# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 54 

### TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. MODIFICATION No.: None This page transmits Revision No.03 of Service Bulletin No.A310-54-2018 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASONRevision No. 03 issued to update the threshold and intervals as per analysis improvement and inservice crack findings consistency. CHANGES SUMMARY MODIFICATIONS Minor editorial or document structure change N REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Minor editorial or document structure change N GENERAL EVALUATION Minor editorial or document structure change N MATERIAL PRICE INFORMATION Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N EFFECTIVITY Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REFERENCES / REPERCUSSIONS Minor editorial or document structure change N NATURE OF THE WORK Minor editorial or document structure change N DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
MANPOWER Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N APPENDICES Minor editorial or document structure change N Fig. A-FSAAA Minor editorial or document structure change N Fig. A-FSAAA Sheet 01 Minor editorial or document structure change N Fig. A-FSBAA Minor editorial or document structure change N Fig. A-FSBAA Sheet 01 Minor editorial or document structure change N Fig. A-FSCAA Minor editorial or document structure change N Fig. A-FSCAA Sheet 01 Minor editorial or document structure change N PLANNING INFORMATION EFFECTIVITY Minor editorial or document structure change N Configuration definition Minor editorial or document structure change N CONF 001 Minor editorial or document structure change N CONF 002 Minor editorial or document structure change N CONF 003 Minor editorial or document structure change N CONF 004 Minor editorial or document structure change N CONF 005 Minor editorial or document structure change N CONF 006 Minor editorial or document structure change N CONF 007 Minor editorial or document structure change N Material Effectivity Minor editorial or document structure change N Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REASON Minor editorial or document structure change N History Minor editorial or document structure change N Objective/Action Minor editorial or document structure change N Advantages Minor editorial or document structure change N Operational/Maintenance Consequences Minor editorial or document structure change N DESCRIPTION Minor editorial or document structure change N COMPLIANCE Minor editorial or document structure change N Classification Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Accomplishment Timescale Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N APPROVAL Minor editorial or document structure change N Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N WEIGHT AND BALANCE Minor editorial or document structure change N Minor editorial or document structure change N ELECTRICAL LOAD DATA Minor editorial or document structure change N REFERENCES Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N PUBLICATION AFFECTED Minor editorial or document structure change N Minor editorial or document structure change N INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N SPARES Minor editorial or document structure change N MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N Procurement Addresses Minor editorial or document structure change N Price and Availability Minor editorial or document structure change N INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N LIST OF COMPONENTS Minor editorial or document structure change N Kit 542018A01R03 Minor editorial or document structure change N LIST OF MATERIALS - OPERATOR SUPPLIED Minor editorial or document structure change N Consumable Materials Minor editorial or document structure change N Consumable CMLA01 Minor editorial or document structure change N Components Minor editorial or document structure change N Equipment Minor editorial or document structure change N

