@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

MODIFICATION No.: 58773S30712

This page transmits Revision No.02 of Service Bulletin No.A330-92-3088

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 02 issued to take into account connector PN MS3456KT24-10S :

- Material paragraph modified, COMPA01 added,

- Accomplishment instructions paragraph modified.

CHANGES

Layout changes due to computerization of this revision are not identified.

SUMMARY

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Material Effectivity MATERIAL EFFECTIVITY ADDED N

MATERIAL EFFECTIVITY DELETED FOR

APPLICABLE MSN

D

COMPLIANCE

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

REVISION No.: 02 - Sep 01/10 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL SET UPDATED

R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

LIST OF COMPONENTS

Kit 923088A01R02 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Minor editorial or document structure change R

Consumable Materials CONSUMABLE MATERIALS PARAGRAPH ADDED N

Components COMPONENTS PARAGRAPH ADDED N

Component COMPA01 PART MATERIAL SET ADDED N

Equipment EQUIPMENT PARAGRAPH ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 923088- 831-801-001-Modification

Subtask 923088-910-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 923088-831-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 923088-831-002-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

REVISION No.: 02 - Sep 01/10 Page: 2

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 923088-831-003-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Fig. A-FADAA

Fig. A-FADAA Sheet 01 SHEET UPDATED R

Fig. A-FAEAA FIGURE SOLUTION ADDED N

Fig. A-FAEAA Sheet 01 SHEET ADDED N

Appendix 01

APPENDIX CONTENT APPENDIX CONTENT UPDATED R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to change the commercial policy and to create a Kit.

REVISION SEQUENCE

ORIGINAL: Sep 02/09

REVISION No. : 01 - Feb 22/10

REVISION No. : 02 - Sep 01/10

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

REVISION No.: 02 - Sep 01/10 Page: 4

5

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@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.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 58773S30712

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

Several A330/A340 aircraft family operators have reported in service occurrences of hydraulic pump

electrical motor connector internal arcing resulting in false hydraulic system overheat Electronic

Centralized Aircraft Monitoring (ECAM) warnings and/or hydraulic pump electrical motor malfunction.

Investigations have shown that under some conditions of the cables and the connectors rear grommet

manufacturing tolerances, there is a possible path for fluid ingress resulting in the connector internal

arcing and hydraulic system failure.

This modification introduces heat shrink sleeves to the rear of the gauge 12 and 10 cable contacts and

a sealing plug to the connector free cavity to increase the water tightness of the hydraulic pump

electrical motor connectors 1JCA, 1JJA and 1JVA.

The accomplishment of this Service Bulletin will prevent the possible hydraulic pump electrical motor

connectors fluid ingress from the rear of the connector grommet and will prevent the false hydraulic

system overheat ECAM warnings and/or hydraulic pump electrical motor malfunction.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 923088A01R02 1 877.00 Tubing-heat, Tie-cables, Sealing plugs,

Sockets, Sleeve reducers

Component COMPA01 1 See SB Sockets, Sleeve reducers

EFFECTIVITY

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

44W 46W 99Y AAR ACA ACI AEA AFL AFR ALK ASY AVA AZA

BEC BEL BMA BTV CAL CCA CES CHH CPA CRL CSN CYP DAH

DAL DGA DLH EDW EEZ EIN ETD EVA FIN FWI GFA GIA GRL

HDA HFY HVN I2L IAC IWD IYE JAI JST KAL KFR KKK KLM

LTU LVG MAS MAU MEA MON MSR MXA OBS OHY PAL QAF QFA

QTR SAS SGX SIA STZ SWR TAM TAP TCX THA THY TSC UAE

USA VKG VLK XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER OIT : SE 999.0040/09 dated 25 May 2009

OTHER SBIT : SEMB/914.0742/09

OTHER SBIT : SEMB F92M10018658 dated 6 May 2010

OTHER SBIT : 10-0034 dated 23 August 2010

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

SUMMARY

MANPOWER

Task 923088-831-801-001: Modification

TOTAL MANHOURS 12.50

ELAPSED TIME (HOURS) 4.50

APPENDICES

Appendix 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

G_SB_923088_5_SAAA_01_00

1JVA

1JJA

1JCA

Figure A-FSAAA - Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

REVISION No.: 02 - Sep 01/10 Page: 4

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@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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

MODIFICATION No.: 58773S30712

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

(1) Models

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

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

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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@A330

