@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: 28

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER TANK FUEL PUMP CONTROL CIRCUIT

MODIFICATION No.: 200242H16135

This page transmits Revision No.01 of Service Bulletin No.A330-28-3113

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 01 issued to include: a preparation test procedure for the Ground Fault Interrupter FIN

97QL2.

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

APPROVAL APPROVAL UPDATED R

WEIGHT AND BALANCE Minor editorial or document structure change R

BALANCE UPDATED R

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 283113- 831-895-001-

MODIFICATION

TASK SOLUTION UPDATED

CAUTION UPDATED

R

Task associated data - 001 PANEL UPDATED R

Task associated data - 002 PANEL UPDATED R

Subtask 283113-910-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 283113-910-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 283113-831-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 283113-831-002-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 283113-831-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 283113-800-401-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

ZONE UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER UPDATED

FIN UPDATED

LOCATION UPDATED

REFERENCES UPDATED

R

Subtask 283113-710-401-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

LOCATION UPDATED

REFERENCES UPDATED

R

Subtask 283113-710-403-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

ZONE UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

REFERENCES UPDATED

R

Subtask 283113-800-402-001 SUBTASK SOLUTION ADDED N

Subtask 283113-710-401-002 SUBTASK SOLUTION ADDED N

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 2

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 283113-800-401-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 283113-710-401-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 283113-942-401-002 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

PANEL UPDATED

ZONE UPDATED

R

Subtask 283113-942-401-001 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

PANEL UPDATED

ZONE UPDATED

R

Fig. A-UBAAA FIGURE SOLUTION ADDED N

Fig. A-UBAAA Sheet 01 SHEET ADDED N

Fig. A-UBAAA Sheet 02 SHEET ADDED N

Fig. A-UBAAB FIGURE SOLUTION ADDED N

Fig. A-UBAAB Sheet 01 SHEET ADDED N

Fig. A-UBAAB Sheet 02 SHEET ADDED N

Fig. A-UAA FIGURE DELETED FOR APPLICABLE MSN D

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

No previous revision

REVISION SEQUENCE

ORIGINAL: Jul 19/11

REVISION No. : 01 - Mar 27/12

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 3

7

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 4

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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: 28

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER TANK FUEL PUMP CONTROL CIRCUIT

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 200242H16135

MINOR None

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

The European Aviation Safety Agency (EASA) has requested that Ground Fault Interrupters (GFI) are

installed into the electrical supply circuits of fuel pumps where the inlets become uncovered during

normal operation. This is in response to SFAR88 - Fuel Tank Safety.

The Evaluation Service Bulletin A330-28-3903 (Mod. No. 200241H16397) was issued for operators TAP

and UAE. The Service Bulletin A330-28-3903 introduced a GFI and related base into the electrical

supply circuit of the A330-200 aircraft right center tank transfer pump.

This Service Bulletin introduces GFI, and related bases, into the electrical supply circuits of the

A330-200 aircraft left and right center tank transfer pumps. These GFIs have the same ’footprint’ as

the existing relay/micro-contactors and physically replace them on the electrical panel. The new GFI

sockets are fool-proofed to prevent incorrectly installing normal relay/micro-contactors.

These GFIs will replace the existing 3-phase relay/micro-contactors. The function of the GFI is to

electrically isolate the pump if a ground fault condition occurs downstream of the GFI. The GFI gives

additional earth leakage protection to the downstream circuit.

Accomplishment of this Service Bulletin will not change the characteristics of the aircraft.

The embodiment of this SB affects the ALS part 5, section 5-4. This limitation is applicable to all aircraft

operated under FAA registration.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

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

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 283113A01R00 1 1,740.00 Placard Set, Relay, Base, Nuts

Kit 283113A02R00 1 1,740.00 Placard Set, Relay, Base, Nuts

TOTAL 3,480.00

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 283113A01R00 1 1,740.00 Placard Set, Relay, Base, Nuts