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
PARTS TO BE RE-IDENTIFIED BY OPERATOR Minor editorial or document structure change N TOOLING Minor editorial or document structure change N Tooling - Price and Availability Minor editorial or document structure change N Tools Minor editorial or document structure change N Special Tools Minor editorial or document structure change N ACCOMPLISHMENT INSTRUCTIONS TASK 542018- 832-801-001-Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Minor editorial or document structure change N
Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Subtask 542018-910-005-001 Minor editorial or document structure change N Subtask 542018-900-002-001 Minor editorial or document structure change N Subtask 542018-910-005-001 Minor editorial or document structure change N Subtask 542018-900-002-001 Minor editorial or document structure change N Subtask 542018-910-005-001 Minor editorial or document structure change N Subtask 542018-900-002-001 Minor editorial or document structure change N Subtask 542018-910-005-001 Minor editorial or document structure change N Subtask 542018-900-002-001 Minor editorial or document structure change N Subtask 542018-910-005-001 Minor editorial or document structure change N Subtask 542018-900-002-001 Minor editorial or document structure change N Subtask 542018-910-005-001 Minor editorial or document structure change N Subtask 542018-900-002-001 Minor editorial or document structure change N Subtask 542018-910-005-001 Minor editorial or document structure change N Subtask 542018-900-002-001 Minor editorial or document structure change N Subtask 542018-941-003-001 Minor editorial or document structure change N Subtask 542018-941-003-001 Minor editorial or document structure change N Subtask 542018-941-003-001 Minor editorial or document structure change N Subtask 542018-941-003-001 Minor editorial or document structure change N Subtask 542018-941-003-001 Minor editorial or document structure change N Subtask 542018-941-003-001 Minor editorial or document structure change N Subtask 542018-941-003-001 Minor editorial or document structure change N Subtask 542018-832-002-001 Minor editorial or document structure change N Subtask 542018-832-002-001 Minor editorial or document structure change N Subtask 542018-832-002-001 Minor editorial or document structure change N Subtask 542018-832-002-001 Minor editorial or document structure change N DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 542018-832-002-001 Minor editorial or document structure change N Subtask 542018-832-002-001 Minor editorial or document structure change N Subtask 542018-832-002-001 Minor editorial or document structure change N Subtask 542018-942-004-001 Minor editorial or document structure change N Subtask 542018-942-004-001 Minor editorial or document structure change N Subtask 542018-942-004-001 Minor editorial or document structure change N Subtask 542018-942-004-001 Minor editorial or document structure change N Subtask 542018-942-004-001 Minor editorial or document structure change N Subtask 542018-942-004-001 Minor editorial or document structure change N Subtask 542018-942-004-001 Minor editorial or document structure change N TASK 542018- 832-802-001-Inspection Post Repair Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Subtask 542018-910-001-001 Minor editorial or document structure change N Subtask 542018-839-001-001 Minor editorial or document structure change N Subtask 542018-910-001-001 Minor editorial or document structure change N Subtask 542018-839-001-001 Minor editorial or document structure change N Subtask 542018-910-001-001 Minor editorial or document structure change N Subtask 542018-839-001-001 Minor editorial or document structure change N Subtask 542018-910-001-001 Minor editorial or document structure change N Subtask 542018-839-001-001 Minor editorial or document structure change N Subtask 542018-910-001-001 Minor editorial or document structure change N Subtask 542018-839-001-001 Minor editorial or document structure change N Subtask 542018-910-001-001 Minor editorial or document structure change N Subtask 542018-839-001-001 Minor editorial or document structure change N Subtask 542018-910-001-001 Minor editorial or document structure change N Subtask 542018-839-001-001 Minor editorial or document structure change N Subtask 542018-941-004-001 Minor editorial or document structure change N Subtask 542018-941-004-001 Minor editorial or document structure change N Subtask 542018-941-004-001 Minor editorial or document structure change N Subtask 542018-941-004-001 Minor editorial or document structure change N Subtask 542018-941-004-001 Minor editorial or document structure change N Subtask 542018-941-004-001 Minor editorial or document structure change N Subtask 542018-941-004-001 Minor editorial or document structure change N Subtask 542018-832-005-001 Minor editorial or document structure change N DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 5 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 542018-832-005-001 Minor editorial or document structure change N Subtask 542018-832-005-001 Minor editorial or document structure change N Subtask 542018-832-005-001 Minor editorial or document structure change N Subtask 542018-832-005-001 Minor editorial or document structure change N Subtask 542018-832-005-001 Minor editorial or document structure change N Subtask 542018-832-005-001 Minor editorial or document structure change N Subtask 542018-942-005-001 Minor editorial or document structure change N Subtask 542018-942-005-001 Minor editorial or document structure change N Subtask 542018-942-005-001 Minor editorial or document structure change N Subtask 542018-942-005-001 Minor editorial or document structure change N Subtask 542018-942-005-001 Minor editorial or document structure change N Subtask 542018-942-005-001 Minor editorial or document structure change N Subtask 542018-942-005-001 Minor editorial or document structure change N TASK 542018- 832-803-001-Inspection Post Service Bulletin No. A310-54-2024 Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Subtask 542018-910-003-001 Minor editorial or document structure change N Subtask 542018-839-002-001 Minor editorial or document structure change N Subtask 542018-910-003-001 Minor editorial or document structure change N Subtask 542018-839-002-001 Minor editorial or document structure change N Subtask 542018-910-003-001 Minor editorial or document structure change N Subtask 542018-839-002-001 Minor editorial or document structure change N Subtask 542018-910-003-001 Minor editorial or document structure change N Subtask 542018-839-002-001 Minor editorial or document structure change N Subtask 542018-910-003-001 Minor editorial or document structure change N Subtask 542018-839-002-001 Minor editorial or document structure change N Subtask 542018-910-003-001 Minor editorial or document structure change N Subtask 542018-839-002-001 Minor editorial or document structure change N Subtask 542018-910-003-001 Minor editorial or document structure change N Subtask 542018-839-002-001 Minor editorial or document structure change N Subtask 542018-941-001-001 Minor editorial or document structure change N Subtask 542018-941-001-001 Minor editorial or document structure change N Subtask 542018-941-001-001 Minor editorial or document structure change N Subtask 542018-941-001-001 Minor editorial or document structure change N Subtask 542018-941-001-001 Minor editorial or document structure change N DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 6 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 542018-941-001-001 Minor editorial or document structure change N Subtask 542018-941-001-001 Minor editorial or document structure change N Subtask 542018-832-004-001 Minor editorial or document structure change N Subtask 542018-832-004-001 Minor editorial or document structure change N Subtask 542018-832-004-001 Minor editorial or document structure change N Subtask 542018-832-004-001 Minor editorial or document structure change N Subtask 542018-832-004-001 Minor editorial or document structure change N Subtask 542018-832-004-001 Minor editorial or document structure change N Subtask 542018-832-004-001 Minor editorial or document structure change N Subtask 542018-942-002-001 Minor editorial or document structure change N Subtask 542018-942-002-001 Minor editorial or document structure change N Subtask 542018-942-002-001 Minor editorial or document structure change N Subtask 542018-942-002-001 Minor editorial or document structure change N Subtask 542018-942-002-001 Minor editorial or document structure change N Subtask 542018-942-002-001 Minor editorial or document structure change N Subtask 542018-942-002-001 Minor editorial or document structure change N TASK 542018- 833-803-001-Repair Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Subtask 542018-910-004-001 Minor editorial or document structure change N Subtask 542018-839-003-001 Minor editorial or document structure change N Subtask 542018-910-004-001 Minor editorial or document structure change N Subtask 542018-839-003-001 Minor editorial or document structure change N Subtask 542018-910-004-001 Minor editorial or document structure change N Subtask 542018-839-003-001 Minor editorial or document structure change N Subtask 542018-910-004-001 Minor editorial or document structure change N Subtask 542018-839-003-001 Minor editorial or document structure change N Subtask 542018-910-004-001 Minor editorial or document structure change N Subtask 542018-839-003-001 Minor editorial or document structure change N Subtask 542018-910-004-001 Minor editorial or document structure change N Subtask 542018-839-003-001 Minor editorial or document structure change N Subtask 542018-910-004-001 Minor editorial or document structure change N Subtask 542018-839-003-001 Minor editorial or document structure change N Subtask 542018-941-002-001 Minor editorial or document structure change N Subtask 542018-941-002-001 Minor editorial or document structure change N Subtask 542018-941-002-001 Minor editorial or document structure change N DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 7 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 542018-941-002-001 Minor editorial or document structure change N Subtask 542018-941-002-001 Minor editorial or document structure change N Subtask 542018-941-002-001 Minor editorial or document structure change N Subtask 542018-941-002-001 Minor editorial or document structure change N Subtask 542018-833-016-001 Minor editorial or document structure change N Subtask 542018-833-016-001 Minor editorial or document structure change N Subtask 542018-833-016-001 Minor editorial or document structure change N Subtask 542018-833-016-001 Minor editorial or document structure change N Subtask 542018-833-016-001 Minor editorial or document structure change N Subtask 542018-833-016-001 Minor editorial or document structure change N Subtask 542018-833-016-001 Minor editorial or document structure change N Subtask 542018-942-003-001 Minor editorial or document structure change N Subtask 542018-942-003-001 Minor editorial or document structure change N Subtask 542018-942-003-001 Minor editorial or document structure change N Subtask 542018-942-003-001 Minor editorial or document structure change N Subtask 542018-942-003-001 Minor editorial or document structure change N Subtask 542018-942-003-001 Minor editorial or document structure change N Subtask 542018-942-003-001 Minor editorial or document structure change N Fig. A-FBAAA Minor editorial or document structure change N Fig. A-FBAAA Sheet 01 Minor editorial or document structure change N Fig. A-FBBAA Minor editorial or document structure change N Fig. A-FBBAA Sheet 01 Minor editorial or document structure change N Fig. A-FBCAA Minor editorial or document structure change N Fig. A-FBCAA Sheet 01 Minor editorial or document structure change N Fig. A-FFAAA Minor editorial or document structure change N Fig. A-FFAAA Sheet 01 Minor editorial or document structure change N Appendix 01: Inspection Report Pre repair and Pre Service Bulletin No. A310-54-2024 APPENDIX CONTENT Minor editorial or document structure change N Fig. A-FRAAA Minor editorial or document structure change N Fig. A-FRAAA Sheet 01 Minor editorial or document structure change N Fig. A-FRAAA Sheet 02 Minor editorial or document structure change N Appendix 02: Inspection Report Post repair APPENDIX CONTENT Minor editorial or document structure change N Fig. A-FRBAA Minor editorial or document structure change N Fig. A-FRBAA Sheet 01 Minor editorial or document structure change N Fig. A-FRBAA Sheet 02 Minor editorial or document structure change N Appendix 03: Inspection Report Post Service Bulletin No. A310-54-2024 APPENDIX CONTENT Minor editorial or document structure change N Fig. A-FRCAA Minor editorial or document structure change N Fig. A-FRCAA Sheet 01 Minor editorial or document structure change N
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 8 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-FRCAA Sheet 02 Minor editorial or document structure change N Appendix 04: Non Destructive Testing Procedure APPENDIX CONTENT Minor editorial or document structure change N Fig. A-FAAAA Minor editorial or document structure change N Fig. A-FAAAA Sheet 01 Minor editorial or document structure change N Fig. A-FAAAA Sheet 02 Minor editorial or document structure change N Fig. A-FAAAA Sheet 03 Minor editorial or document structure change N Fig. A-FAAAA Sheet 04 Minor editorial or document structure change N Fig. A-FAAAA Sheet 05 Minor editorial or document structure change N Fig. A-FAAAA Sheet 06 Minor editorial or document structure change N Fig. A-FAAAA Sheet 07 Minor editorial or document structure change N Fig. A-FAAAA Sheet 08 Minor editorial or document structure change N Fig. A-FAAAA Sheet 09 Minor editorial or document structure change N Fig. A-FAAAA Sheet 10 Minor editorial or document structure change N Fig. A-FAAAA Sheet 11 Minor editorial or document structure change N Appendix 05: Elapsed Time Assumption APPENDIX CONTENT Minor editorial or document structure change N Fig. A-FABAA Minor editorial or document structure change N Fig. A-FABAA Sheet 01 Minor editorial or document structure change N Fig. A-FACAA Minor editorial or document structure change N Fig. A-FACAA Sheet 01 Minor editorial or document structure change N Fig. A-FADAA Minor editorial or document structure change N Fig. A-FADAA Sheet 01 Minor editorial or document structure change N Fig. A-FAEAA Minor editorial or document structure change N Fig. A-FAEAA Sheet 01 Minor editorial or document structure change N FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 issued to 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 and replace R54610124 by SRM 54-51-31. REVISION SEQUENCE ORIGINAL: Aug 11/93 REVISION No. : 01 - Nov 16/07 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 9 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET REVISION No. : 02 - Jun 26/08 REVISION No. : 03 - Apr 11/13