SERVICE BULLETIN

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

0652-0659 0661-0667 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 0961-0971 0973-0979 0982-0986 0988-0991 0994 0998

(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

44W 0943 0962 0970 0979

46W 0871

99Y 0747 0951

AAR 0640 0676 0708 0772 0803 0845

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0733 0745 0749 0814 0931 0950

AFL 0963 0973

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

0567 0584 0657

ALK 0303 0306 0311 0313

ASY 0969

AVA 0948 0967

AZA 0272 0339

BEC 0863

BEL 0030 0037 0045 0082

BMA 0398 0401 0404

BTV 0205 0330

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

0805 0823 0838 0861 0920

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 0982

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

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

DAL 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

DGA 0240

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

0913 0922 0989

EDW 0369

EEZ 0665 0802 0822

EIN 0059 0269 0397 0841 0847 0985

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

0854 0868 0975 0991

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

FIN 0994

FWI 0253 0758 0965

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532

GIA 0138 0140 0144 0148 0153 0165 0988

GRL 0230

HDA 0106 0132 0234 0405 0479 0512 0581 0654 0662 0692 0716 0741

0786

HFY 0096

HVN 0087 0255 0262 0275 0294 0299 0366

I2L 0211

IAC 0353 0362

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 0945

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

KKK 0358 0364

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 0926 0984 0998

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

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SERVICE BULLETIN

OPERATOR MSN

MXA 0966 0971

OBS 0461

OHY 0098

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 0976

QTR 0441 0473 0489 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

SAS 0496 0497 0515 0568

SGX 0407

SIA 0978 0983 0986

STZ 0324

SWR 0229 0249 0288 0291 0322 0343

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

0949 0961 0968 0977

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

0990

THY 0463 0504 0697 0704 0742 0754 0774

TSC 0111 0177 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

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388

VKG 0309 0349 0356 0357

VLK 0055 0070 0086

XAX 0054 0952 0974

XLF 0501 0635

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0059 0060 0062

0064 0065 0066 0067 0069 0070 0071 0072 0073 0077 0082

0083 0086 0087 0095 0096 0098 0099 0100 0102 0106 0107

0109 0110 0111 0112 0113 0116 0118 0119 0120 0121 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 0223 0224 0226

0229 0230 0231 0232 0234 0238 0240 0241 0244 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

0346 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 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 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

001

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@A330

SERVICE BULLETIN

MSN CONFIGURATION

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 0962 0963 0964

0965 0966 0967 0968 0969 0970 0971 0973 0974 0975 0976

0977 0978 0979 0982 0983 0984 0985 0986 0988 0989 0990

0991 0994 0998

001

(5) Configuration definition

**CONF 001

Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

NOTE: On the same aircraft, it is possible to find both connectors PN

ASNE0233-24-10S and PN MS3456KT24-10S.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 923088A01R02 1

Component COMPA01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Several A330/A340 aircraft family operators have reported in service occurrences of

hydraulic pump electrical motor connector internal arcing resulting in false hydraulic

system overheat Electronic Centralized Aircraft Monitoring (ECAM) warnings and/or

hydraulic pump electrical motor malfunction. Investigations have shown that under some

conditions of the cables and the connectors rear grommet manufacturing tolerances,

there is a possible path for fluid ingress resulting in the connector internal arcing and

hydraulic system failure.

(2) Objective/Action

This modification introduces heat shrink sleeves to the rear of the gauge 12 and 10

cable contacts and a sealing plug to the connector free cavity to increase the water

tightness of the hydraulic pump electrical motor connectors 1JCA, 1JJA and 1JVA.

(3) Advantages

The accomplishment of this Service Bulletin will prevent the possible hydraulic pump

electrical motor connectors fluid ingress from the rear of the connector grommet and will

prevent the false hydraulic system overheat ECAM warnings and/or hydraulic pump

electrical motor malfunction.

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 923088-831-801-001: Modification

(1) Modify the equipment 1JCA

(2) Modify the equipment 1JJA

(3) Modify the equipment 1JVA

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is requested within 3600 FH from AD effective

date.

Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an

Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA).

The AD must be used as the reference document for the mandatory accomplishment

timescale.

F. APPROVAL

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

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.

