# Airbus Service Bulletin A300-54-0075 ## Copies (2) Copies the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist. - Revision 04 ("SB A300-54-0075 Rev04"), 130 pages: PDF https://openairdocs.org/files/sha256/5c/1f/5c1f062c314083eac9fcbf5299081ac35c14f4e6304715db0d929018e0d0f495; text https://openairdocs.org/service-documents/airbus/a300-54-0075/file/5c1f062c3140.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-6671; AD 2016-18-12 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Revision 02 ("A300-54-0075 R2_"), 46 pages: PDF https://openairdocs.org/files/sha256/b8/09/b809adacaba10a875b3c6bb1433b1f5faa520ada869277618943ea293dfe52f4; text https://openairdocs.org/service-documents/airbus/a300-54-0075/file/b809adacaba1.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2009-0789, the docket of AD 2010-06-04. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md) - Type: Service bulletin (Service Bulletin) - Number: A300-54-0075 - Latest revision known: A300-54-0075, Revision 04, dated May 26, 2015 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/airbus/a300-54-0075 ## ADs that cite it (3) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2016-18-12](https://openairdocs.org/ad/2016-18-12.md), effective Oct 13, 2016: Revisions 01, 02, 03 and 04 - [AD 2015-25-06](https://openairdocs.org/ad/2015-25-06.md), effective Feb 2, 2016: Revisions 01, 02 and 03 - [AD 2010-06-04](https://openairdocs.org/ad/2010-06-04.md), effective Apr 15, 2010: Revision 01 Also cited in [3 proposed ADs](https://openairdocs.org/service-documents/airbus/a300-54-0075/proposed.md). ## Text (130 pages) Revision 04, the newest copy. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-6671; AD 2016-18-12 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 @A300 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 MANDATORY MANDATORY MANDATORY ATA SYSTEM: 54 TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. MODIFICATION No.: None This page transmits Revision No.04 of Service Bulletin No.A300-54-0075 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 04 issued to re-integrate in the effectivity aircraft post Modification No. 03599D9179 (REFERENCE MODIFICATION FOR ST2 (SN 207)). Aircraft in post Modification No. 03599D9179 configuration (which is a collection of several modification including structural Modification No. 02434S3600) were in applicability of the A300-54-0075 revision No. 01 and revision No. 02 but not in revision No. 03 as per MSN. CHANGES No change in accomplishment timescale and instructions. The main changes of this revision are: - add aircraft post modification No. 03599D9179 (REFERENCE MODIFICATION FOR ST2 (SN 207)) and pre modification No. 10432S20461 (PANELS IN THE U PPER CORNER AT RIB 8 - ADD A DOUBLER (PRODUCTION SOLUTION), - update the effectivity note, - update of the notes of accomplishment timescale and ALI replaced by ALS, - notes added at the beginning of the accomplishment instruction, - CML reference updated in para. Standard Practices, - update of the sentences in para Job-Set-up and Close-up. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 2 @A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET FRONT MATTER NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. CONFIGURATION UPDATED R SUMMARY EFFECTIVITY OPERATOR LIST UPDATED R REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE UPDATED R APPENDICES APPENDICES UPDATED R Fig. A-FSAAA FIGURE SOLUTION UPDATED R Fig. A-FSCAA FIGURE SOLUTION 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 Material Effectivity MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED R MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED R MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED R COMPLIANCE Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R APPROVAL APPROVAL UPDATED R MANPOWER MANPOWER UPDATED R MANPOWER UPDATED CONFIGURATION UPDATED R MANPOWER UPDATED CONFIGURATION UPDATED R MANPOWER UPDATED CONFIGURATION UPDATED R REFERENCES REFERENCED DOCUMENTATION UPDATED R REFERENCED DOCUMENTATION UPDATED R REFERENCED DOCUMENTATION 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 R LIST OF MATERIALS - OPERATOR SUPPLIED DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 3 @A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Consumable Materials Consumable CMLA01 CONSUMABLE MATERIAL SET UPDATED CONSUMABLE UPDATED R TOOLING Tooling - Price and Availability TOOLING - PRICE AND AVAILABILITY UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 540075- 832-801-001-Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 TASK SOLUTION UPDATED NOTE UPDATED R Task associated data - 001 PANEL UPDATED R Task associated data - 002 PANEL UPDATED R Task associated data - 003 PANEL UPDATED R Subtask 540075-910-001-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-910-001-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-910-001-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-941-001-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-001-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-001-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-832-004-001 SUBTASK SOLUTION UPDATED PANEL UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED LOCATION UPDATED REFERENCES UPDATED R Subtask 540075-832-004-001 SUBTASK SOLUTION UPDATED PANEL UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED LOCATION UPDATED REFERENCES UPDATED R DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 4 @A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 540075-832-004-001 SUBTASK SOLUTION UPDATED PANEL UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED LOCATION UPDATED REFERENCES UPDATED R Subtask 540075-942-002-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-002-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-002-001 SUBTASK SOLUTION UPDATED R TASK 540075- 832-802-001-Inspection Post Repair TASK SOLUTION UPDATED NOTE UPDATED CAUTION UPDATED R Subtask 540075-910-002-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-910-002-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-910-002-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-941-003-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-003-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-003-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-832-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 540075-832-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 540075-832-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 