EFFECTIVITY

**CONF ALL

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

46W AAW ACI AEA AFL AFR AGC ALK ASY AVA AZA BEC BEL

BER BMA BTV CCA CES CHH CRK CRL CSC CSN CYP DAH DAL

DGA EDW EIN ETD EVA FST FWI GFA GIA GRL HAL HFY HVN

IAC ISS IYE JAI JST KAL KFR KKK KLM LLC MAS MAU MEA

MLR MON MSR OMA QAF QFA QTR RJA RSF SAA SWR TAM TAP

TCX THY TSC UAE UAF USA VKG VOZ XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 283113-831-895-001: MODIFICATION

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

**CONF 002

Task 283113-831-895-001: MODIFICATION

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 7.00

APPENDICES

**CONF ALL

None

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 3

7

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@A330

SERVICE BULLETIN

SUMMARY

**CONF 001

FR14

FR15A

751VU

752VU

G_SB_283113_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 4

7

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@A330

SERVICE BULLETIN

SUMMARY

**CONF 002

FR14

FR15A

751VU

G_SB_283113_5_SAAB_01_00

Figure A-FSAAB - Sheet 01

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 5

7

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@A330

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 6

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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: 28

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER TANK FUEL PUMP CONTROL CIRCUIT

MODIFICATION No.: 200242H16135

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

330-202 330-203 330-223 330-243 330-243F

(2) Effectivity by MSN

0181 0195 0205 0211 0222-0223 0226 0229-0230 0232 0238 0240 0247-0251

0253-0255 0258-0259 0261-0262 0265-0266 0269 0271-0272 0275-0276 0281 0283

0285-0288 0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0314

0316-0317 0320 0322 0324 0326 0328 0330 0334 0339-0340 0343 0345 0348 0353

0358 0361-0362 0364-0366 0369 0372 0382 0384 0392 0396-0398 0401 0403-0404

0409 0422 0427 0432 0437 0441 0443-0444 0448 0451-0452 0454-0456 0458

0461-0463 0465-0466 0469 0472-0473 0476-0477 0480-0481 0486-0487 0489 0491

0493-0494 0498 0500-0511 0513 0516 0518-0519 0521-0522 0525-0527 0529-0530

0532 0535-0536 0551 0555 0567 0571 0573 0584 0587 0597 0600 0605 0609-0610

0612 0614 0616 0618 0620-0621 0625 0627 0631-0635 0638 0644 0647 0649-0650

0652-0653 0655-0658 0661 0664-0667 0678 0682-0684 0686 0688 0693 0696-0697

0700 0703-0704 0709 0717-0718 0722 0724 0726 0728-0730 0732-0733 0735

0737-0739 0742-0743 0745-0747 0749-0751 0754-0756 0759-0760 0770 0774 0778

0780 0785 0788 0792 0795-0797 0801-0802 0807 0809-0811 0814-0815 0818-0822

0824-0825 0828 0831-0832 0834 0839-0842 0849 0852-0854 0860 0863 0867-0869

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 1

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@A330

SERVICE BULLETIN

0871 0873-0877 0881-0885 0887-0888 0890-0892 0898-0901 0903-0904 0906 0909

0911 0914 0916 0919 0923 0926-0927 0930-0932 0934 0939-0941 0943-0951

0956-0957 0961-0963 0966-0971 0973 0975-0977 0979-0980 0982 0984 0988

0991-0992 0995-0996 0998-0999 1002 1004 1008-1009 1011 1014 1016 1019-1020

1022 1028 1031-1034 1036 1038-1039 1041-1043 1045-1047 1049 1052-1054 1057

1059 1061 1069-1070 1073 1076 1080 1082 1094-1096 1100 1104 1112 1114 1116

1118 1120 1123 1129 1133 1135 1138 1155 1159 1161 1169 1171 1174 1183-1184

1186 1191 1198 1200 1202-1203 1208 1210 1213-1214 1217-1218 1220-1221

1223-1225 1227

(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

46W 0871

AAW 0999 1043

ACI 0507 0510

AEA 0461 0551 0597 0733 0745 0749 0814 0931 0950

AFL 0963 0973 1014 1045 1047

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

0567 0584 0657

AGC 0324 0364

ALK 0303 0306 0311 0313 0404

ASY 0747 0951 0969 1036 1183

AVA 0948 0967 1009 1016 1073 1208 1224

AZA 0272 0339 1123 1135 1218 1225

BEC 0863

BEL 0229

BER 0288 0322 0403 0432 0444 0454 0469 0476 0493 0739 0828 0911

BMA 0398 0401

BTV 0205 0330

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

0884 0890 0903 0909 0930 0941 0944 0957

CES 0728 0732 0735 0821 0916

CHH 0875 0881 0906 0919 0982 1159

CRK 1031 1034 1039 1042 1054 1059

CRL 0285 0320

CSC 1082 1138

CSN 0649 0652 0656 0664 0818 0840 1096 1116 1129 1202 1220

CYP 0505 0526

DAH 0644 0647 0650 0653 0667

DAL 0609 0614 0618 0620 0621 0631 0633 0718 0722 0778 0796

DGA 0240

EDW 0291

EIN 0269 0397 0841

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 2

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

0854 0868 0975 0991 1032 1070

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

FST 1033 1046