Task 923088-831-801-001: Modification

Get Access 3.00

On Aircraft

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Task 923088-831-801-001: Modification

Modify the equipment 1JCA 2.00

Modify the equipment 1JJA 2.00

Modify the equipment 1JVA 2.00

Tests 0.50

Close-Up 3.00

TOTAL MANHOURS 12.50

ELAPSED TIME (HOURS) 4.50

NOTE: For detail concerning the elapsed time assumptions, refer to Appendix 01 .

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 12-34-24

29-21-51 29-22-51 29-23-51

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-34 20-42-12

20-48-23 20-48-41 20-55-00

Standards Manual (SM)

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is :

Kit 923088A01R02 AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering modification kits by fax: +49 40

50 76 25 90

For ordering of single spares by fax: +49 40

50 76 40 13

(2) Price and Availability

Kit 923088A01R02

Cost 877.00 USD

Availability 60 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will provide this Service Bulletin kit at no charge for orders placed before December

2012. AIRBUS will also credit the manhours indicated in this Service Bulletin at the operator’s

agreed in-house warranty labor rate. Some Operators will require reducer PN NSA938186-04

and socket PN NSA938192DC0802 for connector PN MS3456KT24-10S as an alternative to

PN ASNE0233-24-10S. These two parts should be sourced directly by the Operator and will

be reimbursed by Airbus. Claims must be received not later than 90 days after completion of

the last affected aircraft of your fleet

C. LIST OF COMPONENTS

Kit 923088A01R02

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

NOTES

E0347DR0801 6 SOCKET E0347DR0801

E0616BB0800 30 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

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

NOTES

NSA935401-04 30 TIE

NSA938186-03 6 REDUCER

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.

NOTE: For information, kits 923088A01R00 and 923088A01R02 contents are

identical.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

Component COMPA01

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

NOTES

NSA938186-04 3 REDUCER

NSA938192DC0802 6 SOCKET NSA938192DC0802

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

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 923088-831-801-001 - 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.

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

Task Associated Data

Zone

147 195 196

Modified FIN

1JCA 1JJA 1JVA

Manpower

TOTAL MANHOURS 12.50

ELAPSED TIME (HOURS) 4.50

A. GENERAL

(1) Subtask 923088-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-53, Page Block 001

Task 12-34-24-860-802

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

20-33-34

20-42-12

20-48-23

20-48-41

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

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(b) Obey the instructions for the heat shrink sleeves installation, (Refer to ESPM

20-33-34).

(c) For the description and the primary characteristics of the heat shrink sleeves,

(Refer to ESPM 20-42-12).

(d) Obey the instructions for the crimping, (Refer to ESPM 20-48-23).

(e) Obey the instructions for the blanking plugs installation, (Refer to ESPM 20-48-41).

(f) For the identification of the frames (FR), (Refer to AMM 06-31-53, Page Block 001).

(g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block

001).

(2) Subtask 923088-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 923088-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

195

196

147

Manpower Resources

Skills NON SPECIFIC

References

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

Task 29-21-51-000-801

Task 29-22-51-000-801

Task 29-23-51-000-801

(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 Green Electric

Pump (1JV), (Refer to AMM Task 29-21-51-000-801).

(d) Do the preparation procedure as specified in the removal of the Blue Electric Pump

(1JC), (Refer to AMM Task 29-22-51-000-801).

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(e) Do the preparation procedure as specified in the removal of the Yellow Electric

Pump (1JJ), (Refer to AMM Task 29-23-51-000-801).

C. PROCEDURE

(1) Subtask 923088-831-001-001 - Modify the equipment 1JCA

Work Zones and Access Panels

Zone Access/Work location

195 Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 923088A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

E0347DR0801 2 SOCKET

E0616BB0800 10 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

NSA935401-04 10 TIE

NSA938186-03 2 REDUCER

NOTE: For information, kits 923088A01R00 and 923088A01R02 contents are

identical.

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA938186-04 1 REDUCER

NSA938192DC0802 2 SOCKET

References

Aircraft Wiring List (AWL)

Fig. A-FAAAA

Location of the equipment

Sheet 01

Fig. A-FADAA

Installation of the heat shrinking sleeves

Sheet 01

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

(a) Pb suppression LOC A01S01

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(b) If connector PN ASNE0233-24-10S is installed :

1 Disconnect the plug 1JCA.

2 Disconnect the wire 2922-0099 (gauge DK10) from the plug 1JCA (if installed).

3 Remove :

1 Socket E0347DR0801 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2922-0100 (gauge CF12 or DK12) from the plug 1JCA (if

installed).