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 10 5

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# @A310 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 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 and Eddy Current inspection of pylon side panels (upper section) at Rib 8, 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. This Service Bulletin is revised in the frame of the A310 extended service goal study. 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.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 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 542018A01R03 1 3,960.00 Doubler **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 542018A01R03 1 3,960.00 Doubler **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 542018A01R03 1 3,960.00 Doubler **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 542018A01R03 1 3,960.00 Doubler **CONF 005 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 542018A01R03 1 3,960.00 Doubler **CONF 006 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 542018A01R03 1 3,960.00 Doubler

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN SUMMARY **CONF 007 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 542018A01R03 1 3,960.00 Doubler EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

18T 19U 52X 58X 82Z 83V 85W 85Z 99Y AFG AIB AIC BAF BBC C9L CFC DGA F2I FDX G2X G8E GAF HFY HJI IRA IRM IYE JAV K1P KAC KZU MGL PCA PIA QAF R1T RJA ROT RZO SBI SGX SUD THY TSC UBD UZB WHT CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU 54.51.31.001 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 OBRM NO MANPOWER **CONF 001 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN SUMMARY Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 002 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 003 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN SUMMARY **CONF 004 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 005 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 006 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 5 5

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# @A310 SERVICE BULLETIN SUMMARY Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 007 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 APPENDICES **CONF ALL Appendix 01: Inspection Report Pre repair and Pre Service Bulletin No. A310-54-2024 Appendix 02: Inspection Report Post repair Appendix 03: Inspection Report Post Service Bulletin No. A310-54-2024 Appendix 04: Non Destructive Testing Procedure Appendix 05: Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 6 5

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

AREAS TO BE INSPECTED

RIB8 

## B **FWD** PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON 

### B **B**



## A RIB8

**NOTES:** RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION 

### A **A**

B_SB_542018_5_SAAA_01_00 Figure A-FSAAA - Sheet 01 Pre Repair and Pre SB No.A310-54-2024 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 7 5

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

DETAILED INSPECTION AREA RIB8 

## B **FWD** 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

B_SB_542018_5_SBAA_01_01 Figure A-FSBAA - Sheet 01 Post Repair DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 8 5

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

DETAILED INSPECTION AREA RIB8 

## B **FWD** 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 B_SB_542018_5_SCAA_01_00 Figure A-FSCAA - Sheet 01 Post SB No.A310-54-2024 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 9 5

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# @A310 SERVICE BULLETIN SUMMARY

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 10 5

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# @A310 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 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 above on which Mod. Mo. 02434S3600 (NEW ENGINE PYLON - COMMON PARTS) is embodied or Mod. No. 04799D9249 (REFERENCE MODIFICATION FOR ST5 (SN.293)) is embodied on one or both pylons. NOTE: The modification No. 10432S20461 (NACELLES/PYLONS - PANELS IN THE UPPER CORNER AT RIB 8 - ADD A DOUBLER (PRODUCTION SOLUTION)) is embodied prior to delivery on aircraft MSN 0693 and subsequent. NOTE: Aircraft with modification No. 10432S20461 (NACELLES/PYLONS - PANELS IN THE UPPER CORNER AT RIB 8 - ADD A DOUBLER (PRODUCTION SOLUTION)) is embodied are not affected by this inspection. (1) Models 310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324 310-325

