# @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



# MANDATORYMANDATORYMANDATORY
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

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# @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 7

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# @A330 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

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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. 

# MANDATORYMANDATORYMANDATORY
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 7

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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 7

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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

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DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 6 7

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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



# MANDATORYMANDATORYMANDATORY
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 7

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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 7

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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 7

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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

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# @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

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# @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 REVISION No.: 01 - Mar 27/12 Page: 6 7

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# @A330 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
DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 7 7

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# @A330 SERVICE BULLETIN
**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 REVISION No.: 01 - Mar 27/12 Page: 8 7

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# @A330 SERVICE BULLETIN 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

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 9 7

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# @A330 SERVICE BULLETIN

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DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 10 7

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# @A330 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 DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 11 7

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# @A330 SERVICE BULLETIN

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 REVISION No.: 01 - Mar 27/12 Page: 12 7

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# @A330 SERVICE BULLETIN
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
DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 13 7

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# @A330 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 toAMM 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 DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 14 7

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# @A330 SERVICE BULLETIN (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 toAMM 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.

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 15 7

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# @A330 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) DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 16 7

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# @A330 SERVICE BULLETIN

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

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 17 7

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# @A330 SERVICE BULLETIN (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
DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 18 7

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# @A330 SERVICE BULLETIN

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).
DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 19 7

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# @A330 SERVICE BULLETIN
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

DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 20 7

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# @A330 SERVICE BULLETIN

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
DATE: Jul 19/11 SERVICE BULLETIN No.: A330-28-3113 REVISION No.: 01 - Mar 27/12 Page: 21 7

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# @A330 SERVICE BULLETIN
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 7

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# @A330 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 7

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# @A330 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 7

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# @A330 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 7

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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 7

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# @A330 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 7

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# @A330 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 7

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# @A330 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 7

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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 7

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# @A330 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 7

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# @A330 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 7

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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 7

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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_0366 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 7

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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_0466 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 7

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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 7

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# @A330 SERVICE BULLETIN

**CONF 001 

## AFTER

(3 POS) 

## D

**E** 97QL2 3 2

1

ELECTRICAL BONDING 

### E 97QL2

B87

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 7

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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 7

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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 7

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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 R 1 R 2 L2 L1

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 R 1 R 2 L2 L1

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 7

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# @A330 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 7

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

# @A330 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 7

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