540075-942-003-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-003-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-003-001 SUBTASK SOLUTION UPDATED R DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 5 @A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET TASK 540075- 832-803-001-Inspection Post Service Bulletin No. A300-54-0081 TASK SOLUTION UPDATED NOTE UPDATED CAUTION UPDATED R Subtask 540075-910-003-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-910-003-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-910-003-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 540075-941-004-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-004-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-004-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-832-003-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 540075-832-003-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 540075-832-003-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED REFERENCES UPDATED R Subtask 540075-942-004-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-004-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-004-001 SUBTASK SOLUTION UPDATED R TASK 540075- 833-802-001-Repair TASK SOLUTION UPDATED NOTE UPDATED R Subtask 540075-910-005-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 6 @A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 540075-910-005-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R Subtask 540075-910-005-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R Subtask 540075-941-005-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-005-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-941-005-001 SUBTASK SOLUTION UPDATED NOTE UPDATED ZONE UPDATED R Subtask 540075-833-016-001 SUBTASK SOLUTION UPDATED R Subtask 540075-833-016-001 SUBTASK SOLUTION UPDATED R Subtask 540075-833-016-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-006-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-006-001 SUBTASK SOLUTION UPDATED R Subtask 540075-942-006-001 SUBTASK SOLUTION UPDATED R Fig. A-FFAAA Fig. A-FFAAA Sheet 01 SHEET UPDATED R Fig. A-FRAAA Fig. A-FRAAA Sheet 02 SHEET UPDATED R Fig. A-FRBAA Fig. A-FRBAA Sheet 02 SHEET UPDATED R Fig. A-FRCAA Fig. A-FRCAA Sheet 02 SHEET UPDATED R Appendix 01 - Non Destructive Testing Procedure APPENDIX CONTENT APPENDIX CONTENT UPDATED R Appendix 02 - Elapsed Time Assumption APPENDIX CONTENT APPENDIX CONTENT UPDATED R APPENDIX APPENDIX DELETED D APPENDIX APPENDIX DELETED D APPENDIX APPENDIX DELETED D FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 7 @A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 issued to inform the operators that this Service Bulletin is rendered mandatory. The thresholds and intervals have also been reviewed. Revision No. 02 is issued to replace the PN ASNA2001 by ASNA2314 andreplace R54610124 by SRM 54-10-00. Revision No. 03 issued to update the threshold and intervals as per analysis improvement and in- service crack findings consistency. REVISION SEQUENCE ORIGINAL: Aug 11/93 REVISION No.: 01 - Nov 09/07 REVISION No.: 02 - Jun 26/08 REVISION No. : 03 - Mar 27/13 REVISION No. : 04 - May 26/15 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 8 @A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET This Page Intentionally Left Blank DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 9 @A300 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. MANDATORY MANDATORY MANDATORY ATA SYSTEM: 54 TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES On aircraft fitted with GE pylon, cracks have been reported on pylon side panels (upper section) at rib8. The crack is starting from the hole at the top edge of the panel and running up and downwards from this fastener hole. This Service Bulletin requires a detailed visual and Eddy Current inspection of pylon side panels (upper section) at rib8, in order to detect any crack. This inspection will make it possible to detect crack propagation at an early stage, thus avoiding an extensive repair. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1) : Service Bulletin must be accomplished. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 10 @A300 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 540075A01R02 1 3,910.00 Doubler **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 540075A01R02 1 3,910.00 Doubler **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 540075A01R02 1 3,910.00 Doubler EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) : 001 22P 81T ABR AFG CEL F2I IAW IRA IRM MSR RUN TIW TNO CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 11 @A300 SERVICE BULLETIN SUMMARY OBRM NO MANPOWER **CONF 001 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 540075-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 540075-833-802-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 002 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 540075-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 540075-833-802-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 003 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 12 @A300 SERVICE BULLETIN SUMMARY Task 540075-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 540075-833-802-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 APPENDICES **CONF ALL Appendix 01 - Non Destructive Testing Procedure Appendix 02 - Elapsed Time Assumption DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 13 @A300 SERVICE BULLETIN SUMMARY **CONF ALL AREAS TO BE INSPECTED RIB8 BFWD PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON A A B B A RIB8 NOTES: RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION A_SB_540075_5_SAAA_01_00 Figure A-FSAAA - Sheet 01 Pre Repair and Pre Service Bulletin No. A300-54-0081 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 14 @A300 SERVICE BULLETIN SUMMARY **CONF ALL DETAILED INSPECTION AREA RIB8 BFWD PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON A A B B A RIB8 NOTES: RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION CUT−OUT A_SB_540075_5_SBAA_01_01 Figure A-FSBAA - Sheet 01 Post Repair DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 15 @A300 SERVICE BULLETIN SUMMARY **CONF ALL DETAILED INSPECTION AREA RIB8 BFWD PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON A A B B A RIB8 NOTES: RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION A_SB_540075_5_SCAA_01_00 Figure A-FSCAA - Sheet 01 Post Service Bulletin No. A300-54-0081 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 16 @A300 SERVICE BULLETIN SUMMARY This Page Intentionally Left Blank DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 17 @A300 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 MANDATORY MANDATORY MANDATORY ATA SYSTEM: 54 TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. MODIFICATION No.: None 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 Service Bulletin is only applicable to aircraft listed below on which MOD No. 02434S3600 (NEW ENGINE PYLON-COMMON PARTS) is embodied or MOD No. 03599D9179 (REFERENCE MODIFICATION FOR ST2 (SN 207)) is embodied on one or both pylons and on which MOD No. 10432S20461 (PANELS IN THE UPPER CORNER AT RIB 8 - ADD A DOUBLER (PRODUCTION SOLUTION)) is not embodied. (1) Models B2-203 B2K-3C B4-203 B4-2C C4-203 F4-203 (2) Effectivity by MSN 0154 0160 0173 0175 0180 0183 0185 0200 0203 0210 0212 0218 0220 0226-0227 0234-0236 0239 0244 0247 0255-0256 0259 0261 0274 0277 0292 0299 0302 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 18 @A300 SERVICE BULLETIN (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 001 0203 0218 22P 0236 81T 0277 0292 ABR 0220 0259 AFG 0180 CEL 0212 F2I 0235 IAW 0239 IRA 0173 0185 0226 0256 0299 0302 IRM 0160 0175 0244 MSR 0200 0255 RUN 0154 0183 TIW 0234 0261 0274 TNO 0210 0227 0247 (4) Configuration by MSN MSN CONFIGURATION 0154 0173 0175 0180 0183 0200 0203 0210 0212 0218 0220 0227 0234 0235 0236 0247 0255 0259 0261 0274 0277 0292 0299 0302 003 0160 0185 0226 0244 001 0239 0256 002 (5) Configuration definition **CONF 001 Config. 001 is valid for A300 B2 aircraft. **CONF 002 Config. 002 is valid for A300 B4-100 aircraft. **CONF 003 Config. 003 is valid for A300 B4-200, C4-200 and F4-200 aircraft. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Kit 540075A01R02 1 Consumable CMLA01 As required DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 19 @A300 SERVICE BULLETIN **CONF 002 MATERIAL QTY PER A/C SEE NOTES Kit 540075A01R02 1 Consumable CMLA01 As required **CONF 003 MATERIAL QTY PER A/C SEE NOTES Kit 540075A01R02 1 Consumable CMLA01 As required **CONF ALL B. CONCURRENT REQUIREMENTS None C. REASON (1) History On aircraft fitted with GE pylon, cracks have been reported on pylon side panels (upper section) at rib8. The crack is starting from the hole at the top edge of the panel and running up and downwards from this fastener hole. (2) Objective/Action This Service Bulletin requires a detailed visual and Eddy Current inspection of pylon side panels (upper section) at rib8, in order to detect any crack. (3) Advantages This inspection will make it possible to detect crack propagation at an early stage, thus avoiding an extensive repair. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 20 @A300 SERVICE BULLETIN Task 540075-832-802-001: Inspection Post Repair (1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 (1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 Task 540075-833-802-001: Repair (1) Repair **CONF 002 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Task 540075-832-802-001: Inspection Post Repair (1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 (1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 Task 540075-833-802-001: Repair (1) Repair **CONF 003 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Task 540075-832-802-001: Inspection Post Repair (1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 (1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 21 @A300 SERVICE BULLETIN Task 540075-833-802-001: Repair (1) Repair **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale **CONF 001 This Service Bulletin has been classified Mandatory by the issue of an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA). The AD must be used as the reference document for the mandated accomplishment timescale. Table 1, Config. 001 - Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold Grace period Repetitive Interval All Aircraft Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 5350 FC None None Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 None None 4300 FC Or Apply Service Bulletin No. A300-54-0081 Before next flight None None No crack found and apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 Refer to table 3 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 22 @A300 SERVICE BULLETIN Table 1, Config. 001 - Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold Grace period Repetitive Interval Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 None None 4300 FC Or Apply Service Bulletin No. A300-54-0081 Before next flight None None Crack found but not confirmed with HFEC Inspection and apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 Refer to table 3 Apply TASK 540075-833-802 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy current inspection. and apply TASK 540075-832-802 001 Inspection Post Repair Refer to table 2 Crack found >=20 mm (0.787 in.) Contact Airbus Before next flight None None NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. Table 2, Config. 001 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair Compliance Time Condition Action Threshold (FH or FC whichever occurs first) Grace period Repetitive Interval (FH or FC whichever occurs first) All Aircraft Apply TASK 540075-832-802 001 Inspection Post Repair 11700 FC /13300 FH from repair embodiment 2000 FC See NOTE (*) None DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 23 @A300 SERVICE BULLETIN Table 2, Config. 001 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair Compliance Time Condition Action Threshold (FH or FC whichever occurs first) Grace period Repetitive Interval (FH or FC whichever occurs first) No crack found Apply SUBTASK 540075-832-002 001 Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair None None 3700 FC /4200 FH Crack found Contact Airbus Before next flight None None NOTE (*): For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval, the inspection is to be accomplished within 2000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. Table 3, Config. 001 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold (FH or FC whichever occurs first) Grace period Repetitive Interval (FH or FC whichever occurs first) All Aircraft Apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 10400 FC /11700 FH from Service Bulletin No. A300-54-0081 accomplishment 1000 FC see NOTE (*) 500 FC see NOTE (**) None No crack found Apply SUBTASK 540075-832-003 001 Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 None None 3700 FC /4200 FH Crack found Contact Airbus Before next flight None None DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 24 @A300 SERVICE BULLETIN Table 3, Config. 