# Airbus Service Bulletin A330-57-3132 Copy: No revision named ("A330-57-3132 R01"), 185 pages: PDF https://openairdocs.org/files/sha256/32/84/3284a7de2ae61ffd2dff92157a306f08dfaf0b586acd2a75bf69d565cb63974f; text https://openairdocs.org/service-documents/airbus/a330-57-3132/file/3284a7de2ae6.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0113, the docket of AD 2019-16-07. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md) - Type: Service bulletin (Service Bulletin) - Number: A330-57-3132 - Page: https://openairdocs.org/service-documents/airbus/a330-57-3132 Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-57-3132/proposed.md). ## Text (185 pages) Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0113, the docket of AD 2019-16-07. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 ATA SYSTEM: 57 TITLE: FUSELAGE - CENTER FUSELAGE - MODIFICATION OF FASTENER HOLES NO 25,38,39 and 43 AT FRAME 40 VERTICAL WEB BELOW CENTER WING BOX LOWER PANEL MODIFICATION No.: 206048S33788 This page transmits Revision No.01 of Service Bulletin No.A330-57-3132 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 extend the effectivity to include A330-200F aircraft model. CHANGES The main changes of this revision are: - Effectivity updated - Work locations updated to add zone 141 and zone 142 - Procedure modified for hole H39: Item (10) replaced by Item (14) - Minor changes applied. Some revision bars are produced due to a text amendment to change ’(Refer to...)’ into ’in accordance with’. FRONT MATTER FUSELAGE - CENTER FUSELAGE - MODIFICATION OF FASTENER HOLES NO 25,38,39 and 43 AT FRAME 40 VERTICAL WEB BELOW CENTER WING BOX LOWER PANEL CONFIGURATION UPDATED R SUMMARY REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES REASON UPDATED R DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 2 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE UPDATED R MATERIAL PRICE INFORMATION TABLE UPDATED R MATERIAL PRICE INFORMATION TABLE UPDATED R MATERIAL PRICE INFORMATION TABLE UPDATED R MATERIAL PRICE INFORMATION TABLE UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONF 001 CONFIGURATION DEFINITION UPDATED R CONF 002 CONFIGURATION DEFINITION UPDATED R CONF 003 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R CONF 004 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R CONF 005 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R REASON Objective/Action OBJECTIVE/ACTION UPDATED R Operational/Maintenance Consequences OPERATIONAL/MAINTENANCE CONSEQUENCES UPDATED R MANPOWER MANPOWER UPDATED R MANPOWER UPDATED R MANPOWER UPDATED R MANPOWER UPDATED CONFIGURATION UPDATED R MANPOWER UPDATED CONFIGURATION UPDATED R PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED R Price and Availability PRICE AND AVAILABILITY UPDATED MATERIAL PRICE UPDATED R INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R TOOLING Tooling - Price and Availability Procurement Addresses PROCUREMENT ADDRESSES UPDATED R Price and Availability PRICE AND AVAILABILITY UPDATED R Tools Standard tool TOOLA01 TOOL MATERIAL SET UPDATED R DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 3 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Standard tool TOOLA02 TOOL MATERIAL SET UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 573132- 831-801-001-Modification TASK SOLUTION UPDATED NOTE UPDATED R Task associated data - 001 ZONE UPDATED R Task associated data - 002 ZONE UPDATED R Task associated data - 003 ZONE UPDATED R Task associated data - 004 ZONE UPDATED R Task associated data - 005 ZONE UPDATED R Subtask 573132-910-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-910-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-910-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-910-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-910-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-941-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED NOTE UPDATED R Subtask 573132-010-005-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-003-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED PANEL UPDATED CAUTION UPDATED R Subtask 573132-941-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED NOTE UPDATED R Subtask 573132-010-005-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-003-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED PANEL UPDATED CAUTION UPDATED R DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 4 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 573132-941-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED NOTE UPDATED R Subtask 573132-010-005-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-003-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED PANEL UPDATED CAUTION UPDATED R Subtask 573132-941-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED NOTE UPDATED R Subtask 573132-010-005-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-003-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED PANEL UPDATED CAUTION UPDATED R Subtask 573132-941-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED NOTE UPDATED R Subtask 573132-010-005-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-003-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-010-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED PANEL UPDATED CAUTION UPDATED R Subtask 573132-000-001-002 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-831-001-002 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-001-002 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 5 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 573132-000-002-004 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-831-002-004 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-002-002 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-000-001-001 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-250-001-003 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 573132-831-001-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-001-001 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-000-002-003 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-250-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 573132-831-002-003 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-002-001 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-000-001-002 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-831-001-002 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 6 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 573132-400-001-002 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-000-002-004 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-831-002-004 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-002-002 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-000-001-002 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-831-001-002 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-001-002 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-000-002-004 SUBTASK SOLUTION UPDATED ZONE UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED LOCATION UPDATED R Subtask 573132-831-002-004 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-002-002 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-000-001-003 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-250-001-004 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 573132-831-001-003 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-001-003 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 7 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 573132-000-002-005 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-250-002-003 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 573132-831-002-001 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED MATERIAL LIST UPDATED R Subtask 573132-400-002-003 SUBTASK SOLUTION UPDATED ZONE UPDATED LOCATION UPDATED R Subtask 573132-410-002-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-410-004-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-942-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-410-002-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-410-004-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-942-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-410-002-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-410-004-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-942-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-410-002-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-410-004-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-942-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Subtask 573132-410-002-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-410-004-001 SUBTASK SOLUTION UPDATED FIN UPDATED R Subtask 573132-942-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 8 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-FBFAA FIGURE SOLUTION UPDATED R Appendix 01 - Manpower Gantt Chart APPENDIX CONTENT APPENDIX CONTENT ADDED N Appendix 02 - Configuration Definition table APPENDIX CONTENT APPENDIX CONTENT UPDATED R FILING 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: Nov 23/16 REVISION No. : 01 - Feb 05/18 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 9 @A330 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 This summary is for information only and is not approved for modification of the aircraft. ATA SYSTEM: 57 TITLE: FUSELAGE - CENTER FUSELAGE - MODIFICATION OF FASTENER HOLES NO 25,38,39 and 43 AT FRAME 40 VERTICAL WEB BELOW CENTER WING BOX LOWER PANEL **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 206048S33788 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 area at Frame (FR) 40 is subjected to a specific maintenance program. A new campaign of modifications has been launched to improve the maintenance program, decrease the number of maintenance actions and to improve the structural potential of the aircraft to meet the future Extended Service Goal (ESG) / Design Service Goal (DSG). This Service Bulletin recommends the application of Cold Working on holes 25, 38, 39 and 43 at FR40 to improve the fatigue behaviour. Depending on the configuration, this reinforcement consists in doing a first or second cold expansion of fastener holes 25, 38, 39 and 43 and installing oversized fastener with high interference. The procedure as described in this Service Bulletin is to be performed if no AIRBUS repair and/or repair improvement has been previously performed in the same area. In case of repairs performed previously, please contact AIRBUS Repair Support department for further instructions. Accomplishment of this Service Bulletin will contribute to prevent cracks and will increase the fatigue life in the area of FR40. Depending on configuration, accomplishment of this Service Bulletin cancels the requirements of Inspection Service Bulletin No. A330-57-3116 for holes 25, 38, 39 and 43, if accomplished after the lower bound described in Inspection Service Bulletin No. A330-57-3116. For hole 25, for Aircraft in Config. 002, this modification Service Bulletin is not terminative and must be monitored by Inspection Service Bulletin No. A330-57-3116. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 10 @A330 SERVICE BULLETIN SUMMARY GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO POTENTIAL AD NO 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 recommended to be accomplished to prevent significant operational disruptions. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 573132A01R01 1 170.00 Bolts, Nuts Kit 573132A02R00 1 51.00 Bolts, Nuts TOTAL 221.00 Standard tool TOOLA01 1 See SB Durable Tool Kit Standard tool TOOLA02 1 See SB Expendable Tool Kit **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 573132A01R01 1 170.00 Bolts, Nuts Standard tool TOOLA01 1 See SB Durable Tool Kit Standard tool TOOLA02 1 See SB Expendable Tool Kit **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 573132A01R01 1 170.00 Bolts, Nuts Kit 573132A02R00 1 51.00 Bolts, Nuts TOTAL 221.00 Standard tool TOOLA01 1 See SB Durable Tool Kit Standard tool TOOLA02 1 See SB Expendable Tool Kit DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 11 @A330 SERVICE BULLETIN SUMMARY **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 573132A01R01 1 170.00 Bolts, Nuts Kit 573132A02R00 1 51.00 Bolts, Nuts TOTAL 221.00 Standard tool TOOLA01 1 See SB Durable Tool Kit Standard tool TOOLA02 1 See SB Expendable Tool Kit **CONF 005 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 573132A02R00 1 51.00 Bolts, Nuts Standard tool TOOLA01 1 See SB Durable Tool Kit Standard tool TOOLA02 1 See SB Expendable Tool Kit EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) : 01Q 12P 18P 36V 38W 39V 41N 43P 44W 56O 64N AAL AAR AAW ACA ACI AEA AFL AFR AIB ALD ALK ARG ASL ASY AVA AZA AZU BEC BEL BER CAL CBJ CCA CEB CES CHH CPA CRK CRL CSA CSC CSN CSZ D2F DAH DAL DGA DLH EDW EIN ETD EVA EVE F2I FBU FIN FJI FWI GCR GFA GIA GRL HAL HDA HFY HKC HVN I2L IAW IBE IRA JAI JAV KAC KAL KLM LAA LKE LNI MAS MAU MEA MLM MNB MOV MSR NMB NWS OBS OHY OMA ONE P2C PAL PLM QAF QFA QTR RNA RSF RSY RWD RZO SAA SAF SAI SAS SEY SIA SVA SWR SXD TAE TAM TAP TAR TBA TCX THA THY TLM TNA TOW TPA TPU TSC U6A UAE UAF VIR VKG VOZ WOW WRC XAX XLF CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU 57.11.00.007 OEB None AOT None SIL None ISI None LINE MAINTENANCE AFFECTED No DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 12 @A330 SERVICE BULLETIN SUMMARY LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 573132-831-801-001: Modification TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 **CONF 002 Task 573132-831-801-001: Modification TOTAL MANHOURS 26.50 ELAPSED TIME (HOURS) 13.50 **CONF 003 Task 573132-831-801-001: Modification TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 **CONF 004 Task 573132-831-801-001: Modification TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 **CONF 005 Task 573132-831-801-001: Modification TOTAL MANHOURS 24.00 ELAPSED TIME (HOURS) 12.25 APPENDICES **CONF ALL Appendix 01 - Manpower Gantt Chart Appendix 02 - Configuration Definition table DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 13 @A330 SERVICE BULLETIN SUMMARY **CONF 001, 003 thru 004 A A Z140 VIEW LOOKING AFT RH SHOWN LH SYMMETRICAL BU P INBD CENTER WING BOX LOWER PANEL REFERENCE COLD WORKING OF 4 FASTENER HOLES FR40 STGR39RH STGR38RH H25 H38 H39 H43 FR47 FR40 B G_SB_573132_5_SAAA_01_03 Figure A-FSAAA - Sheet 01 Cold Working of the Fasteners Holes 25, 38, 39 and 43 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 14 @A330 SERVICE BULLETIN SUMMARY **CONF 002 A Z140 VIEW LOOKING AFT RH SHOWN LH SYMMETRICAL BU P INBD CENTER WING BOX LOWER PANEL REFERENCE COLD WORKING OF 3 FASTENER HOLES FR40 STGR39RH STGR38RH H38 H39 H43 A FR47 FR40 B G_SB_573132_5_SAAB_01_04 Figure A-FSAAB - Sheet 01 Cold Working of the Fasteners Holes 38, 39 and 43 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 15 @A330 SERVICE BULLETIN SUMMARY **CONF 005 A Z140 VIEW LOOKING AFT RH SHOWN LH SYMMETRICAL BU P INBD CENTER WING BOX LOWER PANEL REFERENCE COLD WORKING OF THE FASTENER HOLE FR40 STGR39RH STGR38RH H25 A FR47 FR40 B G_SB_573132_5_SAAC_01_03 Figure A-FSAAC - Sheet 01 Cold Working of the Fastener Hole 25 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 16 @A330 SERVICE BULLETIN SUMMARY This Page Intentionally Left Blank DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 17 @A330 SERVICE BULLETIN AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 ATA SYSTEM: 57 TITLE: FUSELAGE - CENTER FUSELAGE - MODIFICATION OF FASTENER HOLES NO 25,38,39 and 43 AT FRAME 40 VERTICAL WEB BELOW CENTER WING BOX LOWER PANEL MODIFICATION No.: 206048S33788 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE : This modification is applicable by Service Bulletin only. NOTE : This Service Bulletin is only applicable to aircraft on which MOD No. 44360S13013 or MOD No. 44360S13482 is embodied. (1) Models 330-202 330-203 330-223 330-223F 330-243 330-243F 330-301 330-302 330-303 330-322 330-323 330-342 330-343 (2) Effectivity by MSN 0177 0181 0195 0200 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293 0295-0296 0300-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 18 @A330 SERVICE BULLETIN 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782 0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863 0865-0869 0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922-0923 0925-0928 0930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-0998 1000-1004 1006-1016 1018-1023 1025-1026 1028-1029 1031-1039 1041-1049 1051-1055 1057-1063 1065-1067 1069-1078 1080-1082 1084-1090 1092-1101 1103-1108 1110 1112 1114-1116 1118 1120 1123-1124 1126-1127 1129-1133 1135-1138 1141 1143 1145-1151 1153 1155-1157 1159-1161 1163-1165 1167-1175 1177-1178 1180-1181 1183-1184 1186-1193 1195-1196 1198-1206 1208-1241 1243-1252 1254-1256 1258-1272 1274-1423 1425-1521 1523-1651 1653-1660 1662-1681 1684-1701 1703-1704 1706 1708-1716 1718-1794 1796-1812 1814-1818 1820-1823 1825-1835 1837-1843 1845-1849 1851-1852 1854-1860 1862-1869 1871-1875 1877-1883 1885-1886 (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 01Q 1830 12P 1787 1848 1883 18P 1321 36V 1164 38W 0401 39V 0255 41N 1676 43P 1053 44W 0979 1002 56O 0231 64N 1751 AAL 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041 1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526 AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340 1435 1464 1518 AAW 1043 1472 1535 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0461 0505 0526 0733 0745 0749 0814 0931 0950 0992 1097 1574 AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247 1264 1270 1284 1299 1301 1323 1328 1345 1356 1371 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 19 @A330 SERVICE BULLETIN OPERATOR