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN (2) Effectivity by MSN 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303 0313 0316 0318 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0389-0390 0392 0394 0397 0399-0400 0406-0407 0410 0413 0418-0419 0421-0422 0425 0427-0429 0431 0434 0436-0437 0439 0441 0444-0449 0452 0454 0456-0458 0467 0472-0473 0475-0476 0478 0480-0485 0488-0492 0494-0500 0502-0503 0519-0520 0522-0524 0526-0527 0534 0537-0539 0541-0542 0544-0545 0547 0549-0552 0562 0564-0565 0567-0568 0571 0573-0574 0576 0585-0588 0590-0595 0597 0599-0600 0620 0622 0624 0636 0638 0644 0646-0649 0651-0654 0656 0658 0660-0661 0663 0667 0669 0671-0672 0674 0676 0678 0682 0684 0686-0687 0689 0691 (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 18T 0473 19U 0399 52X 0410 58X 0431 82Z 0550 0551 83V 0427 0428 85W 0684 85Z 0547 99Y 0489 AFG 0496 0497 AIB 0686 AIC 0392 0406 0407 0429 0538 0544 0654 0669 BAF 0367 0372 BBC 0594 C9L 0652 CFC 0425 0441 0444 0446 0482 DGA 0418 0421 0422 F2I 0448 FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303 0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346 0353 0355 0356 0359 0360 0362 0364 0369 0378 0394 0397 0400 0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539 0542 0549 0552 0593 0638 G2X 0573 G8E 0475 GAF 0434 0484 0498 0503 0522 0523 HFY 0495 0565 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN

OPERATOR MSN HJI 0413 IRA 0338 0370 0375 0379 0389 0390 0436 0671 IRM 0488 0499 0524 0537 0564 0567 0586 0595 0620 IYE 0568 JAV 0357 0481 K1P 0648 KAC 0647 0649 0663 KZU 0592 0622 0646 MGL 0526 PCA 0419 PIA 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689 0691 QAF 0667 R1T 0591 RJA 0445 0490 0491 ROT 0636 0644 RZO 0571 0624 0651 0661 SBI 0520 SGX 0519 0562 SUD 0437 THY 0476 0478 0480 0502 TSC 0447 0472 0483 0485 0527 0541 0545 0588 0597 0599 0600 0658 UBD 0672 0674 UZB 0574 0576 WHT 0494 (4) Configuration by MSN MSN CONFIGURATION 0162 0217 0224 0251 0260 0267 0278 0288 0303 0313 0318 0331 0333 0339 0342 0343 0345 0346 0357 0367 0372 0419 003 0191 0201 0230 0233 0237 0241 0245 0248 0254 0257 0264 0273 0281 0283 0297 0316 0326 0335 0338 0353 0355 0356 0359 0360 0362 0364 0369 0370 0375 0379 0389 0390 0394 0397 0400 0454 001

0378 0439 0449 0452 0456 0457 0458 0467 0489 0492 0500 0534 0539 0542 0549 0568 0574 0576 0591 0594 0624 0636 0638 0644 0654 0660 0669 0672 0674 0676 0678 0682 0684 0686 0687 0689 005

0392 0406 0407 0413 0421 0422 0428 0429 0431 0434 0436 006 0399 0410 0437 004 0418 0425 0441 0444 0445 0446 0447 0448 0472 0473 0475 0476 0478 0480 0481 0482 0483 0484 0485 0488 0490 0491 0494 0495 0496 0497 0498 0499 0502 0503 0519 0520 0522 0523 0524 0526 0527 0537 0538 0541 0544 0545 0547 0550 0551 0552 0562 0564 0565 0567 0571 0573 0585 0586 0587 0588 0590 0592 0593 0595 0597 0599 0600 0620 0622 0646 0647 0648 0649 0651 0652 0653 0656 0658 0661 0663 0667 0671 0691 007

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN

MSN CONFIGURATION 0427 002 (5) Configuration definition **CONF 001 Config. 001 is valid for aircraft model A310-200 equipped with GENERAL ELECTRIC CF6-80A3 engines. **CONF 002 Config. 002 is valid for aircraft model A310-200 equipped with GENERAL ELECTRIC CF6-80C2 engines. **CONF 003 Config. 003 is valid for aircraft model A310-200 equipped with PRATT and WHITNEY engines. **CONF 004 Config. 004 is valid for aircraft model A310-300 equipped with PRATT and WHITNEY JT9D engines. **CONF 005 Config. 005 is valid for aircraft model A310-300 equipped with PRATT and WHITNEY 4000 engines. **CONF 006 Config. 006 is valid for aircraft model A310-300 equipped with GENERAL ELECTRIC engines and without embodiment of Mod. No. 6080S6778. **CONF 007 Config. 007 is valid for aircraft model A310-300 equipped with GENERAL ELECTRIC engines and with embodiment of Mod. No. 6080S6778. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Kit 542018A01R03 1 Consumable CMLA01 1 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.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN (2) Objective/Action This Service Bulletin requires a detailed and Eddy Current inspection of pylon side panels (upper section) at Rib 8, 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. This Service Bulletin is revised in the frame of the A310 extended service goal study. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Task 542018-832-802-001: Inspection Post Repair (1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Task 542018-833-803-001: Repair (1) Repair the Side Panel of the Pylon **CONF 002 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Task 542018-832-802-001: Inspection Post Repair (1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 5 5

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# @A310 SERVICE BULLETIN Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Task 542018-833-803-001: Repair (1) Repair the Side Panel of the Pylon **CONF 003 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Task 542018-832-802-001: Inspection Post Repair (1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Task 542018-833-803-001: Repair (1) Repair the Side Panel of the Pylon **CONF 004 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Task 542018-832-802-001: Inspection Post Repair (1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Task 542018-833-803-001: Repair (1) Repair the Side Panel of the Pylon

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 6 5

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# @A310 SERVICE BULLETIN
**CONF 005 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Task 542018-832-802-001: Inspection Post Repair (1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Task 542018-833-803-001: Repair (1) Repair the Side Panel of the Pylon **CONF 006 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Task 542018-832-802-001: Inspection Post Repair (1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Task 542018-833-803-001: Repair (1) Repair the Side Panel of the Pylon **CONF 007 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Task 542018-832-802-001: Inspection Post Repair (1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 7 5

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# @A310 SERVICE BULLETIN Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 (1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Task 542018-833-803-001: Repair (1) Repair the Side Panel of the Pylon **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale **CONF 001 This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Config. 001 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 9,700 FC /19,400 FH None None Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None 6,700 FC /13,400 FH Or Apply SB A310-54-2024 Before next flight None None No crack found

and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 8 5

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# @A310 SERVICE BULLETIN
Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None 6,700 FC /13,400 FH Or Apply SB A310-54-2024 Before next flight None None Crack found but not confirmed with HFEC inspection and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3 Apply TASK 542018-833-803 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection and apply TASK 542018-832-802 001 Inspection Post Repair Refer to table 2

Crack found >=20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection Contact Airbus Before next flight None None

NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 9 5

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# @A310 SERVICE BULLETIN
Table 2: 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) Config. 001 Apply TASK 542018-832-802 001 Inspection Post Repair 11,200 FC /22,500 FH from repair embodiment 2,000 FC See NOTE (*) None