001 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold (FH or FC whichever occurs first) Grace period Repetitive Interval (FH or FC whichever occurs first) NOTE (*): A300 aircraft with Service Bulletin No. A300-54-0081 applied with less than 20900 FC from Service Bulletin accomplishment: For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval, the inspection is to be accomplished within 1000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE (**): A300 aircraft with Service Bulletin No. A300-54-0081 applied with more than 20900 FC from Service Bulletin accomplishment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 500 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. **CONF 002 This Service Bulletin has been classified Mandatory by the issue of an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA). The AD must be used as the reference document for the mandated accomplishment timescale. Table 1, Config. 002 - Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold Grace period Repetitive Interval All Aircraft Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 5350 FC None None DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 25 @A300 SERVICE BULLETIN Table 1, Config. 002 - Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold Grace period Repetitive Interval Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 None None 4300 FC Or Apply Service Bulletin No. A300-54-0081 Before next flight None None No crack found and apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 Refer to table 3 Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 None None 4300 FC Or Apply Service Bulletin No. A300-54-0081 Before next flight None None Crack found but not confirmed with HFEC Inspection and apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 Refer to table 3 Apply TASK 540075-833-802 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy current inspection and apply TASK 540075-832-802 001 Inspection Post Repair Refer to table 2 Crack found >=20 mm (0.787 in.) Contact Airbus Before next flight None None NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 9 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 26 @A300 SERVICE BULLETIN NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. Table 2, Config. 002 - Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval Threshold (FC or FH whichever occurs first) All Aircraft Apply TASK 540075-832-802 001 Inspection Post Repair 11700 FC /16100 FH from repair embodiment 2000 FC see NOTE (*) None No crack found Apply SUBTASK 540075-832-002 001 Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair None None 3700 FC /5100 FH Crack found Contact Airbus Before next flight None None NOTE (*): For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval, the inspection is to be accomplished within 2,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. Table 3, Config. 002 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold (FH or FC whichever occurs first) Grace period Repetitive Interval (FH or FC whichever occurs first) All Aircraft Apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 10400 FC /14200 FH from Service Bulletin No. A300-54-0081 accomplishment 1000 FC see NOTE (*) 500 FC see NOTE (**) None DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 10 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 27 @A300 SERVICE BULLETIN Table 3, Config. 002 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold (FH or FC whichever occurs first) Grace period Repetitive Interval (FH or FC whichever occurs first) No crack found Apply SUBTASK 540075-832-003 001 Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 None None 3700 FC /5100 FH Crack found Contact Airbus Before next flight None None NOTE (*): A300 aircraft with Service Bulletin No. A300-54-0081 applied with less than 20900 FC from Service Bulletin accomplishment: For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval, the inspection is to be accomplished within 1000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE (**): A300 aircraft with Service Bulletin No. A300-54-0081 applied with more than 20900 FC from Service Bulletin accomplishment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 500 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. **CONF 003 This Service Bulletin has been classified Mandatory by the issue of an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA). The AD must be used as the reference document for the mandated accomplishment timescale. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 11 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 28 @A300 SERVICE BULLETIN Table 1, Config. 003 - Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold Grace period Repetitive Interval All Aircraft Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 5350 FC None None Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 None None 4300 FC Or Apply Service Bulletin No. A300-54-0081 Before next flight None None No crack found and apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 Refer to table 3 Apply TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 None None 4300 FC Or Apply Service Bulletin No. A300-54-0081 Before next flight None None Crack found but not confirmed with HFEC Inspection and apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 Refer to table 3 Apply TASK 540075-833-802 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy current inspection. and apply TASK 540075-832-802 001 Inspection Post Repair Refer to table 2 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 12 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 29 @A300 SERVICE BULLETIN Table 1, Config. 003 - Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold Grace period Repetitive Interval Crack found >=20 mm (0.787 in.) Contact Airbus Before next flight None None NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. Table 2, Config. 003 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR:11800 FC from repair embodiment All Aircraft Apply TASK 540075-832-802 001 Inspection Post Repair LR:11700 FC /26700 FH from repair embodiment 2000 FC see NOTE (*) None SR:4000 FC /5500 FH No crack found Apply SUBTASK 540075-832-002 001 Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair None None LR:3700 FC /8400 FH Crack found Contact Airbus Before next flight None None NOTE (*): For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval, the inspection is to be accomplished within 2000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE : For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to Airworthiness Limitations Section (ALS) Part 2. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 13 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 30 @A300 SERVICE BULLETIN Table 3, Config. 003 - Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 Compliance Time Condition Action Threshold (FH or FC whichever occurs first) Grace period Repetitive Interval (FH or FC whichever occurs first) SR:11200 FC /15400 FH from Service Bulletin No. A300-54-0081 accomplishment All Aircaft Apply TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 LR:10400 FC /23600 FH from Service Bulletin No. A300-54-0081 accomplishment 1000 FC see NOTE (*) 500 FC see NOTE (**) None SR:4000 FC /5500 FH No crack found Apply SUBTASK 540075-832-003 001 Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 None None LR:3700 FC /8400 FH Crack found Contact Airbus Before next flight None None NOTE (*): A300 aircraft with Service Bulletin No. A300-54-0081 applied with less than 20900 FC from Service Bulletin accomplishment: For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval, the inspection is to be accomplished within 1000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE (**): A300 aircraft with Service Bulletin No. A300-54-0081 applied with more than 20900 FC from Service Bulletin accomplishment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 500 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB (Rev. 02). NOTE : A300 B2 aircraft model concerns aircraft models A300 B2-203, A300 B2K-3C. NOTE : A300 B4-100 aircraft model concerns aircraft models A300 B4-2C. NOTE : A300 B4-200 aircraft model concerns aircraft models A300 B4-203, C4-203 and F4-203. NOTE : For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to Airworthiness Limitations Section (ALS) Part 2. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 14 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 31 @A300 SERVICE BULLETIN **CONF ALL 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 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FABAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FACAA given in Appendix 02 - Elapsed Time Assumption . DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 15 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 32 @A300 SERVICE BULLETIN NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 Get Access 6.00 On Aircraft Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FADAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-833-802-001: Repair Get Access 6.00 On Aircraft Repair 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FAEAA given in Appendix 02 - Elapsed Time Assumption . **CONF 002 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FABAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 16 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 33 @A300 SERVICE BULLETIN Task 540075-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FACAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 Get Access 6.00 On Aircraft Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FADAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-833-802-001: Repair Get Access 6.00 On Aircraft Repair 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FAEAA given in Appendix 02 - Elapsed Time Assumption . **CONF 003 Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 Get Access 6.00 On Aircraft DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 17 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 34 @A300 SERVICE BULLETIN Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FABAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FACAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081 Get Access 6.00 On Aircraft Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FADAA given in Appendix 02 - Elapsed Time Assumption . NOTE : The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. Task 540075-833-802-001: Repair Get Access 6.00 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 18 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 35 @A300 SERVICE BULLETIN Task 540075-833-802-001: Repair On Aircraft Repair 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FAEAA given in Appendix 02 - Elapsed Time Assumption . **CONF ALL H. WEIGHT AND BALANCE **CONF 001 thru 002 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07. For TASK 540075-833-802 001 Repair: Manufacturers Empty Weight +0.85 KG (+1.8739 LB) Effect on Balance +23.15 KGM (+167.44 LB.FT ) **CONF 003 Not Changed **CONF ALL I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-21-00 06-21-54 20-31-00 24-00-00 24-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 Non Destructive Test Manual (NTM) 51-31-11 51-40-00 54-40-03 Service Bulletin (SB) A300-54-0075 A300-54-0081 Standards Manual (SM) Structural Repair Manual (SRM) 51-40-00 54-10-00 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 19 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 36 @A300 SERVICE BULLETIN **CONF 002 Aircraft Maintenance Manual (AMM) 06-21-00 06-21-54 20-31-00 24-00-00 24-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 Non Destructive Test Manual (NTM) 51-31-11 51-40-00 54-40-03 Service Bulletin (SB) A300-54-0075 A300-54-0081 Standards Manual (SM) Structural Repair Manual (SRM) 51-40-00 54-10-00 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 003 Airworthiness Limitation Section (ALS) Airworthiness Limitations Section (ALS) Part 2 Aircraft Maintenance Manual (AMM) 06-21-00 06-21-54 20-31-00 24-00-00 24-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 Non Destructive Test Manual (NTM) 51-31-11 51-40-00 54-40-03 Service Bulletin (SB) A300-54-0075 A300-54-0081 Standards Manual (SM) Structural Repair Manual (SRM) 51-40-00 54-10-00 **CONF ALL K. PUBLICATION AFFECTED Maintenance Planning Document (MPD) 543002-0602-4 543002-0602-5 543002-0602-6 543002-0602-7 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 20 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 37 @A300 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 540075A01R02 AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 2590 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability Kit 540075A01R02 Cost 3,910.00 USD Availability 90 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. C. LIST OF COMPONENTS Kit 540075A01R02 ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES A5461255220000 1 Doubler A5461255220100 1 Doubler A5461255320000 8 Washer A5461255420000 6 Washer ASNA2314-4-13 6 Screw ASNA2314-6-14 4 Screw ASNA2314-6-16 8 Screw NAS1153E3 4 Screw DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 21 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 38 @A300 SERVICE BULLETIN ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim 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 Non Aqueous Cleaner-General 08BAA9 As required (2) Components None (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING (1) Tooling - Price and Availability To accomplish this Service Bulletin it is necessary to use the following tools and equipment : - For inspection program after accomplishment of the Service Bulletin No. A300-54-0081 , equipment and material for control by eddy current as per NTM 54-40-03 Part 6. - For inspection program during accomplishment of repair, equipment and material for control by eddy current as per NTM 51-31-11 Part 1. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 22 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 39 @A300 SERVICE BULLETIN (2) Tools None (3) Special Tools None DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 23 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 40 @A300 SERVICE BULLETIN This Page Intentionally Left Blank DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 24 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 41 @A300 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 540075-832-801-001 - Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 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 is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. NOTE : The purpose of flow charts is to supplement the information given in the Procedure and Compliance paragraphs and not to serve as the primary source for tasks or compliance times given in this Service Bulletin. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 25 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 42 @A300 SERVICE BULLETIN Task Associated Data **CONF 001 Zone From 410 to 420 Access Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER 423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF 002 Zone From 410 to 420 Access Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER 423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF 003 Zone From 410 to 420 Access Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER 423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 540075-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 26 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 43 @A300 SERVICE BULLETIN Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner- General 08BAA9 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the identification of zones, refer to AMM 06-21-00, Page Block 001. (b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001. (c) For the specification of material (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML) . (d) Clean the surfaces to seal with: Non Aqueous Cleaner-General 08BAA9 As required and refer to AMM 20-31-00, Page Block 001. (2) Subtask 540075-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF 002 (1) Subtask 540075-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner- General 08BAA9 As required DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 27 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 44 @A300 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the identification of zones, refer to AMM 06-21-00, Page Block 001. (b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001. (c) For the specification of material (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML) . (d) Clean the surfaces to seal with: Non Aqueous Cleaner-General 08BAA9 As required and refer to AMM 20-31-00, Page Block 001. (2) Subtask 540075-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF 003 (1) Subtask 540075-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner- General 08BAA9 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the identification of zones, refer to AMM 06-21-00, Page Block 001. (b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 28 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 45 @A300 SERVICE BULLETIN (c) For the specification of material (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML) . (d) Clean the surfaces to seal with: Non Aqueous Cleaner-General 08BAA9 As required and refer to AMM 20-31-00, Page Block 001. (2) Subtask 540075-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 540075-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 NOTE : The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic system s depressurized - Access to the cockpit and cabin is available - All circuit breakers are in closed position DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 29 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 46 @A300 SERVICE BULLETIN - All controls in NORM, AUTO or OFF position (a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page Block 301. (b) De-energize the aircraft electrical circuits, refer to AMM 24-41-00, Page Block 301. (c) Put an access platform in position at zones 410 and 420. (d) Remove the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and 413EL, refer to AMM 06-21-54, Page Block 001. (e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and 414EL, refer to AMM 06-21-54, Page Block 001. (f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and 423EL, refer to AMM 06-21-54, Page Block 001. (g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and 424EL, refer to AMM 06-21-54, Page Block 001. **CONF 002 (1) Subtask 540075-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 NOTE : The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic system s depressurized - Access to the cockpit and cabin is available - All circuit breakers are in closed position DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 30 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 47 @A300 SERVICE BULLETIN - All controls in NORM, AUTO or OFF position (a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page Block 301. (b) De-energize the aircraft electrical circuits, refer to AMM 24-41-00, Page Block 301. (c) Put an access platform in position at zones 410 and 420. (d) Remove the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and 413EL, refer to AMM 06-21-54, Page Block 001. (e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and 414EL, refer to AMM 06-21-54, Page Block 001. (f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and 423EL, refer to AMM 06-21-54, Page Block 