crew Operating Manual (FCOM) VOL 1 and 3 and cancels Operating

Engineering Bulletin (OEB) No. 61, 68 and 69.

Operators having programmed an OEB reminder should delete the reminder(s) from

their system.

NOTE: For a full improvement description, refer to MOI No. 56729.

D. DESCRIPTION

NOTE: For CONF 001 and 002 only, to accomplish this Service Bulletin, you have

two possibilities :

- Either you modify the two FWCs by replacement or by reprogramming

of the OBRMs as described in SUBTASK 313125-831-001 001 Modify

the FWCs (1WW1 and 1WW2) in the Main Rack 800VU. SUBTASK

313125-831-001 001 Modify the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

- Or you replace them as described in SUBTASK 313125-831-002 001

Replace the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

SUBTASK 313125-831-002 001 Replace the FWCs (1WW1 and 1WW2)

in the Main Rack 800VU.

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 313125-831-801-001: MODIFICATION

(1) Modify the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

(2) Replace the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

(3) Modify the Wiring in the Main Rack 800VU.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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**CONF 002

Task 313125-831-801-001: MODIFICATION

(1) Modify the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

(2) Replace the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

(3) Modify the Wiring in the Main Rack 800VU.

**CONF 003

Task 313125-831-801-001: MODIFICATION

(1) Remove the FWCs (1WW1 and 1WW2) from the Main Rack 800VU.

(2) Modify the FWCs (1WW1 and 1WW2).

(3) Modify the Wiring in the Main Rack 800VU.

(4) Install the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

**CONF 004

Task 313125-831-801-001: MODIFICATION

(1) Remove the FWCs (1WW1 and 1WW2) from the Main Rack 800VU.

(2) Modify the FWCs (1WW1 and 1WW2).

(3) Modify the Wiring in the Main Rack 800VU.

(4) Install the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

**CONF ALL

E. COMPLIANCE

(1) Classification

RECOMMENDED

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available.

F. APPROVAL

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

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SERVICE BULLETIN

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

**CONF 001

Task 313125-831-801-001: MODIFICATION

Get Access 2.00

On Aircraft

Replace the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

1.00

Modify the Wiring in the Main Rack 800VU. 2.00

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 002

Task 313125-831-801-001: MODIFICATION

Get Access 2.00

On Aircraft

Replace the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

1.00

Modify the Wiring in the Main Rack 800VU. 2.00

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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**CONF 003

Task 313125-831-801-001: MODIFICATION

Get Access 2.00

On Aircraft

Remove the FWCs (1WW1 and 1WW2) from the Main

Rack 800VU.

0.50

Modify the Wiring in the Main Rack 800VU. 2.00

Install the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

0.50

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2). AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 004

Task 313125-831-801-001: MODIFICATION

Get Access 2.00

On Aircraft

Remove the FWCs (1WW1 and 1WW2) from the Main

Rack 800VU.

0.50

Modify the Wiring in the Main Rack 800VU. 2.00

Install the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

0.50

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer to:

Modify the FWCs (1WW1 and 1WW2). AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

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I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 12-34-24 25-52-00 31-50-00

31-51-00 31-53-34 45-10-00

52-10-00 52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-52-10 20-52-21

20-55-00

Modification Operational Impact (MOI) MOI No. 56729

Service Bulletin (SB) A330-28-3080

A330-31-3028

A330-31-3052

A330-31-3062

A330-31-3084

A330-34-3102

A330-31-3104

A330-31-3106

Standards Manual (SM)

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 002

Aircraft Maintenance Manual (AMM) 12-34-24 25-52-00 31-50-00

31-51-00 31-53-34 45-10-00

52-10-00 52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-52-10 20-52-21

20-55-00

Modification Operational Impact (MOI) MOI No. 56729

Service Bulletin (SB) A330-28-3080

A330-31-3028

A330-31-3052

A330-31-3062

A330-31-3084

A330-34-3102

A330-31-3104

A330-31-3106

Standards Manual (SM)

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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**CONF 003

Aircraft Maintenance Manual (AMM) 12-34-24 25-52-00 31-50-00

31-51-00 31-53-34 52-10-00

52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-52-10 20-52-21

20-55-00

Modification Operational Impact (MOI) MOI No. 56729

Service Bulletin (SB) A330-28-3080

A330-31-3028

A330-31-3052

A330-31-3062

A330-31-3084

A330-34-3102

A330-31-3105

Standards Manual (SM)

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 004

Aircraft Maintenance Manual (AMM) 12-34-24 25-52-00 31-50-00

31-51-00 31-53-34 52-10-00

52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-52-10 20-52-21

20-55-00

Modification Operational Impact (MOI) MOI No. 56729

Service Bulletin (SB) A330-28-3080

A330-31-3028

A330-31-3052

A330-31-3062

A330-31-3084

A330-34-3102

A330-31-3105

Standards Manual (SM)

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 31-51-21 31-51-22 31-51-23

31-51-24 31-51-26 31-51-27

31-51-28 31-51-29 31-51-30

31-51-31 31-51-32 31-51-33

31-51-34 31-51-36 31-51-38

31-51-45 31-51-46 31-51-49

31-51-52 31-51-70 31-52-00

31-54-00

Aircraft Schematic Manual (ASM) 31-52-00

Aircraft Wiring List (AWL)

Aircraft Wiring Manual (AWM) 31-52-97 31-52-98

Flight Crew Operating Manual (FCOM) VOL 1

VOL 3

Flight Manual (FM)

Illustrated Parts Catalog (IPC) 31-52-08 31-53-54

Master Minimum Equipment List (MMEL)

Trouble Shooting Manual (TSM) 22-12-00 23-13-00 23-77-00

24-21-00 24-22-00 24-23-00

24-32-00 24-38-00 24-51-00

34-15-00 34-35-00 34-36-00

34-43-00 71-00-00 73-30-00

77-11-00 77-30-00

NOTE: This Service Bulletin has an operational impact. Please inform AIRBUS,

at least four weeks in advance, in case you need your operational

documentation to be amended by an intermediate revision prior to Service

Bulletin embodiment. For this purpose, please request the intermediate

revision by fax, telex or mail to:

SEDCC, AIRBUS - Customer Services Directorate

Fax No.: 33 (0) 5 61 93 28 06

Sita No.: TLSBP7X E-mail: sb.reporting@airbus.com

These amendments will be confirmed by the next normal revision of

operational documentation, once your Service Bulletin accomplishment report

has been sent, as usual, to our Customer Services Directorate (SEDCC).

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

FWC LA2E20202T10000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

FWC LA2E0060D8K0000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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NOTE (2): For A330 aircraft enhanced or enhanced cabin, the System Data Acquisition

Concentrator (SDAC) C7-0 (installed by Mod. No. 51450S16808, Service

Bulletins No. A330-31-3052 or A330-31-3062) or C8-0 (installed by Mod. No.