FWI 0253

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

GIA 0988 1020 1028 1052 1184 1214

GRL 0230

HAL 1104 1114 1171 1217

HFY 0211 1008

HVN 0255 0262 0275 0294 0299 0366 0943 0962 1019

IAC 0353 0362

ISS 0665 0802 0822

IYE 0625 0632

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

JST 0506 0508 0513 0522 0842 0853 0940 0945 1198

KAL 0222 0226 0258 1133 1155 1200 1203

KFR 0874 0891 0927 0939 0946

KKK 0343 0358

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 1161

LLC 1053

MAS 0290 0296 0300

MAU 0883 1057

MEA 0926 0984 0995 0998

MLR 0627

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

OMA 1038 1049 1120 1227

QAF 0487 0605

QFA 0887 0892 0898 0976 1061 1094 1169 1174

QTR 0441 0473 0489 0511 0521 0571 0612 0616 0638 0684 0743 0746

0760 0792 0820 0849

RJA 0970 0979 1002

RSF 0980 0996

SAA 1191 1210 1223

SWR 0249

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

0949 0961 0968 0977 1112 1118 1213 1221

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

TCX 0254 0266 0301 0427 0456

THY 0463 0504 0697 0704 0742 0754 0774 1004

TSC 0250 0271 0369 0480 0795 0966 0971

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382

0384 0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509

0518 0525 0536

UAF 1080 1186

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 3

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@A330

SERVICE BULLETIN

OPERATOR MSN

USA 1011 1022 1041 1069 1076 1095 1100

VKG 0309

VOZ 0365 0372

XLF 0501 0635

(4) Configuration by MSN

MSN CONFIGURATION

0181 0195 0223 0248 0251 0283 0293 0295 0305 0308 0312

0314 0316 0317 0326 0328 0345 0348 0365 0372 0382 0384

0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509

0518 0525 0536 0877 0899 0904 0914 0934

001 002

0205 0211 0222 0226 0229 0230 0232 0238 0240 0247 0249

0250 0253 0254 0255 0258 0259 0261 0262 0265 0266 0269

0271 0272 0275 0276 0281 0285 0286 0287 0288 0290 0291

0294 0296 0299 0300 0301 0303 0306 0309 0311 0313 0320

0322 0324 0330 0334 0339 0340 0343 0353 0358 0361 0362

0364 0366 0369 0397 0398 0401 0403 0404 0422 0427 0432

0441 0443 0444 0448 0454 0456 0458 0461 0463 0465 0466

0469 0472 0473 0476 0477 0480 0481 0486 0487 0489 0493

0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0510

0511 0513 0516 0519 0521 0522 0526 0527 0529 0530 0532

0535 0551 0555 0567 0571 0573 0584 0587 0597 0600 0605

0609 0610 0612 0614 0616 0618 0620 0621 0625 0627 0631

0632 0633 0634 0635 0638 0644 0647 0649 0650 0652 0653

0655 0656 0657 0658 0661 0664 0665 0666 0667 0678 0682

0683 0684 0686 0688 0693 0696 0697 0700 0703 0704 0709

0717 0718 0722 0724 0726 0728 0729 0730 0732 0733 0735

0737 0738 0739 0742 0743 0745 0746 0747 0749 0750 0751

0754 0755 0756 0759 0760 0770 0774 0778 0780 0785 0788

0792 0795 0796 0797 0801 0802 0807 0809 0810 0811 0814

0815 0818 0819 0820 0821 0822 0824 0825 0828 0831 0832

0834 0839 0840 0841 0842 0849 0852 0853 0854 0860 0863

0867 0868 0869 0871 0873 0874 0875 0876 0881 0882 0883

0884 0885 0887 0888 0890 0891 0892 0898 0900 0901 0903

0906 0909 0911 0916 0919 0923 0926 0927 0930 0931 0932

0939 0940 0941 0943 0944 0945 0946 0947 0948 0949 0950

0951 0956 0957 0961 0962 0963 0966 0967 0968 0969 0970

0971 0973 0975 0976 0977 0979 0980 0982 0984 0988 0991

0992 0995 0996 0998 0999 1002 1004 1008 1009 1011 1014

1016 1019 1020 1022 1028 1031 1032 1033 1034 1036 1038

1039 1041 1042 1043 1045 1046 1047 1049 1052 1053 1054

1057 1059 1061 1069 1070 1073 1076 1080 1082 1094 1095

1096 1100 1104 1112 1114 1116 1118 1120 1123 1129 1133

1135 1138 1155 1159 1161 1169 1171 1174 1183 1184 1186

1191 1198 1200 1202 1203 1208 1210 1213 1214 1217 1218

1220 1221 1223 1224 1225 1227

001

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 4

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Evaluation Service Bulletin No. A330-28-3903 is

not accomplished or for aircraft on which the restoration of Evaluation Service Bulletin

No. A330-28-3903 is accomplished.

**CONF 002

Config. 002 is valid for aircraft on which Evaluation Service Bulletin No. A330-28-3903 is

accomplished and the restoration is not accomplished (during the evaluation period).

These aircraft will not have to do the restoration of Evaluation Service Bulletin No.

A330-28-3903.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 283113A01R00 1

Kit 283113A02R00 1

Consumable CMLA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 283113A01R00 1

Consumable CMLA01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The European Aviation Safety Agency (EASA) has requested that Ground Fault