No crack found Apply TASK 542018-832-802 001 Inspection Post Repair None None 3,500 FC /7,100 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 sheduled 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Config .001 Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 9,900 FC/ 19,800 FH from SB A310-54- 2024 embodiment 1,000 FC see NOTE (*) 500 FC see NOTE (**) None

No crack found Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 None None 3,500 FC /7,100 FH Crack found Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 10 5

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# @A310 SERVICE BULLETIN
Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE (**): For A310-200 post SB 54-0024 with more than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with more than 13,900 FC from embodiment: 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. **CONF 002 This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Config. 002 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 7,800 FC /15,600 FH None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 11 5

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# @A310 SERVICE BULLETIN
Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None 5,800 FC /11,600 FH Or Apply SB A310-54-2024 Before next flight None None No crack found

and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None 5,800 FC /11,600 FH Or Apply SB A310-54-2024 Before next flight None None Crack found but not confirmed with HFEC inspection and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3 Apply TASK 542018-833-803 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection and apply TASK 542018-832-802 001 Inspection Post Repair Refer to table 2

Crack found >=20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection Contact Airbus Before next flight None None

NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 12 5

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# @A310 SERVICE BULLETIN
NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. Table 2: 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) Config. 002 Apply TASK 542018-832-802 001 Inspection Post Repair 11,200 FC /22,500 FH from repair embodiment 2,000 FC See NOTE (*) None

No crack found Apply TASK 542018-832-802 001 Inspection Post Repair None None 3,500 FC /7,100 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 sheduled 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Config .002 Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 9,900 FC /19,800 FH from SB A310-54- 2024 embodiment 1,000 FC see NOTE (*) 500 FC see NOTE (**) None

No crack found Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 None None 3,500 FC /7,100 FH Crack found Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 13 5

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# @A310 SERVICE BULLETIN
Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE (**): For A310-200 post SB 54-0024 with more than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with more than 13,900 FC from embodiment: 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. **CONF 003 This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Config. 003 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 9,700 FC /19,400 FH None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 14 5

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# @A310 SERVICE BULLETIN
Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None 6,700 FC /13,400 FH Or Apply SB A310-54-2024 Before next flight None None No crack found

and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None 6,700 FC /13,400 FH Or Apply SB A310-54-2024 Before next flight None None Crack found but not confirmed with HFEC inspection and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3 Apply TASK 542018-833-803 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection and apply TASK 542018-832-802 001 Inspection Post Repair Refer to table 2

Crack found >=20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection Contact Airbus Before next flight None None

NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 15 5

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# @A310 SERVICE BULLETIN
NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. Table 2: 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) Config. 003 Apply TASK 542018-832-802 001 Inspection Post Repair 10,200 FC /20,400 FH from repair embodiment 2,000 FC See NOTE (*) None

No crack found Apply TASK 542018-832-802 001 Inspection Post Repair None None 3,200 FC /6,400 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 sheduled 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Config .003 Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 9,000 FC /18,000 FH from SB A310-54- 2024 embodiment 1,000 FC see NOTE (*) 500 FC see NOTE (**) None

No crack found Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 None None 3,200 FC /6,400 FH Crack found Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 16 5

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# @A310 SERVICE BULLETIN
Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE (**): For A310-200 post SB 54-0024 with more than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with more than 13,900 FC from embodiment: 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. **CONF 004 This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 8,600 FC /24,000 FH Config. 004 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 LR: 5,900 FC /29,500 FH None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 17 5

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# @A310 SERVICE BULLETIN
Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 6,700 FC /18,700 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 6,000 FC /30,300 FH Or Apply SB A310-54-2024 Before next flight None None No crack found

and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3
SR: 6,700 FC /18,700 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 6,000 FC /30,300 FH Or Apply SB A310-54-2024 Before next flight None None Crack found and its length is not confirmed with Eddy Current Inspection
and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3 Apply TASK 542018-833-803 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection and apply TASK 542018-832-802 001 Inspection Post Repair Refer to table 2

Crack found >=20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 18 5

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# @A310 SERVICE BULLETIN
NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B. Table 2: 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: 9,600 FC /25,500 FH from repair embodiment Config. 004 Apply TASK 542018-832-802 001 Inspection Post Repair

LR: 8,200 FC /41200 FH from repair embodiment 2,000 FC See NOTE (*) None

SR: 3,000 FC /8,100 FH No crack found Apply TASK 542018-832-802 001 Inspection Post Repair None None

LR: 2,600 FC /13,000 FH Crack found Contact Airbus Before next flight None None NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 19 5

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# @A310 SERVICE BULLETIN
Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 8,400 FC /22,500 FH from SB A310-54- 2024 embodiment Config. 004 Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024

LR: 7,200 FC /36,400 FH from SB A310-54- 2024 embodiment 1,000 FC see NOTE (*) 500 FC see NOTE (**) None

SR: 3,000 FC /8,100 FH No crack found Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 None None

LR: 2,600 FC /13,000 FH Crack found Contact Airbus Before next flight None None NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE (**): For A310-200 post SB 54-0024 with more than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with more than 13,900 FC from embodiment: 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 20 5

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# @A310 SERVICE BULLETIN
**CONF 005 This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 7,000 FC /19,600 FH Config. 005 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 LR: 4,800 FC /24,000 FH None None

SR: 5,800 FC /16,200 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 5,200 FC /26,300 FH Or Apply SB A310-54-2024 Before next flight None None No crack found

and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3
SR: 5,800 FC /16,200 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 5,200 FC /26,300 FH Or Apply SB A310-54-2024 Before next flight None None Crack found and its length is not confirmed with Eddy Current Inspection
and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 21 5

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# @A310 SERVICE BULLETIN
Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Apply TASK 542018-833-803 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection and apply TASK 542018-832-802 001 Inspection Post Repair Refer to table 2

Crack found >=20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection Contact Airbus Before next flight None None

NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 22 5

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# @A310 SERVICE BULLETIN
Table 2: 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: 9,600 FC /25,500 FH from repair embodiment Config. 005 Apply TASK 542018-832-802 001 Inspection Post Repair

LR: 8,200 FC /41,200 FH from repair embodiment 2,000 FC See NOTE (*) None

SR: 3,000 FC /8,100 FH No crack found Apply TASK 542018-832-802 001 Inspection Post Repair None None

LR: 2,600 FC /13,000 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 sheduled 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 23 5

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# @A310 SERVICE BULLETIN
Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 8,400 FC /22,500 FH from SB A310-54- 2024 embodiment Config. 005 Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024