53069S18365, Service Bulletin No. A330-31-3084) standard must be installed

with FWC T2-0 standard. Otherwise, SDAC C3-0A (installed by Mod. No.

46947S14693, Service Bulletin No. A330-31-3028) could also be installed.

NOTE (3): Not authorized. Replacement/modification of the 2 FWCs has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph C of

this Service Bulletin.

NOTE (4): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

FWC LA2E20202T10000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

FWC LA2E0060D8K0000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (2): For A330 aircraft enhanced or enhanced cabin, the System Data Acquisition

Concentrator (SDAC) C7-0 (installed by Mod. No. 51450S16808, Service

Bulletins No. A330-31-3052 or A330-31-3062) or C8-0 (installed by Mod. No.

53069S18365, Service Bulletin No. A330-31-3084) standard must be installed

with FWC T2-0 standard. Otherwise, SDAC C3-0A (installed by Mod. No.

46947S14693, Service Bulletin No. A330-31-3028) could also be installed.

NOTE (3): Not authorized. Replacement/modification of the 2 FWCs has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph C of

this Service Bulletin.

NOTE (4): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

FWC LA2E20202T10000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

FWC LA2E0060D8K0000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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SERVICE BULLETIN

NOTE (2): For A330 aircraft enhanced or enhanced cabin, the System Data Acquisition

Concentrator (SDAC) C7-0 (installed by Mod. No. 51450S16808, Service

Bulletins No. A330-31-3052 or A330-31-3062) or C8-0 (installed by Mod. No.

53069S18365, Service Bulletin No. A330-31-3084) standard must be installed

with FWC T2-0 standard. Otherwise, SDAC C3-0A (installed by Mod. No.

46947S14693, Service Bulletin No. A330-31-3028) could also be installed.

NOTE (3): Not authorized. Replacement/modification of the 2 FWCs has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph C of

this Service Bulletin.

NOTE (4): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

FWC LA2E20202T10000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

FWC LA2E0060D8K0000 LA2E20202T20000 03 Not

Applicable

(1) (2) (3)

(4)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (2): For A330 aircraft enhanced or enhanced cabin, the System Data Acquisition

Concentrator (SDAC) C7-0 (installed by Mod. No. 51450S16808, Service

Bulletins No. A330-31-3052 or A330-31-3062) or C8-0 (installed by Mod. No.

53069S18365, Service Bulletin No. A330-31-3084) standard must be installed

with FWC T2-0 standard. Otherwise, SDAC C3-0A (installed by Mod. No.

46947S14693, Service Bulletin No. A330-31-3028) could also be installed.

NOTE (3): Not authorized. Replacement/modification of the 2 FWCs has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph C of

this Service Bulletin.

NOTE (4): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF ALL

M. SPARES

FWC LA2E0060D8K0000

FWC LA2E20202T10000

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.

Vendor parts are to be ordered from :

Equipment BFEA01 AIRBUS FRANCE S.A.S.

AVIONICS AND SIMULATION PRODUCTS

EYY - M6525 - 316, route de Bayonne

31060 TOULOUSE Cedex 09

FRANCE

Tel : (33) 5 61 18 14 33

Fax : (33) 5 61 18 04 94

e-mail : systems.support@airbus.com

(2) Price and Availability

Refer to the vendor Service Bulletin for the equipment modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

For the organization of this retrofit, operators are kindly requested to contact AIRBUS retrofit

management department.

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 67 19 06 22

Fax : (33) 5 61 93 27 45

E-mail : monitored.retrofit@airbus.com

Modification of parts/equipment is at no charge for the operator. The man-hours indicated in

this Service Bulletin will remain at the operators’ cost.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

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(2) Components

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT REMARK

EN3155-015F2018 4 Contact

NOTE: If you find part numbers of hardware components in the related kit(s)

which you cannot identify in the LIST OF COMPONENTS of this Service

Bulletin, refer to Standards Manual (SM). The SM will give you the

correct part number to part number relationship.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT REMARK

EN3155-003F2222 4 Contact

NOTE: If you find part numbers of hardware components in the related kit(s)

which you cannot identify in the LIST OF COMPONENTS of this Service

Bulletin, refer to Standards Manual (SM). The SM will give you the

correct part number to part number relationship.

(3) Equipment

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT REMARK

LA2E20202T20000 2 FWC LA2E0060D8K0000 03 (1)(2)(3)

LA2E20202T10000 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): For A330 aircraft enhanced or enhanced cabin, the System

Data Acquisition Concentrator (SDAC) C7-0 (installed by Mod. No.

51450S16808, Service Bulletins No. A330-31-3052 or A330-31-3062)

or C8-0 (installed by Mod. No. 53069S18365, Service Bulletin No.

A330-31-3084) standard must be installed with FWC T2-0 standard.

Otherwise, SDAC C3-0A (installed by Mod. No. 46947S14693, Service

Bulletin No. A330-31-3028) could also be installed.

NOTE (2): Not authorized. Replacement/modification of the 2 FWCs has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph

C of this Service Bulletin.

NOTE (3): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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SERVICE BULLETIN

F. TOOLING

None

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 313125-831-801-001 - MODIFICATION

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS :

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION, REFER TO ESPM 20-55-00.

CAUTION: THE ELECTROSTATIC DISCHARGE PRECAUTIONS DESCRIBED IN ARINC

REPORT 606 ARE RECOMMENDED.

Task Associated Data

**CONF 001

Zone 120 130 210

Modified FIN 1WW1 1WW2

Access Door 811 821 831

Panel 131AW 131BW 132CW

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer

to:

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 002

Zone 120 130 210

Modified FIN 1WW1 1WW2

Access Door 811 821 831

Panel 131AW 131BW 132CW

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Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer

to:

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 003

Zone 120 130 210

Modified FIN 1WW1 1WW2

Access Door 811 821

Panel 131AW 131BW 132CW

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer

to:

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

**CONF 004

Zone 120 130 210

Modified FIN 1WW1 1WW2

Access Door 811 821

Panel 131AW 131BW 132CW

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

C

Additional manhours related to Vendor SB; refer

to:

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-007

AIRBUS FRANCE SAS Service

Bulletin No. LA2E2-31-008

A. GENERAL

**CONF 001

(1) Subtask 313125-910-001-002 - Standard Practices

Manpower Resources

Skills ELECTRICAL

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References

Elec. Std. Practices Manual (ESPM) 20-33-00

20-52-21

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Put blanking caps on the disconnected electrical connectors.

(c) Make sure that the electrical connectors are serviceable before you connect them

again.