Interrupters (GFI) are installed into the electrical supply circuits of fuel pumps where the

inlets become uncovered during normal operation. This is in response to SFAR88 - Fuel

Tank Safety.

The Evaluation Service Bulletin A330-28-3903 (Mod. No. 200241H16397) was issued for

operators TAP and UAE. The Service Bulletin A330-28-3903 introduced a GFI and

related base into the electrical supply circuit of the A330-200 aircraft right center tank

transfer pump.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 5

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(2) Objective/Action

This Service Bulletin introduces GFI, and related bases, into the electrical supply circuits

of the A330-200 aircraft left and right center tank transfer pumps. These GFIs have the

same ’footprint’ as the existing relay/micro-contactors and physically replace them on the

electrical panel. The new GFI sockets are fool-proofed to prevent incorrectly installing

normal relay/micro-contactors.

(3) Advantages

These GFIs will replace the existing 3-phase relay/micro-contactors. The function of the

GFI is to electrically isolate the pump if a ground fault condition occurs downstream of

the GFI. The GFI gives additional earth leakage protection to the downstream circuit.

Accomplishment of this Service Bulletin will not change the characteristics of the aircraft.

(4) Operational/Maintenance Consequences

The embodiment of this SB affects the ALS part 5, section 5-4. This limitation is

applicable to all aircraft operated under FAA registration.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 283113-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

(2) Modify the Equipment and the Wiring in the RH Relay Box 752VU

**CONF 002

Task 283113-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

The accomplishment timescale for this Service Bulletin will be 4 years.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

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SERVICE BULLETIN

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the (thresholds

and/or intervals and/or date) given above but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

F. APPROVAL

The technical content of this document is approved under the authority of 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.

**CONF 001

Task 283113-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

3.00

Modify the Equipment and the Wiring in the RH Relay

Box 752VU

3.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

**CONF 002

Task 283113-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

3.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 7.00

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**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight +0.122 KG (+0.2689 LB)

Effect on Balance +1.170 KGM (+8.462 LB.FT )

**CONF 002

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight +0.061 KG (+0.1344 LB)

Effect on Balance +0.585 KGM (+4.231 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-21-13 12-34-24 20-21-15

20-28-00 28-25-00 52-30-00

52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-52-21 20-55-00

Service Bulletin (SB) A330-28-3903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-21-13 12-34-24 20-21-15

20-28-00 28-25-00 52-30-00

52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-52-21 20-55-00

Service Bulletin (SB) A330-28-3903

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

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Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Airworthiness Limitation Section (ALS)

Aircraft Schematic Manual (ASM) 28-20-01 28-26-02 28-26-03

Aircraft Wiring List (AWL)

Aircraft Wiring Manual (AWM) 28-26-21 28-26-22

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

**CONF 002

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

**CONF ALL

M. SPARES

None

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This Page Intentionally Left Blank

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SERVICE BULLETIN

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 283113A01R00

Kit 283113A02R00

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 by Email: airbus.kit@airbus.com

(2) Price and Availability

Kit 283113A01R00

Cost 1,740.00 USD

Availability 60 calendar days from receipt of order

Kit 283113A02R00

Cost 1,740.00 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.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will provide a 15% reduction to the commercial rate applicable to sales prices given

in the paragraph ’Price and Availability’ for orders placed before 31 December 2017.