MSN AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 AIB 0871 ALD 0326 0328 0392 ALK 0303 0306 0311 0313 0456 0627 1564 1583 1604 1650 1669 1687 1689 ARG 0290 0300 0358 0364 0587 0634 1605 1623 1737 1748 ASL 0885 ASY 0747 0892 0898 0951 0969 1036 1183 AVA 1009 1016 1073 1208 1224 1279 1342 1357 1400 AZA 0272 0339 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313 1327 1354 AZU 0365 0372 0462 0494 0527 0529 0532 BEC 0863 BEL 0229 0249 0291 0324 1085 BER 0288 0322 0739 CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769 0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450 1539 CBJ 0988 1020 1028 1052 1753 1763 1775 1782 1847 1862 1880 CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873 0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187 1199 1216 1237 1260 1282 1304 1330 1333 1353 1373 1383 1396 1413 1434 1444 1459 1471 1493 1509 1525 1538 1541 1563 1570 1587 1658 1673 1685 1695 1752 1765 1786 1802 1807 1811 CEB 1420 1445 1495 1527 1552 1602 1712 1789 CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830 0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291 1303 1324 1331 1372 1375 1402 1421 1429 1440 1461 1468 1479 1484 1500 1520 1537 1547 1551 1569 1588 1595 1603 1617 1632 1639 1655 1664 1788 1796 1798 1801 1804 1809 1816 1833 1841 1842 1868 1869 1873 1881 CHH 0875 0881 0906 0982 1159 1168 1178 1190 1255 1325 1438 1532 1558 1573 1591 1614 1634 1656 1663 1677 1686 1703 1827 1831 1837 1855 1860 1871 1875 CPA 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0679 0776 0850 0855 0895 0915 0959 1163 1196 1222 1239 1285 1317 1343 1349 1362 1366 1387 1409 1436 1443 1618 1621 CRK 0396 0452 1031 1034 1039 1042 1051 1054 1059 1062 1099 1105 1107 1115 1124 1146 1157 1277 1286 1322 1358 1369 1384 1398 1668 1863 1865 1874 CRL 0285 0320 1359 1376 CSA 0425 CSC 1082 1138 1241 1397 1432 1528 1579 1662 1746 1780 1825 1856 CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954 0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 1335 1392 1425 1430 1494 1519 1536 1575 1593 1625 1636 1645 1699 1714 1760 1776 1793 1814 1815 1818 1821 1826 1846 1852 1858 1885 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 20 @A330 SERVICE BULLETIN OPERATOR MSN CSZ 1810 1829 1839 1867 1879 D2F 0209 0968 1112 DAH 0644 0647 0650 0653 0667 1613 1630 1649 DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620 0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799 0806 0817 0827 0843 0857 0858 0859 0865 1627 1628 1637 1679 1701 1716 1720 1721 1769 1783 DGA 0240 1735 1808 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905 0913 0922 0989 1292 1305 1314 1497 EDW 1193 1711 EIN 0269 0330 0397 0841 0847 0985 1025 1106 1742 1744 1791 1817 ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852 0854 0868 0975 0991 1032 1070 1071 1081 1167 1205 1226 1245 1414 1486 1521 1524 1772 EVA 0678 0693 0755 1254 1268 1274 1684 1690 1767 1778 1794 1806 EVE 0670 0802 1691 F2I 0200 FBU 1727 FIN 0994 1007 1013 1023 1067 1078 1088 1173 FJI 1394 1416 1465 1692 FWI 0253 0343 0758 0965 1021 1265 GCR 0919 1756 1758 1773 1805 1840 1849 GFA 0276 0281 0286 0287 0334 0340 GIA 1184 1214 1261 1288 1364 1410 1446 1474 1548 1560 1577 1585 1654 1671 1698 1709 1723 1733 GRL 0230 HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404 1422 1469 1488 1496 1511 1530 1565 1606 1615 1672 1732 1823 HDA 0234 0244 0405 0479 0512 0581 0669 0673 1457 1503 1523 1545 1557 1567 1598 HFY 0211 0262 1008 1878 HKC 1175 1320 HVN 0366 0943 0962 1019 1256 1266 I2L 0275 0444 0454 0469 0493 0665 0822 0828 0911 IAW 1339 IBE 1377 1385 1405 1426 1437 1490 1507 1515 1694 1700 1710 1719 1728 1736 1740 1747 1755 1761 1777 1784 1835 1854 1864 1877 1882 IRA 1540 1586 JAI 0888 0923 0947 0956 1351 1361 1370 1391 JAV 0409 KAC 1626 1643 1653 1678 1681 KAL 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0428 0484 0490 0550 1133 1155 1200 1203 1393 1556 1576 1590 1611 1638 1647 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 21 @A330 SERVICE BULLETIN OPERATOR MSN KLM 0682 0686 0703 0738 0770 0801 0925 1161 1287 1294 1300 1381 1580 LAA 1412 1505 1543 LKE 1838 1843 1851 1866 LNI 1675 1680 1693 MAS 1136 1148 1180 1209 1219 1229 1234 1243 1281 1318 1336 1337 1347 1388 1395 1431 1470 1489 MAU 0883 1057 MEA 0926 0984 0995 0998 1725 MLM 0451 MNB 1332 MOV 0535 0655 0661 MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246 NMB 1451 1466 NWS 1213 1221 OBS 0833 OHY 0316 0345 0353 0362 0404 0437 0491 0509 0525 0625 0632 OMA 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599 ONE 1492 1506 1508 1608 1657 P2C 0891 0927 PAL 1449 1456 1460 1463 1467 1475 1482 1504 1510 1531 1546 1553 1559 1566 1568 PLM 0261 0265 0551 QAF 0487 0605 QFA 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0842 0853 0887 0940 0945 0976 1061 1094 1169 1174 1198 1251 1258 1365 QTR 0441 0473 0489 0511 0521 0571 0623 0637 0638 0659 0680 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820 0826 0849 0893 0907 0918 1350 1386 1406 1578 1584 1594 1688 1708 RNA 1872 RSF 0980 0996 1235 1379 1478 1516 RSY 0283 0293 0295 0946 RWD 1741 1759 RZO 0970 SAA 1191 1210 1223 1236 1249 1271 1745 1754 1757 1779 1792 SAF 1667 1762 1799 1822 1857 1886 SAI 0811 0819 0834 0900 SAS 0496 0497 0515 0568 1660 1665 1697 1715 SEY 0751 0807 SIA 0978 0983 0986 1010 1132 1149 1156 1382 1401 1427 1447 1453 1477 1485 1517 1544 1562 1597 1609 1633 1648 1666 SVA 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513 1724 1726 1729 1731 1734 1738 1739 1743 1749 1764 1766 1770 1774 1781 1790 1797 1800 1803 1812 1834 SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290 1355 1403 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 22 @A330 SERVICE BULLETIN OPERATOR MSN SXD 0504 0530 0555 0573 0612 0616 0684 TAE 0348 TAM 0232 0238 0247 0259 0361 0466 0472 0700 TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486 0877 0899 0904 0914 0934 0997 1006 1012 1015 TAR 1631 1641 TBA 1730 1771 1785 1845 1859 TCX 0254 0266 0301 0398 0948 0967 THA 0346 0990 1003 1035 1037 1060 1074 1086 1090 1263 1269 1289 1338 1348 1374 1408 THY 0463 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901 0932 0939 0949 0961 0977 1004 1092 1118 1150 1160 1170 1172 1204 1212 1228 1240 1298 1307 1311 1344 1418 1442 1458 1476 1483 1487 1491 1499 1501 1514 1529 1542 1550 1554 1571 1592 1616 1620 1622 1629 1635 1640 1642 1644 1651 1696 1704 1706 1713 1718 1722 1750 1768 TLM 1820 1828 1832 TNA 1378 TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498 1555 1601 1610 TPA 1368 1380 1428 1534 TPU 1448 TSC 0177 0248 0250 0251 0271 0314 0369 0407 0427 0455 0480 0518 0536 0795 0966 0971 U6A 0224 UAE 0382 0384 UAF 1080 1186 1250 VIR 0403 0432 0476 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352 VKG 0309 0349 0356 0357 VOZ 1293 1306 1319 1407 1452 1561 WOW 1098 1607 1624 WRC 0296 XAX 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066 1075 1126 1131 1165 1411 1423 1433 1481 1533 1549 1581 1589 1596 1600 1612 1619 1646 1659 1670 1674 XLF 0501 0597 0635 1360 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 23 @A330 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0177 0200 0209 0224 0231 0234 0240 0244 0248 0251 0261 0265 0283 0285 0288 0293 0295 0301 0306 0313 0314 0316 0320 0326 0328 0345 0346 0348 0365 0369 0372 0382 0384 0386 0389 0392 0393 0396 0403 0405 0409 0418 0420 0421 0422 0423 0425 0432 0437 0439 0441 0443 0444 0448 0451 0452 0454 0455 0458 0465 0469 0472 0473 0476 0477 0479 0481 0486 0489 0491 0493 0498 0500 0503 0506 0507 0508 0509 0510 0512 0522 002 0181 0195 0206 0211 0219 0222 0223 0226 0229 0230 0232 0238 0241 0247 0249 0250 0253 0254 0255 0256 0258 0259 0262 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281 0284 0286 0287 0290 0291 0296 0300 0303 0305 0308 0309 0311 0312 0315 0317 0322 0323 0324 0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0349 0350 0351 0353 0356 0357 0358 0361 0362 0364 0366 0368 0370 0375 0380 0388 0397 0398 0400 0401 0404 0407 0408 0412 0419 0427 0428 0456 0461 0462 0463 0466 0480 0484 0487 0490 0494 0496 0497 0501 0502 0504 0505 001 002 0511 0513 0515 0516 0518 0519 0521 0524 0525 0526 0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549 0550 0551 0552 0553 0555 0558 0564 0565 0567 0568 0570 0571 0573 0574 0576 0578 0579 0581 0584 0587 0588 0591 0593 0595 0597 0600 0602 0603 0605 0607 0609 0610 0612 0614 0616 0618 0620 0621 0623 0625 0627 0629 0631 0632 0633 0634 0635 0636 0637 0638 0640 0641 0642 0644 0645 0647 0648 0649 0650 0652 0653 0654 0655 0656 0657 0658 0659 0661 0662 0663 0664 0665 0666 0667 0669 0670 0671 0673 0674 0675 0676 0678 0679 0680 0682 0683 0684 0686 0687 0688 0690 0691 0692 0693 0695 0696 0697 0699 0700 0701 0703 0704 0705 0707 0708 0709 0711 0712 0713 0714 0716 0717 0718 0720 0721 0722 0724 0725 0726 0728 0729 0730 0732 0733 0734 0735 0737 0738 0739 0741 0742 0743 0745 0746 0747 0749 0750 0751 0752 0754 0755 0756 0758 0759 0760 0769 0770 