(d) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 313125-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 313125-910-001-002 - Standard Practices

Manpower Resources

Skills ELECTRICAL

References

Elec. Std. Practices Manual (ESPM) 20-33-00

20-52-21

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Put blanking caps on the disconnected electrical connectors.

(c) Make sure that the electrical connectors are serviceable before you connect them

again.

(d) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 313125-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 25

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SERVICE BULLETIN

**CONF 003

(1) Subtask 313125-910-001-002 - Standard Practices

Manpower Resources

Skills ELECTRICAL

References

Elec. Std. Practices Manual (ESPM) 20-33-00

20-52-21

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Put blanking caps on the disconnected electrical connectors.

(c) Make sure that the electrical connectors are serviceable before you connect them

again.

(d) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 313125-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 004

(1) Subtask 313125-910-001-002 - Standard Practices

Manpower Resources

Skills ELECTRICAL

References

Elec. Std. Practices Manual (ESPM) 20-33-00

20-52-21

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Put blanking caps on the disconnected electrical connectors.

(c) Make sure that the electrical connectors are serviceable before you connect them

again.

(d) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 313125-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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SERVICE BULLETIN

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

**CONF 001

(1) Subtask 313125-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 31-53-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-000-801).

(2) Subtask 313125-010-001-002 - Remove/Open for Access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-000-801

Task 52-10-00-010-801

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

(a) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

(b) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(c) In the FWD cargo-compartment at FR20, remove the partition panels 131AW,

131BW and 132CW (Refer to AMM Task 25-52-00-000-801).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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(3) Subtask 313125-941-002-001 - Parity Configuration Recording

Manpower Resources

Skills ELECTRICAL

References

Fig. A-FCCAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCDAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCEAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

Fig. A-FCFAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

(a) For the FWC-1 (1WW1) parity wiring, before any disconnection, record the figure

number of the Hook-up Chart on which the line 1 agree with the aircraft wiring

configuration (Refer to Fig. A-FCCAA Sheet 02 and Fig. A-FCDAA Sheet 02).

(b) For the FWC-2 (1WW2) parity wiring, before any disconnection, record the figure

number of the Hook-up Chart on which the line 1 agree with the aircraft wiring

configuration (Refer to Fig. A-FCEAA Sheet 02 and Fig. A-FCFAA Sheet 02).

**CONF 002

(1) Subtask 313125-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 31-53-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-000-801).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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(2) Subtask 313125-010-001-002 - Remove/Open for Access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-000-801

Task 52-10-00-010-801

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

(a) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

(b) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(c) In the FWD cargo-compartment at FR20, remove the partition panels 131AW,

131BW and 132CW (Refer to AMM Task 25-52-00-000-801).

(3) Subtask 313125-941-002-002 - Parity Configuration Recording

Work Zones and Access Panels

Zone Access/Work location

120 Work location Electrical panel 800VU

Manpower Resources

Skills ELECTRICAL

References

Fig. A-FCCAB Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCDAB Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCEAB Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

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References

Fig. A-FCFAB Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

(a) For the FWC-1 (1WW1) parity wiring, before any disconnection, record the figure

number of the Hook-up Chart on which the line 1 agree with the aircraft wiring

configuration (Refer to Fig. A-FCCAB Sheet 02 and Fig. A-FCDAB Sheet 02).

(b) For the FWC-2 (1WW2) parity wiring, before any disconnection, record the figure

number of the Hook-up Chart on which the line 1 agree with the aircraft wiring

configuration (Refer to Fig. A-FCEAB Sheet 02 and Fig. A-FCFAB Sheet 02).

**CONF 003

(1) Subtask 313125-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 31-53-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-000-801).

(2) Subtask 313125-010-001-002 - Remove/Open for Access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-000-801

Task 52-10-00-010-801

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

(a) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

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(b) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(c) In the FWD cargo-compartment at FR20, remove the partition panels 131AW,

131BW and 132CW (Refer to AMM Task 25-52-00-000-801).

(3) Subtask 313125-941-002-001 - Parity Configuration Recording

Manpower Resources

Skills ELECTRICAL

References

Fig. A-FCCAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCDAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCEAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

Fig. A-FCFAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

(a) For the FWC-1 (1WW1) parity wiring, before any disconnection, record the figure

number of the Hook-up Chart on which the line 1 agree with the aircraft wiring

configuration (Refer to Fig. A-FCCAA Sheet 02 and Fig. A-FCDAA Sheet 02).

(b) For the FWC-2 (1WW2) parity wiring, before any disconnection, record the figure

number of the Hook-up Chart on which the line 1 agree with the aircraft wiring

configuration (Refer to Fig. A-FCEAA Sheet 02 and Fig. A-FCFAA Sheet 02).

**CONF 004

(1) Subtask 313125-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 31-53-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

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(b) Put access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-000-801).

(2) Subtask 313125-010-001-002 - Remove/Open for Access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-000-801

Task 52-10-00-010-801

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

(a) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

(b) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(c) In the FWD cargo-compartment at FR20, remove the partition panels 131AW,

131BW and 132CW (Refer to AMM Task 25-52-00-000-801).

C. PROCEDURE

NOTE: For CONF 001 and 002 only, to accomplish this Service Bulletin, you have

two possibilities :

- Either you modify the two FWCs by replacement or by reprogramming

of the OBRMs as described in SUBTASK 313125-831-001 001 Modify

the FWCs (1WW1 and 1WW2) in the Main Rack 800VU. SUBTASK

313125-831-001 001 Modify the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

- Or you replace them as described in SUBTASK 313125-831-002 001

Replace the FWCs (1WW1 and 1WW2) in the Main Rack 800VU.

SUBTASK 313125-831-002 001 Replace the FWCs (1WW1 and 1WW2)

in the Main Rack 800VU.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

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**CONF 001

(1) Subtask 313125-831-001-001 - Modify the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

210 Access to open Door 831

References

Aircraft Maintenance Manual (AMM) Task 31-50-00-740-801

Task 45-10-00-860-801

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS LA2E2-31-008

(a) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(b) Do the Line Replaceable Unit (LRU) identification test :

1 Job set-up

a Do the procedure to get access to the SYSTEM REPORT/TEST 3/6 page

(Refer to AMM Task 45-10-00-860-801).

b Make sure that these circuit breakers are closed :

PANEL DESIGNATION FIN LOCATION REMARK

742VU FWC 1 2WW1 80 Q

722VU FWC 2 2WW2 48 C

721VU PRINTER 1TP 02 D

2 Procedure

ACTION RESULT

1. On the SYSTEM REPORT/TEST page :

- Push the line key adjacent to the WARNING

indication.

The FWS menu page comes into view.

2. On the FWS menu page :

- Push the line key adjacent to the LRU

identification.

The LRU identification page comes into view.

3. On the FWS LRU identification page :

- Make sure that the old P/N of the two FWCs is

LA2E20202T10000.