C. LIST OF COMPONENTS

Kit 283113A01R00

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

NOTES

1 ABS1629-28A0 1 GFI (1) E0667A28A0

2 E0673C0S 1 Base (2) E0673A0S

3 MS21042-04 3 Nut

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

NOTES

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214395 1 Set

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.

Kit 283113A02R00

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

NOTES

1 ABS1629-28A0 1 GFI (1) E0667A28A0

2 E0673C0S 1 Base (2) E0673A0S

3 MS21042-04 3 Nut

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214495 1 Set

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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent (varsol/white

Spirit)

11-002 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 283113-831-895-001 - MODIFICATION

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

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

**CONF 001

Zone

121 122 191 192 211 212

Modified FIN

5QL1 5QL1A 5QL2 5QL2A 97QL1 97QL1A 97QL2 97QL2A

Access

Door 132AZ 821

Electrical panel 751VU 752VU

Manpower

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

**CONF 002

Zone

121 191 192 211 212

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SERVICE BULLETIN

Modified FIN

5QL1 5QL1A 97QL1 97QL1A

Access

Door 132AZ 821

Electrical panel 751VU

Manpower

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 7.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 283113-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802).

(b) For the specification of the material numbers (Mat. No.) that you must use in this

Service Bulletin (Refer to the Consumable Material List (CML)).

(c) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(d) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-30-00).

(f) For the installation of the relays (Refer to ESPM 20-46-50).

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

(2) Subtask 283113-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 283113-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802).

(b) For the specification of the material numbers (Mat. No.) that you must use in this

Service Bulletin (Refer to the Consumable Material List (CML)).

(c) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(d) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-30-00).

(f) For the installation of the relays (Refer to ESPM 20-46-50).

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

(2) Subtask 283113-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

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SERVICE BULLETIN

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 283113-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

(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.

(2) Subtask 283113-010-001-001 - Remove/Open for Access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

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

52-30-00-010-804).

(b) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(3) Subtask 283113-865-002-001 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

(a) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

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PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

722VU FUEL XFR R PUMP 1QL2 48 G

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF 002

(1) Subtask 283113-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

(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.

(2) Subtask 283113-010-001-001 - Remove/Open for Access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

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

52-30-00-010-804).

(b) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(3) Subtask 283113-865-002-002 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

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(a) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 283113-831-001-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 283113A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673C0S 1 Base

3 MS21042-04 3 Nut

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214395 1 Set

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002

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References

Fig. A-FCAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBBAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove (Refer to Fig. A-FBBAA Sheet 01).

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

(c) Modify the wiring in the LH Relay Box 751VU:

1 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 01 and Fig. A-FCAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FCAAA Sheet 03).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

2 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBBAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 2

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

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FIN 97QL1

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the screws to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

b Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

c Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBBAA Sheet 02, supplied in:

1 Placard Set F9100095214395

(d) Close the LH Relay Box 751VU.

(2) Subtask 283113-831-002-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Electrical panel 752VU

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 283113A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673C0S 1 Base

3 MS21042-04 3 Nut

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214495 1 Set

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Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002

References

Fig. A-FCBAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBCAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

(b) Remove (Refer to Fig. A-FBCAA Sheet 01).

FIN 5QL2

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL2A

1 Base E0673A0S Item (2) Discard

FIN 5QL2

1 Placard Discard

(c) Modify the wiring in the RH Relay Box 752VU:

1 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCBAA Sheet 01 and Fig. A-FCBAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FCBAA Sheet 03).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

2 Install the relay GFI 97QL2.

a Install (Refer to Fig. A-FBCAA Sheet 02):

FIN 97QL2A

1 Base E0673C0S Item 2

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attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL2

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the screws to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

b Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

c Near the relay, bond the placard identified 97QL2 as shown in Fig. AFBCAA Sheet 02, supplied in:

1 Placard Set F9100095214495

(d) Close the RH Relay Box 752VU.