0772 0773 0774 0776 0777 0778 0780 0781 0782 0784 0785 0786 0788 0789 0791 0792 0795 0796 0797 0799 0801 0802 0803 0805 0806 0807 0809 0810 0811 0813 0814 0815 0817 0818 0819 0820 0821 0822 0823 0826 003 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 24 @A330 SERVICE BULLETIN MSN CONFIGURATION 0824 0825 0827 0828 0830 0831 0832 0833 0834 0836 0838 0839 0840 0841 0842 0843 0845 0847 0849 0850 0851 0852 0853 0854 0855 0857 0858 0859 0860 0861 0862 0863 0865 0866 0867 0868 0869 0871 0873 0874 0875 0876 0877 0879 0881 0882 0883 0884 0885 0887 0888 0889 0890 0891 0892 0893 0895 0896 0898 0899 0900 0901 0903 0904 0905 0906 0907 0908 0909 0911 0913 0914 0915 0916 0918 0919 0920 0922 0923 0925 0926 0927 0928 0930 0931 0932 0934 0935 0936 0937 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948 0949 0950 0951 0952 0954 0956 0957 0958 0959 0961 0962 0963 0964 0965 0966 0967 0968 0969 0970 0971 0973 0974 0975 0976 0977 0978 0979 0980 0982 0983 0984 0985 0986 0988 0989 0990 0991 0992 0994 0995 0996 0997 0998 1000 1001 1002 1003 1004 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016 1018 1019 1020 1021 1022 1023 1025 1026 1028 1029 1031 1032 1033 1034 1035 1036 1037 1038 1039 1041 1042 1043 1044 1045 1046 1047 1048 1049 1051 1052 1053 1054 1055 1057 1058 1059 1060 1061 1062 1063 1065 1066 1067 1069 1070 1071 1072 1073 1074 1075 1076 1077 1078 1080 1081 1082 1084 1085 1086 1087 1088 1089 1090 1092 1093 1094 1095 1096 1097 1098 1099 1100 1101 1103 1104 1105 1106 1107 1108 1110 1112 1114 1115 1116 1118 1120 1123 1124 1126 1127 1129 1130 1131 1132 1133 1135 1136 1137 1138 1141 1143 1145 1146 1147 1148 1149 1150 1151 1153 1155 1156 1157 1159 1160 1161 1163 1164 1165 1167 1168 1169 1170 1171 1172 1173 1174 1175 1177 1178 1180 1181 1183 1184 1186 1187 1188 1189 1190 1191 1192 1193 1195 1196 1198 1199 1200 1201 1202 1203 1204 1205 1206 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217 1218 1219 1220 1221 1222 1223 1224 1225 1226 1227 1228 1229 1230 1231 1232 1233 1234 1235 1236 1237 1238 1239 1240 1241 1243 1244 1245 1246 1247 1248 1249 1250 1251 1252 1254 1255 1256 1258 1259 1260 1261 1262 1263 1264 1265 1266 1267 1268 1269 1270 1271 1272 1274 1275 1276 1277 1278 1279 1280 1281 1282 1283 1284 1285 1286 1287 1288 1289 1290 1291 1292 1293 1294 1295 1296 1297 1298 1299 1300 1301 1302 1303 1304 1305 1306 1307 1308 1309 1310 1311 1312 1313 1314 1315 1316 1317 1318 1319 1320 1321 1322 1323 1324 1325 1326 1327 1328 1329 1330 1331 1332 1333 1334 1335 1336 1337 1338 1339 1340 1341 1342 1343 1344 1345 1346 1347 1348 1349 1350 1351 1352 1353 1354 1355 1356 1357 1358 1359 1360 1361 1362 1363 1364 1365 1366 1367 1368 1369 1370 1371 1372 1373 1374 1375 1376 1377 1378 1379 1380 1381 1382 1383 1384 1385 1386 1387 1388 1389 1390 1391 1392 1393 1394 1395 1396 1397 1398 1399 1400 1401 1402 1403 1404 1405 1406 1407 1408 1409 1410 1411 1412 1413 1414 1415 1416 1417 1418 1419 1420 1421 1422 1423 1425 1426 1427 1428 1429 1430 1431 1432 1433 1434 1435 1436 1437 1438 1439 1440 004 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 25 @A330 SERVICE BULLETIN MSN CONFIGURATION 1441 1442 1443 1444 1445 1446 1447 1448 1449 1450 1451 1452 1453 1454 1455 1456 1457 1458 1459 1460 1461 1462 1463 1464 1465 1466 1467 1468 1469 1470 1471 1472 1473 1474 1475 1476 1477 1478 1479 1480 1481 1482 1483 1484 1485 1486 1487 1488 1489 1490 1491 1492 1493 1494 1495 1496 1497 1498 1499 1500 1501 1502 1503 1504 1505 1506 1507 1508 1509 1510 1511 1512 1513 1514 1515 1516 1517 1518 1519 1520 1521 1523 1524 1525 1526 1527 1528 1529 1530 1531 1532 1533 1534 1535 1536 1537 1538 1539 1540 1541 1542 1543 1544 1545 1546 1547 1548 1549 1550 1551 1552 1553 1554 1555 1556 1557 1558 1559 1560 1561 1562 1563 1564 1565 1566 1567 1568 1569 1570 1571 1572 1573 1574 1575 1576 1577 1578 1579 1580 1581 1582 1583 1584 1585 1586 1587 1588 1589 1590 1591 1592 1593 1594 1595 1596 1597 1598 1599 1600 1601 1602 1603 1604 1605 1606 1607 1608 1609 1610 1611 1612 1613 1614 1615 1616 1617 1618 1619 1620 1621 1622 1623 1624 1625 1626 1627 1628 1629 1630 1631 1632 1633 1634 1635 1636 1637 1638 1639 1640 1641 1642 1643 1644 1645 1646 1647 1648 1649 1650 1651 1653 1654 1655 1656 1657 1658 1659 1660 1662 1663 1664 1665 1666 1667 1668 1669 1670 1671 1672 1673 1674 1675 1676 1677 1678 1679 1680 1681 1684 1685 1686 1687 1688 1689 1690 1691 1692 1693 1694 1695 1696 1697 1698 1699 1700 1701 1703 1704 1706 1708 1709 1710 1711 1712 1713 1714 1715 1716 1718 1719 1720 1721 1722 1723 1724 1725 1726 1727 1728 1729 1730 1731 1732 1733 1734 1735 1736 1737 1738 1739 1740 1741 1742 1743 1744 1745 1746 1747 1748 1749 1750 1751 1752 1760 004 1753 1754 1755 1756 1757 1758 1759 1761 1762 1763 1764 1765 1766 1767 1768 1769 1770 1771 1772 1773 1774 1775 1776 1777 1778 1779 1780 1781 1782 1783 1784 1785 1786 1787 1788 1789 1790 1791 1792 1793 1794 1796 1797 1798 1799 1800 1801 1802 1803 1804 1805 1806 1807 1808 1809 1810 1811 1812 1814 1815 1816 1817 1818 1820 1821 1822 1823 1825 1826 1827 1828 1829 1830 1831 1832 1833 1834 1835 1837 1838 1839 1840 1841 1842 1843 1845 1846 1847 1848 1849 1851 1852 1854 1855 1856 1857 1858 1859 1860 1862 1863 1864 1865 1866 1867 1868 1869 1871 1872 1873 1874 1875 1877 1878 1879 1880 1881 1882 1883 1885 1886 005 (5) Configuration definition The following table gives further information of the Configuration Definition. **CONF 001 Config 001 is valid for aircraft on which: - MOD No. 49202S16307 is not embodied and on which - Service Bulletin No. A330-57-3083 is not accomplished. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 9 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 26 @A330 SERVICE BULLETIN **CONF 002 Config 002 is valid for aircraft on which: - MOD No. 49202S16307 is not embodied and on which - Service Bulletin No. A330-57-3083 is accomplished. **CONF 003 Config 003 is valid for aircraft on which: - MOD No. 49202S16307 is embodied - MOD No. 55306S18660 is not embodied - MOD No. 205225S33534 is not embodied. OR - MOD No. 49202S16307 is embodied - MOD No. 55792S18775 is not embodied - MOD No. 205225S33534 is not embodied. **CONF 004 Config 004 is valid for aircraft on which: - MOD No. 49202S16307 is embodied - MOD No. 55306S18660 is embodied - MOD No. 205225S33534 is not embodied OR - MOD No. 49202S16307 is embodied - MOD No. 55792S18775 is embodied - MOD No. 205225S33534 is not embodied **CONF 005 Config 005 is valid for aircraft on which: - MOD No. 49202S16307 is embodied - MOD No. 55306S18660 is embodied - MOD No. 205225S33534 is embodied. OR - MOD No. 49202S16307 is embodied - MOD No. 55792S18775 is embodied - MOD No. 205225S33534 is embodied. For further information concerning the Configuration Definition, refer to Appendix 02 - Configuration Definition table . (6) Material Effectivity NOTE : Only 1 TOOL Kit is necessary to perform the Cold Working, either TOOLA01 or TOOLA02 depending on the supplier chosen. **CONF 001, 003 thru 004 MATERIAL QTY PER A/C SEE NOTES Kit 573132A01R01 1 Kit 573132A02R00 1 Consumable CMLA01 1 Standard tool TOOLA01 1 Standard tool TOOLA02 1 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 10 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 27 @A330 SERVICE BULLETIN **CONF 002 MATERIAL QTY PER A/C SEE NOTES Kit 573132A01R01 1 Consumable CMLA01 1 Standard tool TOOLA01 1 Standard tool TOOLA02 1 **CONF 005 MATERIAL QTY PER A/C SEE NOTES Kit 573132A02R00 1 Consumable CMLA01 1 Standard tool TOOLA01 1 Standard tool TOOLA02 1 **CONF ALL B. CONCURRENT REQUIREMENTS None C. REASON (1) History The area at Frame (FR) 40 is subjected to a specific maintenance program. A new campaign of modifications has been launched to improve the maintenance program, decrease the number of maintenance actions and to improve the structural potential of the aircraft to meet the future Extended Service Goal (ESG) / Design Service Goal (DSG). (2) Objective/Action This Service Bulletin recommends the application of Cold Working on holes 25, 38, 39 and 43 at FR40 to improve the fatigue behaviour. Depending on the configuration, this reinforcement consists in doing a first or second cold expansion of fastener holes 25, 38, 39 and 43 and installing oversized fastener with high interference. The procedure as described in this Service Bulletin is to be performed if no AIRBUS repair and/or repair improvement has been previously performed in the same area. In case of repairs performed previously, please contact AIRBUS Repair Support department for further instructions. (3) Advantages Accomplishment of this Service Bulletin will contribute to prevent cracks and will increase the fatigue life in the area of FR40. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 11 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 28 @A330 SERVICE BULLETIN (4) Operational/Maintenance Consequences Depending on configuration, accomplishment of this Service Bulletin cancels the requirements of Inspection Service Bulletin No. A330-57-3116 for holes 25, 38, 39 and 43, if accomplished after the lower bound described in Inspection Service Bulletin No. A330-57-3116. For hole 25, for Aircraft in Config. 