4. Print the FWS LRU identification page (if the

printer is not available, a visual check is

acceptable).

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SERVICE BULLETIN

3 Close-up

a Put the aircraft back to its initial configuration.

<1> On the Multi-Purpose Control and Display Unit (MCDU), push

the line key adjacent to the RETURN indication until the

MAINTENANCE MENU 1/2 page comes into view.

<2> On the MCDU, set the BRT knob to the OFF position.

(c) Open safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION REMARK

742VU FWC 1 2WW1 80 Q

722VU FWC 2 2WW2 48 C

(d) Replace or reprogram the OBRM on the FWCs (1WW1 and 1WW2) (Refer to

AIRBUS FRANCE SAS Service Bulletin No. LA2E2-31-008).

(2) Subtask 313125-831-002-001 - Replace the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2E20202T20000 2 FWC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-000-801

Task 31-53-34-400-801

(a) Remove (Refer to AMM Task 31-53-34-000-801) :

FIN 1WW1

1 FWC LA2E20202T10000

and

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 34

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SERVICE BULLETIN

FIN 1WW2

1 FWC LA2E20202T10000

(b) Install (Refer to AMM Task 31-53-34-400-801) :

FIN 1WW1

1 FWC LA2E20202T20000

and

FIN 1WW2

1 FWC LA2E20202T20000

NOTE: Install the new FWCs after the modification of the wiring.

(3) Subtask 313125-831-004-002 - Modify the Wiring in the Main Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 821

Panel 131AW, Panel 131BW, Panel 132CW

Work location Electrical panel 800VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

EN3155-015F2018 6 Contact

References

Fig. A-FBAAA Sheet 01 - Location of the Equipment

Fig. A-FCAAB Sheet 01 - Modification of the Pin

Programming of the FWC-1

Sheet 02 - Modification of the Pin

Programming of the FWC-1

Fig. A-FCBAB Sheet 01 - Modification of the Pin

Programming of the FWC-2

Sheet 02 - Modification of the Pin

Programming of the FWC-2

Fig. A-FCCAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 35

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SERVICE BULLETIN

References

Fig. A-FCDAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCEAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

Fig. A-FCFAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

(a) Modify the pin programming of the FWC-1.

1 Modify the connection of the wire shown on the wiring diagram Fig. A-FCAAB

Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCAAB Sheet 02).

2 If necessary, use :

1 Contact EN3155-015F2018

(b) Modify the parity of the FWC-1.

1 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCCAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCCAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCCAA Sheet 02).

b If necessary, use :

1 Contact EN3155-015F2018

2 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCDAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCDAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCDAA Sheet 02).

b If necessary, use :

1 Contact EN3155-015F2018

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 36

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C@A330

SERVICE BULLETIN

(c) Modify the pin programming of the FWC-2.

1 Modify the connection of the wire shown on the wiring diagram Fig. A-FCBAB

Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCBAB Sheet 02).

2 If necessary, use :

1 Contact EN3155-015F2018

(d) Modify the parity of the FWC-2.

1 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCEAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCEAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCEAA Sheet 02).

b If necessary, use :

1 Contact EN3155-015F2018

2 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCFAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCFAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCFAA Sheet 02).

b If necessary, use :

1 Contact EN3155-015F2018

**CONF 002

(1) Subtask 313125-831-001-001 - Modify the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

210 Access to open Door 831

References

Aircraft Maintenance Manual (AMM) Task 31-50-00-740-801

Task 45-10-00-860-801

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 37

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SERVICE BULLETIN

References

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS LA2E2-31-008

(a) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(b) Do the Line Replaceable Unit (LRU) identification test :

1 Job set-up

a Do the procedure to get access to the SYSTEM REPORT/TEST 3/6 page

(Refer to AMM Task 45-10-00-860-801).

b Make sure that these circuit breakers are closed :

PANEL DESIGNATION FIN LOCATION REMARK

742VU FWC 1 2WW1 80 Q

722VU FWC 2 2WW2 48 C

721VU PRINTER 1TP 02 D

2 Procedure

ACTION RESULT

1. On the SYSTEM REPORT/TEST page :

- Push the line key adjacent to the WARNING

indication.

The FWS menu page comes into view.

2. On the FWS menu page :

- Push the line key adjacent to the LRU

identification.

The LRU identification page comes into view.

3. On the FWS LRU identification page :

- Make sure that the old P/N of the two FWCs is

LA2E20202T10000.

4. Print the FWS LRU identification page (if the

printer is not available, a visual check is

acceptable).

3 Close-up

a Put the aircraft back to its initial configuration.

<1> On the Multi-Purpose Control and Display Unit (MCDU), push

the line key adjacent to the RETURN indication until the

MAINTENANCE MENU 1/2 page comes into view.

<2> On the MCDU, set the BRT knob to the OFF position.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 38

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C@A330

SERVICE BULLETIN

(c) Open safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION REMARK

742VU FWC 1 2WW1 80 Q

722VU FWC 2 2WW2 48 C

(d) Replace or reprogram the OBRM on the FWCs (1WW1 and 1WW2) (Refer to

AIRBUS FRANCE SAS Service Bulletin No. LA2E2-31-008).

(2) Subtask 313125-831-002-001 - Replace the FWCs (1WW1 and 1WW2) in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2E20202T20000 2 FWC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-000-801

Task 31-53-34-400-801

(a) Remove (Refer to AMM Task 31-53-34-000-801) :

FIN 1WW1

1 FWC LA2E20202T10000

and

FIN 1WW2

1 FWC LA2E20202T10000

(b) Install (Refer to AMM Task 31-53-34-400-801) :

FIN 1WW1

1 FWC LA2E20202T20000

and

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 39

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C@A330

SERVICE BULLETIN

FIN 1WW2

1 FWC LA2E20202T20000

NOTE: Install the new FWCs after the modification of the wiring.

(3) Subtask 313125-831-004-004 - Modify the Wiring in the Main Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 821

Panel 131AW, Panel 131BW, Panel 132CW

Work location Electrical panel 800VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD

EN3155-003F2222 6 Contact

References

Fig. A-FBAAB Sheet 01 - Location of the Equipment

Fig. A-FCAAC Sheet 01 - Modification of the Pin

Programming of the FWC-1

Sheet 02 - Modification of the Pin

Programming of the FWC-1

Fig. A-FCBAC Sheet 01 - Modification of the Pin

Programming of the FWC-2

Sheet 02 - Modification of the Pin

Programming of the FWC-2

Fig. A-FCCAB Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCDAB Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCEAB Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 40

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C@A330

SERVICE BULLETIN

References

Fig. A-FCFAB Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

(a) Modify the pin programming of the FWC-1.

1 Modify the connection of the wire shown on the wiring diagram Fig. A-FCAAC

Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCAAC Sheet 02).