7 Remove :

1 Socket E0347DR0801 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

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and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

and

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FADAA).

9 Reconnect the wires on the plug 1JCA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JCA.

(c) If connector PN MS3456KT24-10S is installed :

1 Disconnect the plug 1JCA.

2 Disconnect the wire 2922-0099 (gauge DK10) from the plug 1JCA (if installed).

3 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket NSA938192DC0802

with :

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1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2922-0100 (gauge CF12 or DK12) from the plug 1JCA (if

installed).

7 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

and

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-04

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FAEAA).

9 Reconnect the wires on the plug 1JCA (Refer to Aircraft Wiring List (AWL)).

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10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JCA.

(2) Subtask 923088-831-002-001 - Modify the equipment 1JJA

Work Zones and Access Panels

Zone Access/Work location

196 Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 923088A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

E0347DR0801 2 SOCKET

E0616BB0800 10 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

NSA935401-04 10 TIE

NSA938186-03 2 REDUCER

NOTE: For information, kits 923088A01R00 and 923088A01R02 contents are

identical.

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA938186-04 1 REDUCER

NSA938192DC0802 2 SOCKET

References

Aircraft Wiring List (AWL)

Fig. A-FABAA

Location of the equipment

Sheet 01

Fig. A-FADAA

Installation of the heat shrinking sleeves

Sheet 01

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References

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

(a) If connector PN ASNE0233-24-10S is installed :

1 Disconnect the plug 1JJA.

2 Disconnect the wire 2923-0211 (gauge DK10) from the plug 1JJA (if installed).

3 Remove :

1 Socket E0347DR0801 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2923-0212 (gauge CF12 or DK12) from the plug 1JJA (if

installed).

7 Remove :

1 Socket E0347DR0801 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

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1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

and

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FADAA).

9 Reconnect the wires on the plug 1JJA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JJA.

(b) If connector PN MS3456KT24-10S is installed :

1 Disconnect the plug 1JJA.

2 Disconnect the wire 2923-0211 (gauge DK10) from the plug 1JJA (if installed).

3 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

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5 Install on the wire :

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2923-0212 (gauge CF12 or DK12) from the plug 1JJA (if

installed).

7 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

and

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-04

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FAEAA).

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9 Reconnect the wires on the plug 1JJA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JJA.

(3) Subtask 923088-831-003-001 - Modify the equipment 1JVA

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 923088A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

E0347DR0801 2 SOCKET

E0616BB0800 10 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

NSA935401-04 10 TIE

NSA938186-03 2 REDUCER

NOTE: For information, kits 923088A01R00 and 923088A01R02 contents are

identical.

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA938186-04 1 REDUCER

NSA938192DC0802 2 SOCKET

References

Aircraft Wiring List (AWL)

Fig. A-FACAA

Location of the equipment

Sheet 01

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References

Fig. A-FADAA

Installation of the heat shrinking sleeves

Sheet 01

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

(a) If connector PN ASNE0233-24-10S is installed :

1 Disconnect the plug 1JVA.

2 Disconnect the wire 2921-0183 (gauge DK10) from the plug 1JVA (if installed).

3 Remove :

1 Socket E0347DR0801 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2921-0184 (gauge CF12 or DK12) from the plug 1JVA (if

installed).

7 Remove :

1 Socket E0347DR0801 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

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and

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

and

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FADAA).

9 Reconnect the wires on the plug 1JVA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JVA.

(b) If connector PN MS3456KT24-10S is installed :

1 Disconnect the plug 1JVA.

2 Disconnect the wire 2921-0183 (gauge DK10) from the plug 1JVA (if installed).

3 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

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5 Install on the wire :

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2921-0184 (gauge CF12 or DK12) from the plug 1JVA (if

installed).

7 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

and

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-04

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FAEAA).

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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9 Reconnect the wires on the plug 1JVA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JVA.

D. TEST

(1) Subtask 923088-865-001-001 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801

Task 29-22-51-400-801

Task 29-23-51-400-801

(a) Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the green electric pump (1JV), (Refer to AMM Task

29-21-51-400-801).

(b) Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the blue electric pump (1JC), (Refer to AMM Task

29-22-51-400-801)

(c) Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the yellow electric pump (1JJ), (Refer to AMM Task

29-23-51-400-801)

(2) Subtask 923088-710-001-001 - Operational

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801

Task 29-22-51-400-801

Task 29-23-51-400-801

(a) Do the test procedure as specified after the installation of the Green Electric Pump

(1JV), (Refer to AMM Task 29-21-51-400-801).