LR: 7,200 FC /36,400 FH from SB A310-54- 2024 embodiment 1,000 FC see NOTE (*) 500 FC see NOTE (**) None

SR: 3,000 FC /8,100 FH No crack found Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 None None

LR: 2,600 FC /13,000 FH Crack found Contact Airbus Before next flight None None NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE (**): For A310-200 post SB 54-0024 with more than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with more than 13,900 FC from embodiment: 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 24 5

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# @A310 SERVICE BULLETIN
**CONF 006 This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 7,000 FC /19,600 FH Config. 006 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 LR: 4,800 FC /24,100 FH None None

SR: 5,700 FC /15,900 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 5,100 FC /25,500 FH Or Apply SB A310-54-2024 Before next flight None None No crack found

and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3
SR: 5,700 FC /15,900 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 5,100 FC /25,500 FH Or Apply SB A310-54-2024 Before next flight None None Crack found and its length is not confirmed with Eddy Current Inspection
and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 25 5

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# @A310 SERVICE BULLETIN
Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Apply TASK 542018-833-803 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection and apply TASK 542018-832-802 001 Inspection Post Repair Refer to table 2

Crack found >=20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection Contact Airbus Before next flight None None

NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 26 5

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# @A310 SERVICE BULLETIN
Table 2: 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: 10,900 FC /30,600 FH from repair embodiment Config. 006 Apply TASK 542018-832-802 001 Inspection Post Repair

LR: 10,100 FC /50,800 FH from repair embodiment 2,000 FC See NOTE (*) None

SR: 3,400 FC /9,700 FH No crack found Apply TASK 542018-832-802 001 Inspection Post Repair None None

LR: 3,200 FC /16,100 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 sheduled 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 27 5

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# @A310 SERVICE BULLETIN
Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 9,600 FC /27,000 FH from SB A310-54- 2024 embodiment Config. 006 Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024

LR: 8,900 FC /44,900 FH from SB A310-54- 2024 embodiment 1,000 FC see NOTE (*) 500 FC see NOTE (**) None

SR: 3,400 FC /9,700 FH No crack found Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 None None

LR: 3,200 FC /16,100 FH Crack found Contact Airbus Before next flight None None NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE (**): For A310-200 post SB 54-0024 with more than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with more than 13,900 FC from embodiment: 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 28 5

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# @A310 SERVICE BULLETIN
**CONF 007 This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 7,000 FC /19,600 FH Config. 007 Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 LR: 4,800 FC /24,100 FH None None

SR: 5,700 FC /15,900 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 5,100 FC /25,500 FH Or Apply SB A310-54-2024 Before next flight None None No crack found

and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3
SR: 5,700 FC /15,900 FH Apply TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 None None

LR: 5,100 FC /25,500 FH Or Apply SB A310-54-2024 Before next flight None None Crack found and its length is not confirmed with Eddy Current Inspection
and apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 Refer to table 3

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 29 5

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# @A310 SERVICE BULLETIN
Table 1: Detailed Inspection of the LH/RH side Panels on the Pylon 1 and 2 Pre-repair and pre Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) Apply TASK 542018-833-803 001 Repair Before 1000 FC None None Crack found <20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection and apply TASK 542018-832-802 001 Inspection Post Repair Refer to table 2

Crack found >=20 mm (0.787 in.) and its length confirmed with Eddy Current Inspection Contact Airbus Before next flight None None

NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 30 5

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# @A310 SERVICE BULLETIN
Table 2: 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: 12,100 FC /33,800 FH from repair embodiment Config. 007 Apply TASK 542018-832-802 001 Inspection Post Repair

LR: 10,400 FC /51,800 FH from repair embodiment 2,000 FC See NOTE (*) None

SR: 3,800 FC /10,700 FH No crack found Apply TASK 542018-832-802 001 Inspection Post Repair None None

LR: 3,500 FC /17,800 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 sheduled 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 31 5

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# @A310 SERVICE BULLETIN
Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No. A310-54-2024 Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) SR: 10,700 FC /29,900 FH from SB A310-54- 2024 embodiment Config. 007 Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024

LR: 9,900 FC /49,700 FH from SB A310-54- 2024 embodiment 1,000 FC see NOTE (*) 500 FC see NOTE (**) None

SR: 3,800 FC /10,700 FH No crack found Apply TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 None None

LR: 3,500 FC /17,800 FH Crack found Contact Airbus Before next flight None None NOTE (*): For A310-200 post SB A310-54-2024 with less than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with less than 13,900 FC from embodiment: For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval, the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB. NOTE (**): For A310-200 post SB 54-0024 with more than 17,700 FC from embodiment or A310-300 post SB A310-54-2024 with more than 13,900 FC from embodiment: 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. NOTE: A310-200 aircraft model concerns aircraft models A310-203, 310-203C, 310-204, 310-221, 310-222. NOTE: A310-300 aircraft model concerns aircraft models A310-304, 310-308, 310-322, 310-324, 310-325. NOTE: For Average Flight Time (AFT - limit between Short Range (SR) and Long Range (LR) mission) configuration refer to ALI Document Section B.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 32 5

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# @A310 SERVICE BULLETIN
**CONF ALL F. APPROVAL Approved underEASA Design Organisation ApprovalNo. 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. For an explanation of the manhours and elapsed time, refer to the Gantt Chart given in Appendix 05. **CONF 001 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and 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 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 18.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 33 5

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# @A310 SERVICE BULLETIN
Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair Get Access 6.00 On Aircraft Repair the Side Panel of the Pylon 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 002 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and 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 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair Get Access 6.00 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 34 5

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# @A310 SERVICE BULLETIN
Task 542018-833-803-001: Repair On Aircraft Repair the Side Panel of the Pylon 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 003 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and 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 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair Get Access 6.00 On Aircraft Repair the Side Panel of the Pylon 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 35 5

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# @A310 SERVICE BULLETIN
**CONF 004 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and 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 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair Get Access 6.00 On Aircraft Repair the Side Panel of the Pylon 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 005 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 4.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 36 5

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# @A310 SERVICE BULLETIN
Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and 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 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair Get Access 6.00 On Aircraft Repair the Side Panel of the Pylon 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 006 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair Get Access 6.00 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 37 5

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# @A310 SERVICE BULLETIN
Task 542018-832-802-001: Inspection Post Repair On Aircraft Do a Detailed Inspection of the LH and 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 Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair Get Access 6.00 On Aircraft Repair the Side Panel of the Pylon 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 007 Task 542018-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 4.00 Close-Up 6.00 TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 Task 542018-832-802-001: Inspection Post Repair Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH and 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 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 38 5