001. (g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and 424EL, refer to AMM 06-21-54, Page Block 001. **CONF 003 (1) Subtask 540075-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 NOTE : The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic system s depressurized - Access to the cockpit and cabin is available - All circuit breakers are in closed position DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 31 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 48 @A300 SERVICE BULLETIN - All controls in NORM, AUTO or OFF position (a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page Block 301. (b) De-energize the aircraft electrical circuits, refer to AMM 24-41-00, Page Block 301. (c) Put an access platform in position at zones 410 and 420. (d) Remove the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and 413EL, refer to AMM 06-21-54, Page Block 001. (e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and 414EL, refer to AMM 06-21-54, Page Block 001. (f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and 423EL, refer to AMM 06-21-54, Page Block 001. (g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and 424EL, refer to AMM 06-21-54, Page Block 001. **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 540075-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413EL , Panel 413DL, Panel 414DR or 414ER , Panel 414CR or 414EL Work location Rib 8 To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel 424DR or 424ER, Panel 424CR or 424EL Work location Rib 8 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-31-11 51-40-00 Part 1 Service Bulletin (SB) A300-54-0081 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 32 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 49 @A300 SERVICE BULLETIN References Fig. A-FBAAA Inspection Area: Pre Repair and Pre Service Bulletin No. A300-54-0081 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FRAAA Inspection Report Sheet 01 Sheet 02 At the threshold given in PLA NNING INFORMATION paragraph E.(2) (a) Do a detailed inspection, refer to NTM 51-40-00 Part 1 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01 1 If no crack is found: a Re-inspect the area as described in TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the interval given in PLANNING INFORMATION Paragraph E.(2). or b Accomplish Service Bulletin No. A300-54-0081 and Do a Special Detailed Inspection as described in TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack length with High Frequency Eddy Current (HFEC) Inspection, refer to NTM 51-31-11. a If crack is not confirmed: <1> Re-inspect the area as described in TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the interval given in PLANNING INFORMATION Paragraph E.(2). or <2> Accomplish Service Bulletin No. A300-54-0081 and Do a Special Detailed Inspection as described in TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold given in PLANNING INFORMATION Paragraph E.(2). DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 33 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 50 @A300 SERVICE BULLETIN b If crack < 20 mm (0.787 in.): <1> Do the repair before 1000 fli ghts cycles, in accordance with TASK 540075-833-802 001 Repair and Do a Special Detailed Inspection the area as described in TASK 540075-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). c If crack >=20 mm (0.787 in.): <1> Contact Airbus before next flight. (b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA . **CONF 002 (1) Subtask 540075-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413EL , Panel 413DL, Panel 414DR or 414ER , Panel 414CR or 414EL Work location Rib 8 To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel 424DR or 424ER, Panel 424CR or 424EL Work location Rib 8 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-31-11 51-40-00 Part 1 Service Bulletin (SB) A300-54-0081 Fig. A-FBAAA Inspection Area: Pre Repair and Pre Service Bulletin No. A300-54-0081 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FRAAA Inspection Report Sheet 01 Sheet 02 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 34 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 51 @A300 SERVICE BULLETIN At the threshold given in PLA NNING INFORMATION paragraph E.(2) (a) Do a detailed inspection, refer to NTM 51-40-00 Part 1 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01 1 If no crack is found: a Re-inspect the area as described in TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the interval given in PLANNING INFORMATION Paragraph E.(2). or b Accomplish Service Bulletin No. A300-54-0081 and Do a Special Detailed Inspection as described in TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack length with High Frequency Eddy Current (HFEC) Inspection, refer to NTM 51-31-11. a If crack is not confirmed: <1> Re-inspect the area as described in TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the interval given in PLANNING INFORMATION Paragraph E.(2). or <2> Accomplish Service Bulletin No. A300-54-0081 and Do a Special Detailed Inspection as described in TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold given in PLANNING INFORMATION Paragraph E.(2). b If crack < 20 mm (0.787 in.): <1> Do the repair before 1000 fli ghts cycles, in accordance with TASK 540075-833-802 001 Repair and DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 35 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 52 @A300 SERVICE BULLETIN Do a Special Detailed Inspection the area as described in TASK 540075-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). c If crack >=20 mm (0.787 in.): <1> Contact Airbus before next flight. (b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA . **CONF 003 (1) Subtask 540075-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair and pre Service Bulletin No. A300-54-0081 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413EL , Panel 413DL, Panel 414DR or 414ER , Panel 414CR or 414EL Work location Rib 8 To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel 424DR or 424ER, Panel 424CR or 424EL Work location Rib 8 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-31-11 51-40-00 Part 1 Service Bulletin (SB) A300-54-0081 Fig. A-FBAAA Inspection Area: Pre Repair and Pre Service Bulletin No. A300-54-0081 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FRAAA Inspection Report Sheet 01 Sheet 02 At the threshold given in PLA NNING INFORMATION paragraph E.