**CONF 002

(1) Subtask 283113-831-001-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 283113A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673C0S 1 Base

3 MS21042-04 3 Nut

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 22

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214395 1 Set

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002

References

Fig. A-FCAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBBAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove (Refer to Fig. A-FBBAA Sheet 01).

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

(c) Modify the wiring in the LH Relay Box 751VU:

1 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 01 and Fig. A-FCAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FCAAA Sheet 03).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 23

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SERVICE BULLETIN

2 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBBAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 2

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL1

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the screws to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

b Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

c Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBBAA Sheet 02, supplied in:

1 Placard Set F9100095214395

(d) Close the LH Relay Box 751VU.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 283113-865-001-001 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

(a) Remove the safety clips and/or tags and close/unlock these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 24

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SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FUEL XFR R PUMP 1QL2 48 G (1)

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 283113-800-401-001 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAA

Test of the Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the RESET (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 97QL2

1 On the panel 752VU, make sure that the GFI is in the RESET (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 25

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@A330

SERVICE BULLETIN

(3) Subtask 283113-710-401-001 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of the Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE CENTER TANK HAS SUFFICIENT FUEL TO MAKE SURE

THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN THE DRY

CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL (CTR TK

TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 26

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SERVICE BULLETIN

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

(4) Subtask 283113-710-403-001 - Test of Ground Fault Interrupter - 97QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAA

Test of the Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE CENTER TANK HAS SUFFICIENT FUEL TO MAKE SURE

THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN THE DRY

CONDITION.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 27

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SERVICE BULLETIN

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 245VU, set the Push-Button (P/BSW) FIN 15QL (CTR TK TO

INR XFR) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2:

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

3 Operate the transfer fuel pump FIN 600QL2 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL2, on the panel 752VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 97QL2 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL2 (CTR TK R).

4 Push the P/BSW FIN 3QL2 (CTR TK R) to set the transfer fuel pump FIN

600QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 97QL2

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2:

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 28

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SERVICE BULLETIN

**CONF 002

(1) Subtask 283113-865-001-002 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

(a) Remove the safety clips and/or tags and close/unlock these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 283113-800-402-001 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAB

Test of the Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the RESET (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAB Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 29

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@A330

SERVICE BULLETIN

(3) Subtask 283113-710-401-002 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAB

Test of the Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE CENTER TANK HAS SUFFICIENT FUEL TO MAKE SURE

THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN THE DRY

CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL (CTR TK

TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAB Sheet 02).

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAB Sheet 01).

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 30

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SERVICE BULLETIN

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAB Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAB Sheet 02).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 283113-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

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

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 31

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SERVICE BULLETIN

(d) Remove the access platform(s).

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

(2) Subtask 283113-942-401-002 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-21-13-860-051

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

equipment (Refer to AMM Task 12-21-13-860-051).

(b) Remove the access platform(s).

(c) Restore the system and the aircraft to the normal operating condition.

**CONF 002

(1) Subtask 283113-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

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

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

(d) Remove the access platform(s).

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

(2) Subtask 283113-942-401-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 32

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-21-13-860-051

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

equipment (Refer to AMM Task 12-21-13-860-051).

(b) Remove the access platform(s).

(c) Restore the system and the aircraft to the normal operating condition.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 33

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@A330

SERVICE BULLETIN

**CONF ALL

BEFORE

B D

H

A

B

C

C

FR20

FR15A

FR14

FR1

(3 POS) (3)

(2)

(1)

751VU

A

5QL1

G_SB_283113_5_BBAA_01_03

66

5QL1

Figure A-FBBAA - Sheet 01

Modification of the Equipment in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 34

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@A330

SERVICE BULLETIN

**CONF ALL

AFTER

H

(3 POS)

D

E

E

3

2

1

97QL1 ELECTRICAL BONDING

G_SB_283113_5_BBAA_02_04

66

97QL1

Figure A-FBBAA - Sheet 02

Modification of the Equipment in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 35

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@A330

SERVICE BULLETIN

**CONF 001

BEFORE

A

H

A

B

5QL2

C

FR20

FR15A

FR14

FR1

(3 POS) (3)

(2)

(1)

752VU

G_SB_283113_5_BCAA_01_02

5QL2

B

D

3

C

Figure A-FBCAA - Sheet 01

Modification of the Equipment in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 36