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# @A310 SERVICE BULLETIN
Task 542018-832-803-001: Inspection Post Service Bulletin No. A310-54-2024 Get Access 6.00 On Aircraft Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 18.00 Close-Up 6.00 TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 Task 542018-833-803-001: Repair Get Access 6.00 On Aircraft Repair the Side Panel of the Pylon 46.00 Close-Up 6.00 TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF ALL H. WEIGHT AND BALANCE 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 542018-833-802 001 Repair: Manufacturers Empty Weight +0.85 KG (+1.8739 LB) Effect on Balance +20.49 KGM (+148.204 LB.FT ) I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-21-00 06-31-00 06-41-54 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) 51-10-20 51-70-00 54-50-34 Service Bulletin (SB) A310-54-2024 Standards Manual (SM) Structural Repair Manual (SRM) 54-51-31 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 39 5

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# @A310 SERVICE BULLETIN
**CONF 002 Aircraft Maintenance Manual (AMM) 06-21-00 06-31-00 06-41-54 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) 51-10-20 51-70-00 54-50-34 Service Bulletin (SB) A310-54-2024 Standards Manual (SM) Structural Repair Manual (SRM) 54-51-31 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 003 Aircraft Maintenance Manual (AMM) 06-21-00 06-31-00 06-41-54 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) 51-10-20 51-70-00 54-50-34 Service Bulletin (SB) A310-54-2024 Standards Manual (SM) Structural Repair Manual (SRM) 54-51-31 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 004 Aircraft Maintenance Manual (AMM) 06-21-00 06-31-00 06-41-54 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) 51-10-20 51-70-00 54-50-34 Service Bulletin (SB) A310-54-2024 Standards Manual (SM) Structural Repair Manual (SRM) 54-51-31 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 005 Aircraft Maintenance Manual (AMM) 06-21-00 06-31-00 06-41-54 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) 51-10-20 51-70-00 54-50-34 Service Bulletin (SB) A310-54-2024 Standards Manual (SM) Structural Repair Manual (SRM) 54-51-31
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 40 5

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# @A310 SERVICE BULLETIN
Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 006 Aircraft Maintenance Manual (AMM) 06-21-00 06-31-00 06-41-54 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) 51-10-20 51-70-00 54-50-34 Service Bulletin (SB) A310-54-2024 Standards Manual (SM) Structural Repair Manual (SRM) 54-51-31 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 007 Aircraft Maintenance Manual (AMM) 06-21-00 06-31-00 06-41-54 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) 51-10-20 51-70-00 54-50-34 Service Bulletin (SB) A310-54-2024 Standards Manual (SM) Structural Repair Manual (SRM) 54-51-31 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF ALL K. PUBLICATION AFFECTED

Maintenance Planning Document (MPD) 545043-01-1 545043-01-2 545043-02-1 545043-02-2 545043-03-1 545043-03-2 545043-03-3 545043-04-1 545043-04-2 545043-04-3 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 41 5

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# @A310 SERVICE BULLETIN

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# @A310 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 542018A01R03 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 542018A01R03 Cost 3,960.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. 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 542018A01R03 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 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 43 5

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2314-6-16 8 Screw NAS1153E3 4 Screw 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 Solvent General Purpose 11-026 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. A310-54-2024, equipment and material for control by eddy current as per NTM 51-10-20 Part 6. - For inspection program during accomplishment of repair, equipment and material for control by eddy current as per NTM 51-10-20 Part 6.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 44 5

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# @A310 SERVICE BULLETIN (2) Tools None (3) Special Tools None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 45 5

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# @A310 SERVICE BULLETIN

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# @A310 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 542018-832-801-001 - Inspection Pre Repairand Pre Service Bulletin No. A310-54-2024 WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE, TO DO THIS : - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF 002 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 47 5

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# @A310 SERVICE BULLETIN
**CONF 003 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF 004 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF 005 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF 006 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF 007 Zone From 410 to 420 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 48 5

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# @A310 SERVICE BULLETIN

Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 16.00 ELAPSED TIME (HOURS) 4.00 **CONF ALL A. GENERAL 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. **CONF 001 (1) Subtask 542018-910-005-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 49 5

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# @A310 SERVICE BULLETIN (2) Subtask 542018-900-002-001 - 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 542018-910-005-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-900-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 50 5

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# @A310 SERVICE BULLETIN
**CONF 003 (1) Subtask 542018-910-005-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-900-002-001 - 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 004 (1) Subtask 542018-910-005-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 51 5

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# @A310 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-900-002-001 - 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 005 (1) Subtask 542018-910-005-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 52 5

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# @A310 SERVICE BULLETIN

References 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-900-002-001 - 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 006 (1) Subtask 542018-910-005-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 53 5

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# @A310 SERVICE BULLETIN (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-900-002-001 - 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 007 (1) Subtask 542018-910-005-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-900-002-001 - Administrative Manpower Resources Skills NON SPECIFIC DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 54 5

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# @A310 SERVICE BULLETIN 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 542018-941-003-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 002 (1) Subtask 542018-941-003-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 55 5

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# @A310 SERVICE BULLETIN (b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 003 (1) Subtask 542018-941-003-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 56 5

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# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 542018-941-003-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 005 (1) Subtask 542018-941-003-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 57 5

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# @A310 SERVICE BULLETIN (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 006 (1) Subtask 542018-941-003-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 007 (1) Subtask 542018-941-003-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 58 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 542018-832-002-001 - Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 59 5

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# @A310 SERVICE BULLETIN
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) 51-10-20 Part 6 51-70-00 Part 7 Service Bulletin (SB) A310-54-2024 Fig. A-FBAAA Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, refer to NTM 51-70-00 Part 7 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer toFig. A-FBAAA Sheet 01 andFig. A-FFAAA Sheet 01 1 If no crack is found:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack with High Frequency Eddy Current (HFEC) Inspection (Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 60 5

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# @A310 SERVICE BULLETIN

3 If crack is not confirmed:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 4 If crack < 20 mm (0.787 in.):
a Do the repair before 1000FC, refer to TASK 542018-833-803 001 Repair and Do a detailed inspection as described in TASK 542018-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). 5 If crack >=20 mm (0.787 in.):
a Contact Airbus before next flight. **CONF 002 (1) Subtask 542018-832-002-001 - Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 61 5

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# @A310 SERVICE BULLETIN
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) 51-10-20 Part 6 51-70-00 Part 7 Service Bulletin (SB) A310-54-2024 Fig. A-FBAAA Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, refer to NTM 51-70-00 Part 7 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer toFig. A-FBAAA Sheet 01 andFig. A-FFAAA Sheet 01 1 If no crack is found:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack with High Frequency Eddy Current (HFEC) Inspection (Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 62 5