(b) Do the test procedure as specified after the installation of the Blue Electric Pump

(1JC), (Refer to AMM Task 29-22-51-400-801).

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

(c) Do the test procedure as specified after the installation of the Yellow Electric Pump

(1JJ), (Refer to AMM Task 29-23-51-400-801).

E. CLOSE-UP

(1) Subtask 923088-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801

Task 29-22-51-400-801

Task 29-23-51-400-801

(a) Do the close-up procedure as specified after the installation of the Green Electric

Pump (1JV), (Refer to AMM Task 29-21-51-400-801).

(b) Do the close-up procedure as specified after the installation of the Blue Electric

Pump (1JC), (Refer to AMM Task 29-22-51-400-801).

(c) Do the close-up procedure as specified after the installation of the Yellow Electric

Pump (1JJ), (Refer to AMM Task 29-23-51-400-801).

(d) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform(s).

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

**CONF ALL

FR46

FR47

A

Z195

B

1JC

A

1JCA

B

G_SB_923088_5_AAAA_01_00

FR46 FR47

BLUE ELECTRIC PUMP

Figure A-FAAAA - Sheet 01

Location of the equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

**CONF ALL

FR45

FR46

Z196

A

B

1JJ

1JJA B

G_SB_923088_5_ABAA_01_00

FR45

FR46

A

YELLOW ELECTRIC PUMP

Figure A-FABAA - Sheet 01

Location of the equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

**CONF ALL

1JV

B

B

A

1JVA

Z147

FR53.2

FR53.1

A

FR53.1

FR53.2

G_SB_923088_5_ACAA_01_00

GREEN ELECTRIC PUMP

Figure A-FACAA - Sheet 01

Location of the equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

REVISION No.: 02 - Sep 01/10 Page: 29

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SERVICE BULLETIN

**CONF ALL

CABLE GAUGE CF12 OR DK12

(L : 25 mm (0.984 in ))

SLEEVE ASNE0718−03

HEAT−SHRINKING

(L : 30 mm (1.181 in ))

SLEEVE ASNE0718−02

HEAT−SHRINKING

CONTACT

(L : 35 mm (1.378 in ))

SLEEVE ASNE0718−02

HEAT−SHRINKING

NOTE:

01 THIS INSTALLATION IS VALID FOR CONNECTOR PN ASNE0233−24−10S

01

G_SB_923088_5_ADAA_01_03

Figure A-FADAA - Sheet 01

Installation of the heat shrinking sleeves

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

**CONF ALL

CABLE GAUGE CF12 OR DK12

(L : 25 mm (0.984 in ))

SLEEVE ASNE0718−03

HEAT−SHRINKING

(L : 30 mm (1.181 in ))

SLEEVE ASNE0718−03

HEAT−SHRINKING

CONTACT

(L : 35 mm (1.378 in ))

SLEEVE ASNE0718−02

HEAT−SHRINKING

NOTE:

01 THIS INSTALLATION IS VALID FOR CONNECTOR PN MS3456KT24−10S

01

G_SB_923088_5_AEAA_01_02

Figure A-FAEAA - Sheet 01

Installation of the heat shrinking sleeves

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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This Page Intentionally Left Blank

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

Appendix 01

**CONF ALL

(1) For detail concerning the elapsed time assumption of the modification, refer to the Gantt chart

shown next page :

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

Appendix 01

**CONF ALL

G_SB_923088_5_BAAA_01_01

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−92−3088

ELAPSED TIME

(HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH ET PER

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

12.50

4.50

STEPS

0 1 2 3 4 5

GET ACCESS 3.00 1.00 3

MODIF. OF THE EQUIPMENT 1JJ−A 2.00 2.00 1

MODIFICATION 6.00 2.00 3

MODIF. OF THE EQUIPMENT 1JV−A 2.00 2.00 1

TEST 0.50 0.50 1

CLOSE−UP 3.00 1.00 3

MODIF. OF THE EQUIPMENT 1JC−A 2.00 2.00 1

Figure A-FBAAA - Sheet 01

Gantt Chart

DATE: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

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SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

MODIFICATION No.: 58773S30712

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: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

REVISION No.: 02 - Sep 01/10 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: Sep 02/09 SERVICE BULLETIN No.: A330-92-3088

REVISION No.: 02 - Sep 01/10 Page: 1

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