2 If necessary, use :

1 Contact-Socket EN3155-003F2222

(b) Modify the parity of the FWC-1.

1 If, during accomplishment of SUBTASK 313125-941-002 002 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCCAB Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCCAB Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCCAB Sheet 02).

b If necessary, use :

1 Contact-Socket EN3155-003F2222

2 If, during accomplishment of SUBTASK 313125-941-002 002 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCDAB Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCDAB Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCDAB Sheet 02).

b If necessary, use :

1 Contact-Socket EN3155-003F2222

(c) Modify the pin programming of the FWC-2.

1 Modify the connection of the wire shown on the wiring diagram Fig. A-FCBAC

Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCBAC Sheet 02).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 41

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C@A330

SERVICE BULLETIN

2 If necessary, use :

1 Contact-Socket EN3155-003F2222

(d) Modify the parity of the FWC-2.

1 If, during accomplishment of SUBTASK 313125-941-002 002 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCEAB Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCEAB Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCEAB Sheet 02).

b If necessary, use :

1 Contact-Socket EN3155-003F2222

2 If, during accomplishment of SUBTASK 313125-941-002 002 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCFAB Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCFAB Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCFAB Sheet 02).

b If necessary, use :

1 Contact-Socket EN3155-003F2222

**CONF 003

(1) Subtask 313125-020-001-001 - Remove the FWCs (1WW1 and 1WW2) from the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-000-801

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 42

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C@A330

SERVICE BULLETIN

(a) Remove (Refer to AMM Task 31-53-34-000-801) :

FIN 1WW1

1 FWC LA2E0060D8K0000

and

FIN 1WW2

1 FWC LA2E0060D8K0000

(2) Subtask 313125-831-003-001 - Modify the FWCs (1WW1 and 1WW2).

References

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS LA2E2-31-007

AIRBUS FRANCE SAS LA2E2-31-008

(a) On bench, follow instructions given in the Vendor Service Bulletins to modify the

FWCs (1WW1 and 1WW2) (Refer to AIRBUS FRANCE SAS Service Bulletin No.

LA2E2-31-007 and AIRBUS FRANCE SAS Service Bulletin No. LA2E2-31-008).

(3) Subtask 313125-831-004-002 - Modify the Wiring in the Main Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 821

Panel 131AW, Panel 131BW, Panel 132CW

Work location Electrical panel 800VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

EN3155-015F2018 6 Contact

References

Fig. A-FBAAA Sheet 01 - Location of the Equipment

Fig. A-FCAAB Sheet 01 - Modification of the Pin

Programming of the FWC-1

Sheet 02 - Modification of the Pin

Programming of the FWC-1

Fig. A-FCBAB Sheet 01 - Modification of the Pin

Programming of the FWC-2

Sheet 02 - Modification of the Pin

Programming of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 43

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C@A330

SERVICE BULLETIN

References

Fig. A-FCCAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCDAA Sheet 01 - Modification of the Parity of the

FWC-1

Sheet 02 - Modification of the Parity of the

FWC-1

Fig. A-FCEAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

Fig. A-FCFAA Sheet 01 - Modification of the Parity of the

FWC-2

Sheet 02 - Modification of the Parity of the

FWC-2

(a) Modify the pin programming of the FWC-1.

1 Modify the connection of the wire shown on the wiring diagram Fig. A-FCAAB

Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCAAB Sheet 02).

2 If necessary, use :

1 Contact EN3155-015F2018

(b) Modify the parity of the FWC-1.

1 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCCAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCCAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCCAA Sheet 02).

b If necessary, use :

1 Contact EN3155-015F2018

2 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCDAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCDAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCDAA Sheet 02).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 44

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C@A330

SERVICE BULLETIN

b If necessary, use :

1 Contact EN3155-015F2018

(c) Modify the pin programming of the FWC-2.

1 Modify the connection of the wire shown on the wiring diagram Fig. A-FCBAB

Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCBAB Sheet 02).

2 If necessary, use :

1 Contact EN3155-015F2018

(d) Modify the parity of the FWC-2.

1 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCEAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCEAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCEAA Sheet 02).

b If necessary, use :

1 Contact EN3155-015F2018

2 If, during accomplishment of SUBTASK 313125-941-002 001 Parity

Configuration Recording , you recorded that the existing aircraft wiring

corresponded to line 1 of Fig. A-FCFAA Sheet 02 :

a Modify the connection of the wire shown on the wiring diagram Fig. AFCFAA Sheet 01 and as given in the Hook-up Chart lines :

- 1 and 2 (Refer to Fig. A-FCFAA Sheet 02).

b If necessary, use :

1 Contact EN3155-015F2018

(4) Subtask 313125-420-001-001 - Install the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 45

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C@A330

SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2E20202T20000 2 FWC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Install AMM Task 31-53-34-400-801 :

FIN 1WW1

1 FWC LA2E20202T20000

and

FIN 1WW2

1 FWC LA2E20202T20000

**CONF 004

(1) Subtask 313125-020-001-001 - Remove the FWCs (1WW1 and 1WW2) from the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-000-801

(a) Remove (Refer to AMM Task 31-53-34-000-801) :

FIN 1WW1

1 FWC LA2E0060D8K0000

and

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 46

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C@A330

SERVICE BULLETIN

FIN 1WW2

1 FWC LA2E0060D8K0000

(2) Subtask 313125-831-003-001 - Modify the FWCs (1WW1 and 1WW2).

References

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS LA2E2-31-007

AIRBUS FRANCE SAS LA2E2-31-008

(a) On bench, follow instructions given in the Vendor Service Bulletins to modify the

FWCs (1WW1 and 1WW2) (Refer to AIRBUS FRANCE SAS Service Bulletin No.

LA2E2-31-007 and AIRBUS FRANCE SAS Service Bulletin No. LA2E2-31-008).

(3) Subtask 313125-831-004-006 - Modify the Wiring in the Main Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 821

Panel 131AW, Panel 131BW, Panel 132CW

Work location Electrical panel 800VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

EN3155-015F2018 4 Contact

References

Fig. A-FBAAA Sheet 01 - Location of the Equipment

Fig. A-FCAAE Sheet 01 - Modification of the Pin

Programming of the FWC-1

Sheet 02 - Modification of the Pin

Programming of the FWC-1

Fig. A-FCBAE Sheet 01 - Modification of the Pin

Programming of the FWC-2

Sheet 02 - Modification of the Pin

Programming of the FWC-2

(a) Modify the pin programming of the FWC-1.

1 Modify the connections of the wires shown on the wiring diagram Fig. AFCAAE Sheet 01 and as given in the Hook-up Chart lines :

- 1 thru 4 (Refer to Fig. A-FCAAE Sheet 02).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 47

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C@A330

SERVICE BULLETIN

2 If necessary, use :

2 Contact EN3155-015F2018

(b) Modify the pin programming of the FWC-2.