002, this modification Service Bulletin is not terminative and must be monitored by Inspection Service Bulletin No. A330-57-3116. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 573132-831-801-001: Modification (1) Remove the Fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (2) Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (3) Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (4) Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (5) Remove the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (6) Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (7) Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (8) Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side **CONF 002 Task 573132-831-801-001: Modification (1) Remove the Fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (2) Do an Inspection of the Fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (3) Do a Cold Working of the fastener Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 12 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 29 @A330 SERVICE BULLETIN (4) Install the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (5) Remove the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (6) Do an Inspection of the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (7) Do a Cold Working of the fastener Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (8) Install the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side **CONF 003 Task 573132-831-801-001: Modification (1) Remove the Fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (2) Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (3) Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (4) Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (5) Remove the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (6) Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (7) Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (8) Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side **CONF 004 Task 573132-831-801-001: Modification (1) Remove the Fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (2) Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (3) Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 13 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 30 @A330 SERVICE BULLETIN STGR40 at FR40 on the LH side (4) Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side (5) Remove the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (6) Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (7) Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side (8) Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side **CONF 005 Task 573132-831-801-001: Modification (1) Remove the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the LH side (2) Do an Inspection of the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the LH side (3) Do a Cold Working of the Fastener Holes 25 between STGR38 and STGR39 at FR40 on the LH side (4) Install the Fastener at the Holes 25 between STGR38 and STGR39 at FR40 on the LH side (5) Remove the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the RH side (6) Do an Inspection of the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the RH side (7) Do a Cold Working of the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the RH side (8) Install the Fastener at the Holes 25 between STGR38 and STGR39 at FR40 on the RH side **CONF ALL E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 14 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 31 @A330 SERVICE BULLETIN (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation 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 573132-831-801-001: Modification Get Access 10.00 On Aircraft Remove the Fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 1.50 Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Remove the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 1.50 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 15 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 32 @A330 SERVICE BULLETIN Task 573132-831-801-001: Modification Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Tests 0.50 Close-Up 11.00 TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAA given in Appendix 01. **CONF 002 Task 573132-831-801-001: Modification Get Access 10.00 On Aircraft Remove the Fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.50 Do an Inspection of the Fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.50 Do a Cold Working of the fastener Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 1.00 Install the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.50 Remove the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.50 Do an Inspection of the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.50 Do a Cold Working of the fastener Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 1.00 Install the fastener at the Holes 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.50 Tests 0.50 Close-Up 11.00 TOTAL MANHOURS 26.50 ELAPSED TIME (HOURS) 13.50 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAB given in Appendix 01. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 16 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 33 @A330 SERVICE BULLETIN **CONF 003 Task 573132-831-801-001: Modification Get Access 10.00 On Aircraft Remove the Fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 1.50 Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Remove the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 1.50 Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Tests 0.50 Close-Up 11.00 TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAA given in given in Appendix 01. **CONF 004 Task 573132-831-801-001: Modification Get Access 10.00 On Aircraft Remove the Fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 17 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 34 @A330 SERVICE BULLETIN Task 573132-831-801-001: Modification Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 1.50 Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the LH side 0.75 Remove the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Do an Inspection of the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Do a Cold Working of the fastener Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 1.50 Install the fastener at the Holes 25, 38, 39 and 43 between STGR38 and STGR40 at FR40 on the RH side 0.75 Tests 0.50 Close-Up 11.00 TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAA given in Appendix 01. **CONF 005 Task 573132-831-801-001: Modification Get Access 10.00 On Aircraft Remove the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the LH side 0.25 Do an Inspection of the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the LH side 0.25 Do a Cold Working of the Fastener Holes 25 between STGR38 and STGR39 at FR40 on the LH side 0.50 Install the Fastener at the Holes 25 between STGR38 and STGR39 at FR40 on the LH side 0.25 Remove the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the RH side 0.25 Do an Inspection of the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the RH side 0.25 Do a Cold Working of the Fastener at the Hole 25 between STGR38 and STGR39 at FR40 on the RH side 0.50 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 18 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 35 @A330 SERVICE BULLETIN Task 573132-831-801-001: Modification Install the Fastener at the Holes 25 between STGR38 and STGR39 at FR40 on the RH side 0.25 Tests 0.50 Close-Up 11.00 TOTAL MANHOURS 24.00 ELAPSED TIME (HOURS) 12.25 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAC given in Appendix 01. **CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-16-00 20-21-11 21-20-00 21-52-41 24-41-00 25-20-00 25-52-00 25-80-00 27-84-41 32-12-00 36-22-19 52-30-00 52-32-11 53-35-13 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 In Service Information (ISI) 51.48.00001 Non Destructive Test Manual (NTM) 51-10-01 51-10-08 Service Bulletin (SB) A330-57-3083 A330-57-3116 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 Tool Equipment Manual (TEM) 52-30-00 **CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-16-00 20-21-11 21-20-00 21-52-41 24-41-00 25-20-00 25-52-00 25-80-00 27-84-41 32-12-00 36-22-19 52-30-00 52-32-11 53-35-13 Consumable Material List (CML) DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 19 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 36 @A330 SERVICE BULLETIN Elec. Std. Practices Manual (ESPM) 20-55-00 In Service Information (ISI) 51.48.00001 Non Destructive Test Manual (NTM) 51-10-01 51-10-08 Service Bulletin (SB) A330-57-3083 A330-57-3116 