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@A330

SERVICE BULLETIN

**CONF 001

AFTER

(3 POS)

D

E

97QL2

3

2

1

ELECTRICAL BONDING

E

97QL2

B

87

G_SB_283113_5_BCAA_02_04

Figure A-FBCAA - Sheet 02

Modification of the Equipment in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 37

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@A330

SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 01

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 38

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@A330

SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 02

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 39

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@A330

SERVICE BULLETIN

**CONF ALL

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 751VU 5QL1−A C2 2826−0537 B 1M QG16 751VU 1521VC 45 M1O

 2 751VU 97QL1−A C1 EN3155−017F1216 2826−0537 B 1M QG16 751VU 1521VC 45 M1N

 3 751VU 5QL1−A A2 2826−0537 R 1M QG16 751VU 1521VC 43 M1O

 4 751VU 97QL1−A A1 EN3155−017F1216 2826−0537 R 1M QG16 751VU 1521VC 43 M1N

 5 751VU 5QL1−A B2 2826−0537 Y 1M QG16 751VU 1521VC 44 M1O

 6 751VU 97QL1−A B1 EN3155−017F1216 2826−0537 Y 1M QG16 751VU 1521VC 44 M1N

 7 751VU 5QL1−A C1 2826−0538 B 1M QG16 751VU 1523VC 49 M1O

 8 751VU 97QL1−A C2 EN3155−017F1216 2826−0538 B 1M QG16 751VU 1523VC 49 M1N

 9 751VU 5QL1−A A1 2826−0538 R 1M QG16 751VU 1523VC 42 M1O

10 751VU 97QL1−A A2 EN3155−017F1216 2826−0538 R 1M QG16 751VU 1523VC 42 M1N

11 751VU 5QL1−A B1 2826−0538 Y 1M QG16 751VU 1523VC 43 M1O

12 751VU 97QL1−A B2 EN3155−017F1216 2826−0538 Y 1M QG16 751VU 1523VC 43 M1N

13 751VU 5QL1−A 13 2826−0574 1M DK24 751VU 1521VC 35 M1O

14 751VU 97QL1−A 12 EN3155−017F1620 2826−0574 1M DK24 751VU 1521VC 35 M1N

15 751VU 5QL1−A 12 2826−0575 1M DK24 751VU 1407VG GND M1O

16 751VU 97QL1−A 13 EN3155−017F1620 2826−0575 1M DK24 751VU 1407VG GND M1N

17 751VU 5QL1−A X2 2826−0576 1M DK24 751VU 1407VG GND M1O

18 751VU 97QL1−A X2 EN3155−017F1620 2826−0576 1M DK24 751VU 1407VG GND M1N

19 751VU 5QL1−A X1 2826−0579 1M DK24 751VU 4QL1−A 1 M1O

20 751VU 97QL1−A X1 EN3155−017F1620 2826−0579 1M DK24 751VU 4QL1−A 1 M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

 GND = GROUND

Figure A-FCAAA - Sheet 03

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 40

7

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@A330

SERVICE BULLETIN

**CONF 001

Figure A-FCBAA - Sheet 01

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 41

7

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@A330

SERVICE BULLETIN

**CONF 001

Figure A-FCBAA - Sheet 02

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 42

7

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@A330

SERVICE BULLETIN

**CONF 001

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 752VU 5QL2−A C2 2826−0592 B 2M QG16 752VU 1536VC 45 M1O