1 Modify the connections of the wires shown on the wiring diagram Fig. AFCBAE Sheet 01 and as given in the Hook-up Chart lines :

- 1 thru 4 (Refer to Fig. A-FCBAE Sheet 02).

2 If necessary, use :

2 Contact EN3155-015F2018

(4) Subtask 313125-420-001-001 - Install the FWCs (1WW1 and 1WW2) in the Main Rack

800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 811

Work location Electrical panel 800VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2E20202T20000 2 FWC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Install AMM Task 31-53-34-400-801 :

FIN 1WW1

1 FWC LA2E20202T20000

and

FIN 1WW2

1 FWC LA2E20202T20000

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 48

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SERVICE BULLETIN

D. TEST

**CONF 001

(1) Subtask 313125-700-001-001 - Test after Replacement/Modification of the FWCs

(1WW1 and 1WW2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Do the test after installation of the FWCs (1WW1 and 1WW2) (Refer to AMM Task

31-53-34-400-801).

NOTE: The AMM procedure above includes the usual test and an

additional check. The additional check is for a computer modified by

OBRM replacement. If the installed computer is modified by OBRM,

you must do the additional check.

(2) Subtask 313125-700-002-001 - Tests after the Modification of the Pin Programming

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-50-00-740-805

Task 31-50-00-991-001

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Do the usual checks on each connector which was disconnected (Refer to ESPM

20-52-10).

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Read and decode the FWC pin programming (Refer to AMM Task

31-50-00-740-805).

Print the results for the FWC.

NOTE: Make sure that the parity status is OK.

NOTE: Make sure that the 2nd digit of the 1st set of 4 digits of

the 4th line is set to 1, corresponding to the activation of

the ENGINE FEEDLINE BURST MONIT. (see example of pin

programming reading for the FWC 1(2) in the AMM figure AMM

Task 31-50-00-991-001).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 49

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SERVICE BULLETIN

(c) Test of the connectors 2822VC, 2824VC, 2826VC and 2828VC

1 These connectors are tested when reading and decoding the FWC pin

programming (Refer to AMM Task 31-50-00-740-805).

(3) Subtask 313125-700-003-001 - Tests after Cancellation of the OEBs

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-51-00-610-802

(a) On aircraft equipped with OEB REMINDER function, if the Electronic Centralized

Aircraft Monitoring (ECAM) warning has been flagged as described in OEB 61 the

following code should be deleted from the FWC database :

CODE WARN STS

71/00/800/080 YES NO

Refer to AMM Task 31-51-00-610-802.

(b) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 68, the following code should be deleted from the

FWC database :

CODE WARN STS

34/43/010/080 YES NO

Refer to AMM Task 31-51-00-610-802.

(c) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 69, the following code should be deleted from the

FWC database :

CODE WARN STS

28/21/130/086 YES NO

28/21/140/088 YES NO

Refer to AMM Task 31-51-00-610-802.

**CONF 002

(1) Subtask 313125-700-001-001 - Test after Replacement/Modification of the FWCs

(1WW1 and 1WW2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 50

5

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SERVICE BULLETIN

(a) Do the test after installation of the FWCs (1WW1 and 1WW2) (Refer to AMM Task

31-53-34-400-801).

NOTE: The AMM procedure above includes the usual test and an

additional check. The additional check is for a computer modified by

OBRM replacement. If the installed computer is modified by OBRM,

you must do the additional check.

(2) Subtask 313125-700-002-002 - Tests after the Modification of the Pin Programming

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-50-00-740-805

Task 31-50-00-991-001

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Do the usual checks on each connector which was disconnected (Refer to ESPM

20-52-10).

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Read and decode the FWC pin programming (Refer to AMM Task

31-50-00-740-805).

Print the results for the FWC.

NOTE: Make sure that the parity status is OK.

NOTE: Make sure that the 2nd digit of the 1st set of 4 digits of

the 4th line is set to 1, corresponding to the activation of

the ENGINE FEEDLINE BURST MONIT. (see example of pin

programming reading for the FWC 1(2) in the AMM figure AMM

Task 31-50-00-991-001).

(c) Test of the connectors 2959VC, 2961VC, 2967VC and 2969VC

1 These connectors are tested when reading and decoding the FWC pin

programming (Refer to AMM Task 31-50-00-740-805).

(3) Subtask 313125-700-003-001 - Tests after Cancellation of the OEBs

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-51-00-610-802

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 51

5

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SERVICE BULLETIN

(a) On aircraft equipped with OEB REMINDER function, if the Electronic Centralized

Aircraft Monitoring (ECAM) warning has been flagged as described in OEB 61 the

following code should be deleted from the FWC database :

CODE WARN STS

71/00/800/080 YES NO

Refer to AMM Task 31-51-00-610-802.

(b) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 68, the following code should be deleted from the

FWC database :

CODE WARN STS

34/43/010/080 YES NO

Refer to AMM Task 31-51-00-610-802.

(c) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 69, the following code should be deleted from the

FWC database :

CODE WARN STS

28/21/130/086 YES NO

28/21/140/088 YES NO

Refer to AMM Task 31-51-00-610-802.

**CONF 003

(1) Subtask 313125-700-001-001 - Test after Replacement/Modification of the FWCs

(1WW1 and 1WW2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Do the test after installation of the FWCs (1WW1 and 1WW2) (Refer to AMM Task

31-53-34-400-801).

NOTE: The AMM procedure above includes the usual test and an

additional check. The additional check is for a computer modified by

OBRM replacement. If the installed computer is modified by OBRM,

you must do the additional check.

(2) Subtask 313125-700-002-001 - Tests after the Modification of the Pin Programming

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 52

5

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 31-50-00-740-805

Task 31-50-00-991-001

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Do the usual checks on each connector which was disconnected (Refer to ESPM

20-52-10).

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Read and decode the FWC pin programming (Refer to AMM Task

31-50-00-740-805).

Print the results for the FWC.

NOTE: Make sure that the parity status is OK.

NOTE: Make sure that the 2nd digit of the 1st set of 4 digits of

the 4th line is set to 1, corresponding to the activation of

the ENGINE FEEDLINE BURST MONIT. (see example of pin

programming reading for the FWC 1(2) in the AMM figure AMM

Task 31-50-00-991-001).

(c) Test of the connectors 2822VC, 2824VC, 2826VC and 2828VC

1 These connectors are tested when reading and decoding the FWC pin

programming (Refer to AMM Task 31-50-00-740-805).

(3) Subtask 313125-700-003-001 - Tests after Cancellation of the OEBs

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-51-00-610-802

(a) On aircraft equipped with OEB REMINDER function, if the Electronic Centralized

Aircraft Monitoring (ECAM) warning has been flagged as described in OEB 61 the

following code should be deleted from the FWC database :

CODE WARN STS

71/00/800/080 YES NO

Refer to AMM Task 31-51-00-610-802.