(2) (a) Do a detailed inspection, refer to NTM 51-40-00 Part 1 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01 DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 36 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 53 @A300 SERVICE BULLETIN 1 If no crack is found: a Re-inspect the area as described in TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the interval given in PLANNING INFORMATION Paragraph E.(2). or b Accomplish Service Bulletin No. A300-54-0081 and Do a Special Detailed Inspection as described in TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack length with High Frequency Eddy Current (HFEC) Inspection, refer to NTM 51-31-11. a If crack is not confirmed: <1> Re-inspect the area as described in TASK 540075-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the interval given in PLANNING INFORMATION Paragraph E.(2). or <2> Accomplish Service Bulletin No. A300-54-0081 and Do a Special Detailed Inspection as described in TASK 540075-832-803 001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold given in PLANNING INFORMATION Paragraph E.(2). b If crack < 20 mm (0.787 in.): <1> Do the repair before 1000 fli ghts cycles, in accordance with TASK 540075-833-802 001 Repair and Do a Special Detailed Inspection the area as described in TASK 540075-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). c If crack >=20 mm (0.787 in.): <1> Contact Airbus before next flight. (b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA . DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 37 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 54 @A300 SERVICE BULLETIN **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF 003 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 540075-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and 413EL, refer to AMM 06-21-54, Page Block 001. (c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and 414EL, refer to AMM 06-21-54, Page Block 001. (d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and 423EL, refer to AMM 06-21-54, Page Block 001. (e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and 424EL, refer to AMM 06-21-54, Page Block 001. (f) Remove the access platforms. (g) Put the aircraft back to its initial configuration. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 38 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 55 @A300 SERVICE BULLETIN **CONF 002 (1) Subtask 540075-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and 413EL, refer to AMM 06-21-54, Page Block 001. (c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and 414EL, refer to AMM 06-21-54, Page Block 001. (d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and 423EL, refer to AMM 06-21-54, Page Block 001. (e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and 424EL, refer to AMM 06-21-54, Page Block 001. (f) Remove the access platforms. (g) Put the aircraft back to its initial configuration. **CONF 003 (1) Subtask 540075-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and 413EL, refer to AMM 06-21-54, Page Block 001. (c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and 414EL, refer to AMM 06-21-54, Page Block 001. (d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and 423EL, refer to AMM 06-21-54, Page Block 001. (e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and 424EL, refer to AMM 06-21-54, Page Block 001. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 39 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 56 @A300 SERVICE BULLETIN (f) Remove the access platforms. (g) Put the aircraft back to its initial configuration. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 40 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 57 @A300 SERVICE BULLETIN Task 540075-832-802-001 - Inspection Post Repair **CONF ALL 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 is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. NOTE : The purpose of flow charts is to supplement the information given in the Procedure and Compliance paragraphs and not to serve as the primary source for tasks or compliance times given in this Service Bulletin. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 41 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 58 @A300 SERVICE BULLETIN Task Associated Data **CONF 001 Zone From 410 to 420 Access Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER 423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 002 Zone From 410 to 420 Access Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER 423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 003 Zone From 410 to 420 Access Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER 423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 540075-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 42 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 59 @A300 SERVICE BULLETIN Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner- General 08BAA9 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the identification of zones, efer to AMM 06-21-00, Page Block 001. (b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001. (c) For the specification of material (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML) . (d) Clean the surfaces to seal with: Non Aqueous Cleaner-General 08BAA9 As required and refer to AMM 20-31-00, Page Block 001. (2) Subtask 540075-839-002-001 - 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 540075-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner- General 08BAA9 As required DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 43 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 60 @A300 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the identification of zones, efer to AMM 06-21-00, Page Block 001. (b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001. (c) For the specification of material (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML) . (d) Clean the surfaces to seal with: Non Aqueous Cleaner-General 08BAA9 As required and refer to AMM 20-31-00, Page Block 001. (2) Subtask 540075-839-002-001 - 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 540075-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner- General 08BAA9 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the identification of zones, efer to AMM 06-21-00, Page Block 001. (b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001. DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075 REVISION No.: 04 - May 26/15 Page: 44 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. The text continues at https://openairdocs.org/service-documents/airbus/a300-54-0075/file/5c1f062c3140.md?from=61 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.