 2 752VU 97QL2−A C1 EN3155−017F1216 2826−0592 B 2M QG16 752VU 1536VC 45 M1N

 3 752VU 5QL2−A A2 2826−0592 R 2M QG16 752VU 1536VC 43 M1O

 4 752VU 97QL2−A A1 EN3155−017F1216 2826−0592 R 2M QG16 752VU 1536VC 43 M1N

 5 752VU 5QL2−A B2 2826−0592 Y 2M QG16 752VU 1536VC 44 M1O

 6 752VU 97QL2−A B1 EN3155−017F1216 2826−0592 Y 2M QG16 752VU 1536VC 44 M1N

 7 752VU 5QL2−A C1 2826−0593 B 2M QG16 752VU 1536VC 42 M1O

 8 752VU 97QL2−A C2 EN3155−017F1216 2826−0593 B 2M QG16 752VU 1536VC 42 M1N

 9 752VU 5QL2−A A1 2826−0593 R 2M QG16 752VU 1536VC 40 M1O

10 752VU 97QL2−A A2 EN3155−017F1216 2826−0593 R 2M QG16 752VU 1536VC 40 M1N

11 752VU 5QL2−A B1 2826−0593 Y 2M QG16 752VU 1536VC 41 M1O

12 752VU 97QL2−A B2 EN3155−017F1216 2826−0593 Y 2M QG16 752VU 1536VC 41 M1N

13 752VU 5QL2−A 13 2826−0623 2M DK24 752VU 1536VC 5 M1O

14 752VU 97QL2−A 12 EN3155−017F1620 2826−0623 2M DK24 752VU 1536VC 5 M1N

15 752VU 5QL2−A 12 2826−0625 2M DK24 752VU 1402VG GND M1O

16 752VU 97QL2−A 13 EN3155−017F1620 2826−0625 2M DK24 752VU 1402VG GND M1N

17 752VU 5QL2−A X2 2826−0626 2M DK24 752VU 1402VG GND M1O

18 752VU 97QL2−A X2 EN3155−017F1620 2826−0626 2M DK24 752VU 1402VG GND M1N

19 752VU 5QL2−A X1 2826−0627 2M DK24 752VU 4QL2−A 1 M1O

20 752VU 97QL2−A X1 EN3155−017F1620 2826−0627 2M DK24 752VU 4QL2−A 1 M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

 GND = GROUND

Figure A-FCBAA - Sheet 03

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 43

7

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@A330

SERVICE BULLETIN

**CONF 001

FR20

FR15A

FR14

FR1

RH RELAY BOX

LH RELAY BOX

C

B

751VU

752VU

A

A

C

B

GFI AUTO−TEST

BUTTON

GFI METAL SHAFT IN

CLOSED POSITION

GFI METAL SHAFT IN

OPEN POSITION

C

/

TRIP/RESET BUTTON

97QL1 97QL2

D

G_SB_283113_7_BAAA_01_01

(NOT TRIPPED) (TRIPPED)

Figure A-UBAAA - Sheet 01

Test of the Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 44

7

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@A330

SERVICE BULLETIN

**CONF 001

245VU

E

D

E

OFF

FAULT

OFF OFF

FWD OFF

OFF MAN OFF

ON

FAULT

OFF OFF

LSTBY MODE RSTBY

L1 L2 R 2 R 1

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

FEED

T TANK

L XFR R CTR TANK

ON

OPEN

XFR

OUTR TK

ENG 1 ENG 2

WING X FEED

F

U

E

L

F

U

E

L

FAULT FAULT

FAULT FAULT FAULT

FAULT

FAULT FAULT

FAULT

G_SB_283113_7_BAAA_02_00

3QL1 15QL 3QL2

Figure A-UBAAA - Sheet 02

Test of the Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 45

7

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@A330

SERVICE BULLETIN

**CONF 002

FR20

FR15A

FR14

FR1

GFI AUTO−TEST

BUTTON

GFI METAL SHAFT IN

CLOSED POSITION

GFI METAL SHAFT IN

OPEN POSITION

LH RELAY BOX

751VU

A

A

TRIP/RESET BUTTON

97QL1

B

C

B

G_SB_283113_7_BAAB_01_01

(NOT TRIPPED) (TRIPPED)

Figure A-UBAAB - Sheet 01

Test of the Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 46

7

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@A330

SERVICE BULLETIN

**CONF 002

245VU

OFF

FAULT

OFF OFF

FWD OFF

OFF MAN OFF

ON

FAULT

OFF OFF

LSTBY MODE RSTBY

L1 L2 R 2 R 1

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

FEED

T TANK

L XFR R CTR TANK

ON

OPEN

XFR

OUTR TK

ENG 1 ENG 2

WING X FEED

F

U

E

L

F

U

E

L

FAULT FAULT

FAULT FAULT FAULT

FAULT

FAULT FAULT

FAULT

3QL1 15QL

D

C

D

G_SB_283113_7_BAAB_02_01

Figure A-UBAAB - Sheet 02

Test of the Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 47

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER TANK FUEL PUMP CONTROL CIRCUIT

MODIFICATION No.: 200242H16135

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: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 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 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- 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: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113

REVISION No.: 01 - Mar 27/12 Page: 1

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