(b) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 68, the following code should be deleted from the

FWC database :

CODE WARN STS

34/43/010/080 YES NO

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 53

5

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C@A330

SERVICE BULLETIN

Refer to AMM Task 31-51-00-610-802.

(c) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 69, the following code should be deleted from the

FWC database :

CODE WARN STS

28/21/130/086 YES NO

28/21/140/088 YES NO

Refer to AMM Task 31-51-00-610-802.

**CONF 004

(1) Subtask 313125-700-001-001 - Test after Replacement/Modification of the FWCs

(1WW1 and 1WW2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Do the test after installation of the FWCs (1WW1 and 1WW2) (Refer to AMM Task

31-53-34-400-801).

NOTE: The AMM procedure above includes the usual test and an

additional check. The additional check is for a computer modified by

OBRM replacement. If the installed computer is modified by OBRM,

you must do the additional check.

(2) Subtask 313125-700-002-004 - Test after the Modification of the Pin Programming

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-50-00-740-805

Task 31-50-00-991-001

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Do the usual checks on each connector which was disconnected (Refer to ESPM

20-52-10).

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Read and decode the FWC pin programming (Refer to AMM Task

31-50-00-740-805).

Print the results for the FWC.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 54

5

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SERVICE BULLETIN

NOTE: Make sure that the parity status is OK.

NOTE: Make sure that the 2nd digit of the 1st set of 4 digits of

the 4th line is set to 1, corresponding to the activation of

the ENGINE FEEDLINE BURST MONIT. (see example of pin

programming reading for the FWC 1(2) in the AMM figure AMM

Task 31-50-00-991-001).

NOTE: Make sure that the 2nd digit of the 1st set of 4 digits of the 6th line

is set to 0, corresponding to the de-activation of the HUD OPTION

INSTALLED (see example of pin programming reading for the FWC

1(2) in the AMM figure AMM Task 31-50-00-991-001).

(c) Test of the connectors 2822VC, 2824VC, 2826VC and 2828VC

1 These connectors are tested when reading and decoding the FWC pin

programming (Refer to AMM Task 31-50-00-740-805).

(3) Subtask 313125-700-003-001 - Tests after Cancellation of the OEBs

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-51-00-610-802

(a) On aircraft equipped with OEB REMINDER function, if the Electronic Centralized

Aircraft Monitoring (ECAM) warning has been flagged as described in OEB 61 the

following code should be deleted from the FWC database :

CODE WARN STS

71/00/800/080 YES NO

Refer to AMM Task 31-51-00-610-802.

(b) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 68, the following code should be deleted from the

FWC database :

CODE WARN STS

34/43/010/080 YES NO

Refer to AMM Task 31-51-00-610-802.

(c) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB 69, the following code should be deleted from the

FWC database :

CODE WARN STS

28/21/130/086 YES NO

28/21/140/088 YES NO

Refer to AMM Task 31-51-00-610-802.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 55

5

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SERVICE BULLETIN

E. CLOSE-UP

**CONF 001

(1) Subtask 313125-410-001-002 - Install/Close Items Removed/Opened for access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-400-801

Task 52-10-00-410-801

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

(a) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(b) In the FWD cargo-compartment at FR20, install the partition panels 131AW, 131BW

and 132CW (Refer to AMM Task 25-52-00-400-801).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802 or AMM Task

52-30-00-410-804).

(2) Subtask 313125-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Do the close-up procedure as specified in the installation of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-400-801).

(b) Restore the systems and the aircraft to normal operating condition.

(c) Remove the access platform(s).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 56

5

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C@A330

SERVICE BULLETIN

**CONF 002

(1) Subtask 313125-410-001-002 - Install/Close Items Removed/Opened for access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-400-801

Task 52-10-00-410-801

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

(a) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(b) In the FWD cargo-compartment at FR20, install the partition panels 131AW, 131BW

and 132CW (Refer to AMM Task 25-52-00-400-801).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802 or AMM Task

52-30-00-410-804).

(2) Subtask 313125-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Do the close-up procedure as specified in the installation of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-400-801).

(b) Restore the systems and the aircraft to normal operating condition.

(c) Remove the access platform(s).

**CONF 003

(1) Subtask 313125-410-001-002 - Install/Close Items Removed/Opened for access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 57

5

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C@A330

SERVICE BULLETIN

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-400-801

Task 52-10-00-410-801

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

(a) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(b) In the FWD cargo-compartment at FR20, install the partition panels 131AW, 131BW

and 132CW (Refer to AMM Task 25-52-00-400-801).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802 or AMM Task

52-30-00-410-804).

(2) Subtask 313125-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Do the close-up procedure as specified in the installation of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-400-801).

(b) Restore the systems and the aircraft to normal operating condition.

(c) Remove the access platform(s).

**CONF 004

(1) Subtask 313125-410-001-002 - Install/Close Items Removed/Opened for access

Work Zones and Access Panels

Zone Access/Work location

210

130 Work location Frame 20

Manpower Resources

Skills AIRFRAME

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 58

5

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-400-801

Task 52-10-00-410-801

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

(a) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(b) In the FWD cargo-compartment at FR20, install the partition panels 131AW, 131BW

and 132CW (Refer to AMM Task 25-52-00-400-801).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802 or AMM Task

52-30-00-410-804).

(2) Subtask 313125-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-53-34-400-801

(a) Do the close-up procedure as specified in the installation of the FWCs (1WW1 and

1WW2) (Refer to AMM Task 31-53-34-400-801).

(b) Restore the systems and the aircraft to normal operating condition.

(c) Remove the access platform(s).

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 59

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003 thru 004

1WW2

1WW1

800VU

FR20

FR18

A

Z120

A

G_SB_313125_5_BAAA_01_00

882VU

Figure A-FBAAA - Sheet 01

Location of the Equipment

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 60

5

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C@A330

SERVICE BULLETIN

**CONF 002

1WW2

1WW1

800VU

FR20

FR18

A

Z120

A

G_SB_313125_5_BAAB_01_00

809VU

Figure A-FBAAB - Sheet 01

Location of the Equipment

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 61

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

Figure A-FCAAB - Sheet 01

Modification of the Pin Programming of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 62

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2826VC−A 30 3152−1267 2M CF24 831VU 1WW1−AE 7B M1O

 2 882VU 2828VC−A 30 EN3155−015F2018 3152−1267 2M CF24 831VU 1WW1−AE 7B M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCAAB - Sheet 02

Modification of the Pin Programming of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 63

5

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C@A330

SERVICE BULLETIN

**CONF 002

Figure A-FCAAC - Sheet 01

Modification of the Pin Programming of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 64