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 Tool Equipment Manual (TEM) 52-30-00 **CONF 003 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-16-00 20-21-11 21-20-00 21-52-41 24-41-00 25-20-00 25-52-00 25-80-00 27-84-41 32-12-00 36-22-19 52-30-00 52-32-11 53-35-13 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 In Service Information (ISI) 51.48.00001 Non Destructive Test Manual (NTM) 51-10-01 51-10-08 Service Bulletin (SB) A330-57-3116 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 Tool Equipment Manual (TEM) 52-30-00 **CONF 004 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-16-00 20-21-11 21-20-00 21-52-41 24-41-00 25-20-00 25-52-00 25-80-00 27-84-41 32-12-00 36-22-19 52-30-00 52-32-11 53-35-13 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 In Service Information (ISI) 51.48.00001 Non Destructive Test Manual (NTM) 51-10-01 51-10-08 Service Bulletin (SB) A330-57-3116 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 Tool Equipment Manual (TEM) 52-30-00 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 20 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 37 @A330 SERVICE BULLETIN **CONF 005 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-16-00 20-21-11 21-20-00 21-52-41 24-41-00 25-20-00 25-52-00 25-80-00 27-84-41 32-12-00 36-22-19 52-30-00 52-32-11 53-35-13 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 In Service Information (ISI) 51.48.00001 Non Destructive Test Manual (NTM) 51-10-01 51-10-08 Service Bulletin (SB) A330-57-3116 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 Tool Equipment Manual (TEM) 52-30-00 **CONF ALL K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 21 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 38 @A330 SERVICE BULLETIN This Page Intentionally Left Blank DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 22 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 39 @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 573132A01R01 Kit 573132A02R00 AIRBUS Material, Logistics and Suppliers ATP II B, Hein-Sass-Weg 24 21129 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by E-mail: airbus.kit@airbus.com Telephone Hotline: +49 40 743 51616 (2) Price and Availability Kit 573132A01R01 Cost 170.00 USD Availability 180 calendar days from receipt of order The availability given above is the standard lead time from the date of your purchase order. If items are required 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. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 573132A02R00 Cost 51.00 USD Availability 180 calendar days from receipt of order The availability given above is the standard lead time from the date of your purchase order. If items are required 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. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 23 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 40 @A330 SERVICE BULLETIN For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department: monitored.retrofit@airbus.com. C. LIST OF COMPONENTS Kit 573132A01R01 ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES 10 EN6115K8-22 4 BOLT 11 ASNA2531-8 6 NUT 14 EN6115K8-19 2 BOLT 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 573132A02R00 ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES 12 EN6115K6-12 2 BOLT 13 ASNA2531-6 2 NUT 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 Coating - Flexible Structure 04QAB2 As required Polysulfide Sealant-General Purpose Interfay 06AAC1 As required Polysulfide Sealant-Low Density Multi Purpose Fil 06ACB1 As required Polysulfide Sealant-Fuel Contaminated Area Brusha 06ADA1 As required Adhesion Promoter-For Polysulfide Sealant 06PAG1 As required Non Aqueous Cleaner-General 08BAA9 As required Textile-Lint Free Cotton 14SBA1 As required DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 24 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 41 @A330 SERVICE BULLETIN (2) Components None (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING (1) Tooling - Price and Availability (a) Procurement Addresses NOTE : Only 1 TOOL Kit is necessary to perform the Cold Working, either TOOLA01 or TOOLA02 depending on the supplier chosen. Operators interested in obtaining the Fatigue Technology Incorporated (FTI) tool kit should contact: Standard tool TOOLA01 Standard tool TOOLA02 Fatigue Technology Inc. 401 Andover Park East SEATTLE, WA 98188-7605 USA Internet: www.fatiguetech.com Phone: (206) 2462010 Fax: (206) 2449886 Operators interested in obtaining the West Coast Industries (WCI) tool kit should contact: Standard tool TOOLA01 Standard tool TOOLA02 West Coast Industries Inc. 14900 Whitman Ave. N Seattle, Washington 98133 Tel: (206) 365-7513 Fax: (206) 365-7483 Email: info@coldwork.com Europe, Middle-East, Africa, India and Russia: customer@capaero.com /+33 5 61 92 04 91 (France) (b) Price and Availability Standard tool TOOLA01 Procurement to be negotiated directly with FTI. Standard tool TOOLA02 Procurement to be negotiated directly with WCI. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 25 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 42 @A330 SERVICE BULLETIN (2) Tools NOTE : Only 1 TOOL Kit is necessary to perform the Cold Working, either TOOLA01 or TOOLA02 depending on the supplier chosen. NOTE : To accomplish this Service Bulletin it is necessary to use the tools listed in the subsequent re ferenced tasks: - AMM Task 52-32-11-820-803 - NTM Task 51-10-01-250-801 - NTM Task 51-10-08 - TEM 52-30-00 Standard tool TOOLA01 ITEM TOOL N˚ TOOL NAME QTY SEE NOTES DKA330573132-1 Durable Tooling 1 (1) EKA330573132-1 Expendable Tooling 1 (2) FTIA330573132-1 Capital Tooling 1 (3) NOTE : FTI has allocated the following tool kit numbers for cold expansion: For the definition of capital, durable and expendable tools, refer to ISI 51.48.00001. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE (1) : Durable tooling: Ref. DK-A330-57-3132-1 The durable tool kit contains the minimum quantity of durable tools necessary to accomplish the Service Bulletin on one aircraft. If the Service Bulletin is to be accomplished on more than one aircraft, the number of durable kits required can be established by reference to refer to ISI 51.48.00001. NOTE (2) : Expendable tooling: Ref. EK-A330-57-3132-1 The expendable tool kit contains the quantity of expendable tools required to accomplish the Service Bulletin on one aircraft. Order one expendable tool kit for every aircraft on which this Service Bulletin is to be accomplished. NOTE (3) : Capital tooling: Ref. FTI-A330-57-3132-1 The capital tools provided in this kit are not specific to this Service Bulletin and are normally already available in operators’ stock as a long- term investment or can be loaned from FTI. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 26 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 43 @A330 SERVICE BULLETIN Standard tool TOOLA02 ITEM TOOL N˚ TOOL NAME QTY SEE NOTES DKA330573132-1 Durable Tooling 1 (1) EKA330573132-1 Expendable Tooling 1 (2) WCIA330573132-1 Capital Tooling 1 (3) NOTE : WCI has allocated the following tool kit numbers for cold expansion: For the definition of capital, durable and expendable tools, refer to ISI 51.48.00001. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE (1) : Durable tooling: Ref. DK-A330-57-3132-1 The durable tool kit contains the minimum quantity of durable tools necessary to accomplish the Service Bulletin on one aircraft. If the Service Bulletin is to be accomplished on more than one aircraft, the number of durable kits required can be established by reference to refer to ISI 51.48.00001. NOTE (2) : Expendable tooling: Ref. EK-A330-57-3132-1 The expendable tool kit contains the quantity of expendable tools required to accomplish the Service Bulletin on one aircraft. Order one expendable tool kit for every aircraft on which this Service Bulletin is to be accomplished. NOTE (3) : Capital tooling: Ref. WCI-A330-57-3132-1 The capital tools provided in this kit are not specific to this Service Bulletin and are normally already available in operators’ stock as a long- term investment or can be loaned from WCI. (3) Special Tools None DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 27 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 44 @A330 SERVICE BULLETIN This Page Intentionally Left Blank DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 28 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 45 @A330 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 573132-831-801-001 - Modification WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words ’refer to’ are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words ’in accordance with’ are used then the given procedure must be followed. NOTE : The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE : Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE : This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions contained herein, contact AIRBUS for further instructions and approval. Task Associated Data **CONF 001 Zone 131 132 141 142 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 29 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 46 @A330 SERVICE BULLETIN Manpower TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 **CONF 002 Zone 131 132 141 142 Manpower TOTAL MANHOURS 26.50 ELAPSED TIME (HOURS) 13.50 **CONF 003 Zone 131 132 141 142 Manpower TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 **CONF 004 Zone 131 132 141 142 Manpower TOTAL MANHOURS 29.00 ELAPSED TIME (HOURS) 14.75 **CONF 005 Zone 131 132 141 142 Manpower TOTAL MANHOURS 24.00 ELAPSED TIME (HOURS) 12.25 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 573132-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 30 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 47 @A330 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-16-00-912-801 Task 20-21-11-911-801 Task 21-20-00-010-801 Task 21-20-00-410-801 Consumable Material List (CML) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (d) For the specification of Material Numbers (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (e) If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’ column. (f) If the length of any fastener specified in this Service Bulletin does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. (g) Get alternative and substitute fastener data in accordance SRM 51-43-00. (h) Remove and install fasteners in accordance with SRM 51-42-00. (i) Get fastener hole diameters and drill data in accordance with SRM 51-44-00. (j) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (k) For the general removal of air-conditioning distribution ducts, refer to AMM Task 21-20-00-010-801. (l) For the general installation of air-conditioning distribution ducts, refer to AMM Task 21-20-00-410-801. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 31 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 48 @A330 SERVICE BULLETIN (m) Do the cold working of the fastener holes in accordance with SRM 51-48-00. (n) Apply sealant in accordance with SRM 51-24-00. (o) Renew the protective finish in accordance with SRM 51-75-12. (p) Do the countersink of holes, in accordance with refer to SRM 51-46-00. (2) Subtask 573132-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 573132-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-16-00-912-801 Task 20-21-11-911-801 Task 21-20-00-010-801 Task 21-20-00-410-801 Consumable Material List (CML) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (d) For the specification of Material Numbers (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 32 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 49 @A330 SERVICE BULLETIN (e) If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’ column. (f) If the length of any fastener specified in this Service Bulletin does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. (g) Get alternative and substitute fastener data in accordance SRM 51-43-00. (h) Remove and install fasteners in accordance with SRM 51-42-00. (i) Get fastener hole diameters and drill data in accordance with SRM 51-44-00. (j) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (k) For the general removal of air-conditioning distribution ducts, refer to AMM Task 21-20-00-010-801. (l) For the general installation of air-conditioning distribution ducts, refer to AMM Task 21-20-00-410-801. (m) Do the cold working of the fastener holes in accordance with SRM 51-48-00. (n) Apply sealant in accordance with SRM 51-24-00. (o) Renew the protective finish in accordance with SRM 51-75-12. (p) Do the countersink of holes, in accordance with refer to SRM 51-46-00. (2) Subtask 573132-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 003 (1) Subtask 573132-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 33 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 50 @A330 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-16-00-912-801 Task 20-21-11-911-801 Task 21-20-00-010-801 Task 21-20-00-410-801 Consumable Material List (CML) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (d) For the specification of Material Numbers (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (e) If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’ column. (f) If the length of any fastener specified in this Service Bulletin does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. (g) Get alternative and substitute fastener data in accordance SRM 51-43-00. (h) Remove and install fasteners in accordance with SRM 51-42-00. (i) Get fastener hole diameters and drill data in accordance with SRM 51-44-00. (j) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (k) For the general removal of air-conditioning distribution ducts, refer to AMM Task 21-20-00-010-801. (l) For the general installation of air-conditioning distribution ducts, refer to AMM Task 21-20-00-410-801. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 34 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 51 @A330 SERVICE BULLETIN (m) Do the cold working of the fastener holes in accordance with SRM 51-48-00. (n) Apply sealant in accordance with SRM 51-24-00. (o) Renew the protective finish in accordance with SRM 51-75-12. (p) Do the countersink of holes, in accordance with refer to SRM 51-46-00. (2) Subtask 573132-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 004 (1) Subtask 573132-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-16-00-912-801 Task 20-21-11-911-801 Task 21-20-00-010-801 Task 21-20-00-410-801 Consumable Material List (CML) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (d) For the specification of Material Numbers (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 35 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 52 @A330 SERVICE BULLETIN (e) If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’ column. (f) If the length of any fastener specified in this Service Bulletin does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. (g) Get alternative and substitute fastener data in accordance SRM 51-43-00. (h) Remove and install fasteners in accordance with SRM 51-42-00. (i) Get fastener hole diameters and drill data in accordance with SRM 51-44-00. (j) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (k) For the general removal of air-conditioning distribution ducts, refer to AMM Task 21-20-00-010-801. (l) For the general installation of air-conditioning distribution ducts, refer to AMM Task 21-20-00-410-801. (m) Do the cold working of the fastener holes in accordance with SRM 51-48-00. (n) Apply sealant in accordance with SRM 51-24-00. (o) Renew the protective finish in accordance with SRM 51-75-12. (p) Do the countersink of holes, in accordance with refer to SRM 51-46-00. (2) Subtask 573132-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 005 (1) Subtask 573132-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 36 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 53 @A330 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-16-00-912-801 Task 20-21-11-911-801 Task 21-20-00-010-801 Task 21-20-00-410-801 Consumable Material List (CML) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-44-00 51-46-00 51-48-00 51-75-12 51-75-15 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (d) For the specification of Material Numbers (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (e) If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’ column. (f) If the length of any fastener specified in this Service Bulletin does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. (g) Get alternative and substitute fastener data in accordance SRM 51-43-00. (h) Remove and install fasteners in accordance with SRM 51-42-00. (i) Get fastener hole diameters and drill data in accordance with SRM 51-44-00. (j) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (k) For the general removal of air-conditioning distribution ducts, refer to AMM Task 21-20-00-010-801. (l) For the general installation of air-conditioning distribution ducts, refer to AMM Task 21-20-00-410-801. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 37 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 54 @A330 SERVICE BULLETIN (m) Do the cold working of the fastener holes in accordance with SRM 51-48-00. (n) Apply sealant in accordance with SRM 51-24-00. (o) Renew the protective finish in accordance with SRM 51-75-12. (p) Do the countersink of holes, in accordance with refer to SRM 51-46-00. (2) Subtask 573132-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 573132-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 21-20-00-010-801 Task 24-41-00-861-801 Task 25-80-00-000-801 Task 27-84-41-000-802 Task 32-12-00-010-801 Task 52-30-00-010-801 NOTE : For the basic Aircraft configuration, refer to AMM Chapter "Introduction - Aircraft status for maintenance" in Manual Front Matter section. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Put an access platform(s) in position at doors 821. (c) Open the Main Landing Gear (MLG) doors, refer to AMM Task 32-12-00-010-801. (d) Open the FWD cargo-compartment door 821, refer to AMM Task 52-30-00-010-801 . (e) At Frame 40, in the applicable work area, remove the insulation blankets, refer to AMM Task 25-80-00-000-801. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 38 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 55 @A330 SERVICE BULLETIN (f) Remove the gearbox right angle 5011CW and 5071CW, refer to AMM Task 27-84-41-000-802. (g) Remove the necessary air-conditioning ducts, refer to AMM Task 21-20-00-010-801. (h) Energize the aircraft electrical circuits, refer to AMM Task AMM Task 24-41-00-861-801. (2) Subtask 573132-941-002-001 - Safety Precautions Manpower Resources Skills NON SPECIFIC (a) On the AIR control panel 225VU: 1 Make sure that the APU BLEED, the ENG BLEED 1(2) and the PACK 1(2) pushbutton switches are released. 2 Put a WARNING NOTICE in position to tell persons not to operate these pushbutton switches. (b) On the HP ground connectors, put a WARNING NOTICE in position to tell persons not to supply the ground air source. (3) Subtask 573132-010-005-001 - Remove/Open for access in the Belly Fairing Area LH side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-52-41-000-801 Task 53-35-13-000-802 (a) Remove the Belly Fairing Access-Panels 191FB, 191KB and 192PB, refer to AMM Task 53-35-13-000-802. (b) Remove the Air Conditioning Pack (FIN 521HH ), refer to AMM Task 21-52-41-000-801. (4) Subtask 573132-010-003-001 - Remove/Open for Access in the Belly Fairing Areas RH side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Task 21-52-41-000-801 Task 36-22-19-000-801 Task 53-35-13-000-802 DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 39 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 56 @A330 SERVICE BULLETIN References Fig. A-FBCAA Removal/Installation of the Air Conditioning Ducts between FR39.1 and FR40 (Belly Fairing Area) Sheet 01 Fig. A-FBDAA Removal/Installation of the Air Conditioning Ducts between FR39.1 and FR40 (Belly Fairing Area) Sheet 01 Fig. A-FBAAA Removal/Installation of the Heat Shield Sheet 01 Sheet 02 WARNING : MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL. (a) Remove the belly fairing access-panels 193DB, 192JB and 192GB, refer to AMM Task 53-35-13-000-802. (b) If necessary, on the Right Hand (RH) side, remove and retain the air-conditioning pack outlet duct as follows, refer to AMM Task 21-20-00-010-801 and Fig. A- FBCAA Sheet 01 . 1 Remove: 1 Duct Item (5) Retain (c) On the RH side, remove and retain the air ventilation duct as follows, refer to AMM Task 21-20-00-010-801 and Fig. A-FBDAA Sheet 01 . 1 Remove: 1 Duct Item (6) Retain (d) Remove the Air Conditioning Pack (FIN 522HH ), refer to AMM Task 21-52-41-000-801. (e) If necessary, remove the Wing Bleed-air Duct Sensing Elements (FINs 120HF, 122HF, 124HF, 131HF, 133HF and 135HF), refer to AMM Task 36-22-19-000-801. (f) Remove the Heat Shield of the RH Conditioning Pack, refer to Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02 . 1 Heat Shield Item (7) Retain 4 Screw Item (8) Retain DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 40 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 57 @A330 SERVICE BULLETIN (5) Subtask 573132-010-001-001 - Remove/Open for Access in the FWD Cargo- Compartment Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Task 25-20-00-010-801 Task 25-52-00-000-801 Task 25-80-00-000-801 Task 52-30-00-010-801 Fig. A-FBBAA Removal/Installation of the Air Conditioning Ducts between FR39.1 and FR40 (FWD Cargo- Compartment) Sheet 01 CAUTION : DO NOT STEP ON THE DUCTS BECAUSE THEY ARE FRAGILE. (a) Remove the Ceiling Panels, the Partition Panels and the Sidewall Panels in the Forward Cargo Compartment 131CX, 131DX, 132CX and 132DX, refer to AMM Task 25-52-00-000-801. (b) On the LH and RH sides, remove the air conditioning ducts between Frame 39.1 and Frame 40, refer to AMM Task 21-20-00-010-801 and Fig. A-FBBAA Sheet 01 . 1 Remove: 2 Duct Item (1) Retain 2 Duct Item (2) Retain 2 Recirculation Filter Item (3) Retain 2 Recirculation Fan Item (4) Retain (c) Remove the necessary insulation blankets, refer to AMM Task 25-80-00-000-801. **CONF 002 (1) Subtask 573132-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 41 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 58 @A330 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 21-20-00-010-801 Task 24-41-00-861-801 Task 25-80-00-000-801 Task 27-84-41-000-802 Task 32-12-00-010-801 Task 52-30-00-010-801 NOTE : For the basic Aircraft configuration, refer to AMM Chapter "Introduction - Aircraft status for maintenance" in Manual Front Matter section. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Put an access platform(s) in position at doors 821. (c) Open the Main Landing Gear (MLG) doors, refer to AMM Task 32-12-00-010-801. (d) Open the FWD cargo-compartment door 821, refer to AMM Task 52-30-00-010-801 . (e) At Frame 40, in the applicable work area, remove the insulation blankets, refer to AMM Task 25-80-00-000-801. (f) Remove the gearbox right angle 5011CW and 5071CW, refer to AMM Task 27-84-41-000-802. (g) Remove the necessary air-conditioning ducts, refer to AMM Task 21-20-00-010-801. (h) Energize the aircraft electrical circuits, refer to AMM Task AMM Task 24-41-00-861-801. (2) Subtask 573132-941-002-001 - Safety Precautions Manpower Resources Skills NON SPECIFIC (a) On the AIR control panel 225VU: 1 Make sure that the APU BLEED, the ENG BLEED 1(2) and the PACK 1(2) pushbutton switches are released. 2 Put a WARNING NOTICE in position to tell persons not to operate these pushbutton switches. (b) On the HP ground connectors, put a WARNING NOTICE in position to tell persons not to supply the ground air source. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 42 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 59 @A330 SERVICE BULLETIN (3) Subtask 573132-010-005-001 - Remove/Open for access in the Belly Fairing Area LH side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-52-41-000-801 Task 53-35-13-000-802 (a) Remove the Belly Fairing Access-Panels 191FB, 191KB and 192PB, refer to AMM Task 53-35-13-000-802. (b) Remove the Air Conditioning Pack (FIN 521HH ), refer to AMM Task 21-52-41-000-801. (4) Subtask 573132-010-003-001 - Remove/Open for Access in the Belly Fairing Areas RH side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Task 21-52-41-000-801 Task 36-22-19-000-801 Task 53-35-13-000-802 Fig. A-FBCAA Removal/Installation of the Air Conditioning Ducts between FR39.1 and FR40 (Belly Fairing Area) Sheet 01 Fig. A-FBDAA Removal/Installation of the Air Conditioning Ducts between FR39.1 and FR40 (Belly Fairing Area) Sheet 01 Fig. A-FBAAA Removal/Installation of the Heat Shield Sheet 01 Sheet 02 WARNING : MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL. (a) Remove the belly fairing access-panels 193DB, 192JB and 192GB, refer to AMM Task 53-35-13-000-802. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 43 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 60 @A330 SERVICE BULLETIN (b) If necessary, on the Right Hand (RH) side, remove and retain the air-conditioning pack outlet duct as follows, refer to AMM Task 21-20-00-010-801 and Fig. A- FBCAA Sheet 01 . 1 Remove: 1 Duct Item (5) Retain (c) On the RH side, remove and retain the air ventilation duct as follows, refer to AMM Task 21-20-00-010-801 and Fig. A-FBDAA Sheet 01 . 1 Remove: 1 Duct Item (6) Retain (d) Remove the Air Conditioning Pack (FIN 522HH ), refer to AMM Task 21-52-41-000-801. (e) If necessary, remove the Wing Bleed-air Duct Sensing Elements (FINs 120HF, 122HF, 124HF, 131HF, 133HF and 135HF), refer to AMM Task 36-22-19-000-801. (f) Remove the Heat Shield of the RH Conditioning Pack, refer to Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02 . 1 Heat Shield Item (7) Retain 4 Screw Item (8) Retain (5) Subtask 573132-010-001-001 - Remove/Open for Access in the FWD Cargo- Compartment Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Task 25-20-00-010-801 Task 25-52-00-000-801 Task 25-80-00-000-801 Task 52-30-00-010-801 Fig. A-FBBAA Removal/Installation of the Air Conditioning Ducts between FR39.1 and FR40 (FWD Cargo- Compartment) Sheet 01 CAUTION : DO NOT STEP ON THE DUCTS BECAUSE THEY ARE FRAGILE. (a) Remove the Ceiling Panels, the Partition Panels and the Sidewall Panels in the Forward Cargo Compartment 131CX, 131DX, 132CX and 132DX, refer to AMM Task 25-52-00-000-801. DATE: Nov 23/16 SERVICE BULLETIN No.: A330-57-3132 REVISION No.: 01 - Feb 05/18 Page: 44 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. 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