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@A330

SERVICE BULLETIN

**CONF 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 809VU 2961VC−A 71 3152−1267 2M CF24 831VU 1WW1−AE 7B M1O

 2 809VU 2959VC−A 71 EN3155−003F2222 3152−1267 2M CF24 831VU 1WW1−AE 7B M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCAAC - Sheet 02

Modification of the Pin Programming of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 65

5

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C@A330

SERVICE BULLETIN

**CONF 004

Figure A-FCAAE - Sheet 01

Modification of the Pin Programming of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 66

5

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C@A330

SERVICE BULLETIN

**CONF 004

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2828VC−A 35 3152−0715 2M CF24 831VU 1WW1−AD 13D M1O

 2 882VU 2826VC−A 35 EN3155−015F2018 3152−0715 2M CF24 831VU 1WW1−AD 13D M1N

 3 882VU 2826VC−A 30 3152−1267 2M CF24 831VU 1WW1−AE 7B M1O

 4 882VU 2828VC−A 30 EN3155−015F2018 3152−1267 2M CF24 831VU 1WW1−AE 7B M1N

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCAAE - Sheet 02

Modification of the Pin Programming of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 67

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

Figure A-FCCAA - Sheet 01

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 68

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2828VC−A 45 3152−0716 2M CF24 831VU 1WW1−AD 14D M1O

 2 882VU 2826VC−A 45 EN3155−015F2018 3152−0716 2M CF24 831VU 1WW1−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCCAA - Sheet 02

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 69

5

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C@A330

SERVICE BULLETIN

**CONF 002

Figure A-FCCAB - Sheet 01

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 70

5

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C@A330

SERVICE BULLETIN

**CONF 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 809VU 2959VC−A 68 3152−0716 2M CF24 831VU 1WW1−AD 14D M1O

 2 809VU 2961VC−A 68 EN3155−003F2222 3152−0716 2M CF24 831VU 1WW1−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCCAB - Sheet 02

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 71

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

Figure A-FCDAA - Sheet 01

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 72

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2826VC−A 45 3152−0716 2M CF24 831VU 1WW1−AD 14D M1O

 2 882VU 2828VC−A 45 EN3155−015F2018 3152−0716 2M CF24 831VU 1WW1−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCDAA - Sheet 02

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 73

5

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C@A330

SERVICE BULLETIN

**CONF 002

Figure A-FCDAB - Sheet 01

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 74

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@A330

SERVICE BULLETIN

**CONF 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 809VU 2961VC−A 68 3152−0716 2M CF24 831VU 1WW1−AD 14D M1O

 2 809VU 2959VC−A 68 EN3155−003F2222 3152−0716 2M CF24 831VU 1WW1−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCDAB - Sheet 02

Modification of the Parity of the FWC-1

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 75

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

Figure A-FCBAB - Sheet 01

Modification of the Pin Programming of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 76

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2822VC−A 30 3152−1287 2M CF24 832VU 1WW2−AE 7B M1O

 2 882VU 2824VC−A 30 EN3155−015F2018 3152−1287 2M CF24 832VU 1WW2−AE 7B M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCBAB - Sheet 02

Modification of the Pin Programming of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 77

5

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C@A330

SERVICE BULLETIN

**CONF 002

Figure A-FCBAC - Sheet 01

Modification of the Pin Programming of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 78

5

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C@A330

SERVICE BULLETIN

**CONF 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 809VU 2969VC−A 50 3152−1287 2M CF24 832VU 1WW2−AE 7B M1O

 2 809VU 2967VC−A 50 EN3155−003F2222 3152−1287 2M CF24 832VU 1WW2−AE 7B M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCBAC - Sheet 02

Modification of the Pin Programming of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 79

5

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C@A330

SERVICE BULLETIN

**CONF 004

Figure A-FCBAE - Sheet 01

Modification of the Pin Programming of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 80

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@A330

SERVICE BULLETIN

**CONF 004

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2824VC−A 35 3152−0784 2M CF24 832VU 1WW2−AD 13D M1O

 2 882VU 2822VC−A 35 EN3155−015F2018 3152−0784 2M CF24 832VU 1WW2−AD 13D M1N

 3 882VU 2822VC−A 30 3152−1287 2M CF24 832VU 1WW2−AE 7B M1O

 4 882VU 2824VC−A 30 EN3155−015F2018 3152−1287 2M CF24 832VU 1WW2−AE 7B M1N

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCBAE - Sheet 02

Modification of the Pin Programming of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 81

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

Figure A-FCEAA - Sheet 01

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 82

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@A330

SERVICE BULLETIN

**CONF 001, 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2824VC−A 45 3152−0785 2M CF24 832VU 1WW2−AD 14D M1O

 2 882VU 2822VC−A 45 EN3155−015F2018 3152−0785 2M CF24 832VU 1WW2−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCEAA - Sheet 02

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 83

5

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C@A330

SERVICE BULLETIN

**CONF 002

Figure A-FCEAB - Sheet 01

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 84

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@A330

SERVICE BULLETIN

**CONF 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 809VU 2967VC−A 68 3152−0785 2M CF24 832VU 1WW2−AD 14D M1O

 2 809VU 2969VC−A 68 EN3155−003F2222 3152−0785 2M CF24 832VU 1WW2−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCEAB - Sheet 02

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 85

5

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C@A330

SERVICE BULLETIN

**CONF 001, 003

Figure A-FCFAA - Sheet 01

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 86

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@A330

SERVICE BULLETIN

**CONF 001, 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 882VU 2822VC−A 45 3152−0785 2M CF24 832VU 1WW2−AD 14D M1O

 2 882VU 2824VC−A 45 EN3155−015F2018 3152−0785 2M CF24 832VU 1WW2−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCFAA - Sheet 02

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 87

5

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C@A330

SERVICE BULLETIN

**CONF 002

Figure A-FCFAB - Sheet 01

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 88

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@A330

SERVICE BULLETIN

**CONF 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 809VU 2969VC−A 68 3152−0785 2M CF24 832VU 1WW2−AD 14D M1O

 2 809VU 2967VC−A 68 EN3155−003F2222 3152−0785 2M CF24 832VU 1WW2−AD 14D M1N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCFAB - Sheet 02

Modification of the Parity of the FWC-2

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 89

5

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C@A330

SERVICE BULLETIN

REPORTING SHEET

TITLE: INDICATING / RECORDING SYSTEMS - FLIGHT WARNING COMPUTER

(FWC) - INSTALL FWC STANDARD T2-0.

MODIFICATION No.: 51926S17857 56729S19417 58440S30619

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): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 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

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

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

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service 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 below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Dec 31/08 SERVICE BULLETIN No.: A330-31-3125

REVISION No.: 00 - Dec 31/08 Page: 1

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