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# @A310 SERVICE BULLETIN

3 If crack is not confirmed:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 4 If crack < 20 mm (0.787 in.):
a Do the repair before 1000FC, refer to TASK 542018-833-803 001 Repair and Do a detailed inspection as described in TASK 542018-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). 5 If crack >=20 mm (0.787 in.):
a Contact Airbus before next flight. **CONF 003 (1) Subtask 542018-832-002-001 - Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 63 5

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# @A310 SERVICE BULLETIN
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) 51-10-20 Part 6 51-70-00 Part 7 Service Bulletin (SB) A310-54-2024 Fig. A-FBAAA Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, refer to NTM 51-70-00 Part 7 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer toFig. A-FBAAA Sheet 01 andFig. A-FFAAA Sheet 01 1 If no crack is found:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack with High Frequency Eddy Current (HFEC) Inspection (Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 64 5

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# @A310 SERVICE BULLETIN

3 If crack is not confirmed:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 4 If crack < 20 mm (0.787 in.):
a Do the repair before 1000FC, refer to TASK 542018-833-803 001 Repair and Do a detailed inspection as described in TASK 542018-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). 5 If crack >=20 mm (0.787 in.):
a Contact Airbus before next flight. **CONF 004 (1) Subtask 542018-832-002-001 - Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 65 5

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

# @A310 SERVICE BULLETIN
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) 51-10-20 Part 6 51-70-00 Part 7 Service Bulletin (SB) A310-54-2024 Fig. A-FBAAA Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, refer to NTM 51-70-00 Part 7 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer toFig. A-FBAAA Sheet 01 andFig. A-FFAAA Sheet 01 1 If no crack is found:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack with High Frequency Eddy Current (HFEC) Inspection (Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 66 5

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# @A310 SERVICE BULLETIN

3 If crack is not confirmed:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 4 If crack < 20 mm (0.787 in.):
a Do the repair before 1000FC, refer to TASK 542018-833-803 001 Repair and Do a detailed inspection as described in TASK 542018-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). 5 If crack >=20 mm (0.787 in.):
a Contact Airbus before next flight. **CONF 005 (1) Subtask 542018-832-002-001 - Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 67 5

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# @A310 SERVICE BULLETIN
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) 51-10-20 Part 6 51-70-00 Part 7 Service Bulletin (SB) A310-54-2024 Fig. A-FBAAA Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, refer to NTM 51-70-00 Part 7 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer toFig. A-FBAAA Sheet 01 andFig. A-FFAAA Sheet 01 1 If no crack is found:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack with High Frequency Eddy Current (HFEC) Inspection (Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 68 5

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# @A310 SERVICE BULLETIN

3 If crack is not confirmed:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 4 If crack < 20 mm (0.787 in.):
a Do the repair before 1000FC, refer to TASK 542018-833-803 001 Repair and Do a detailed inspection as described in TASK 542018-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). 5 If crack >=20 mm (0.787 in.):
a Contact Airbus before next flight. **CONF 006 (1) Subtask 542018-832-002-001 - Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 69 5

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# @A310 SERVICE BULLETIN
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) 51-10-20 Part 6 51-70-00 Part 7 Service Bulletin (SB) A310-54-2024 Fig. A-FBAAA Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, refer to NTM 51-70-00 Part 7 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer toFig. A-FBAAA Sheet 01 andFig. A-FFAAA Sheet 01 1 If no crack is found:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack with High Frequency Eddy Current (HFEC) Inspection (Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 70 5

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# @A310 SERVICE BULLETIN

3 If crack is not confirmed:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 4 If crack < 20 mm (0.787 in.):
a Do the repair before 1000FC, refer to TASK 542018-833-803 001 Repair and Do a detailed inspection as described in TASK 542018-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). 5 If crack >=20 mm (0.787 in.):
a Contact Airbus before next flight. **CONF 007 (1) Subtask 542018-832-002-001 - Do a Detailed Inspection of the LH and RH side Panels on the Pylons 1 and 2 Pre Repair and pre SB A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 71 5

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# @A310 SERVICE BULLETIN
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) 51-10-20 Part 6 51-70-00 Part 7 Service Bulletin (SB) A310-54-2024 Fig. A-FBAAA Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, refer to NTM 51-70-00 Part 7 of the side panels on the Pylons 1 and 2 in the upper section at rib 8. Refer toFig. A-FBAAA Sheet 01 andFig. A-FFAAA Sheet 01 1 If no crack is found:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Confirm crack with High Frequency Eddy Current (HFEC) Inspection (Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 72 5

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# @A310 SERVICE BULLETIN

3 If crack is not confirmed:
a Re-inspect the area as described in TASK 542018-832-801 001 Inspection Pre Repair and Pre Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2).
or b Accomplish Service Bulletin No.A310-54-2024. and Do a detailed inspection as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the threshold given in PLANNING INFORMATION Paragraph E.(2). 4 If crack < 20 mm (0.787 in.):
a Do the repair before 1000FC, refer to TASK 542018-833-803 001 Repair and Do a detailed inspection as described in TASK 542018-832-802 001 Inspection Post Repair at the threshold given in PLANNING INFORMATION Paragraph E.(2). 5 If crack >=20 mm (0.787 in.):
a Contact Airbus before next flight. **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF 003 None **CONF 004 None **CONF 005 None
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 73 5

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# @A310 SERVICE BULLETIN
**CONF 006 None **CONF 007 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 542018-942-004-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 002 (1) Subtask 542018-942-004-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 74 5

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# @A310 SERVICE BULLETIN (b) Install the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 003 (1) Subtask 542018-942-004-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 004 (1) Subtask 542018-942-004-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 75 5

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# @A310 SERVICE BULLETIN (b) Install the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 005 (1) Subtask 542018-942-004-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 006 (1) Subtask 542018-942-004-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 76 5

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# @A310 SERVICE BULLETIN (b) Install the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 007 (1) Subtask 542018-942-004-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 77 5

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# @A310 SERVICE BULLETIN

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DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 78 5

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# @A310 SERVICE BULLETIN Task 542018-832-802-001 - 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 002 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 79 5

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# @A310 SERVICE BULLETIN
**CONF 003 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 004 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 005 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 006 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 007 Zone From 410 to 420 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 80 5

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# @A310 SERVICE BULLETIN

Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF ALL A. GENERAL 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. **CONF 001 (1) Subtask 542018-910-001-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-31-00, 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 06-31-00, Page Block 001.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 81 5

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# @A310 SERVICE BULLETIN (2) Subtask 542018-839-001-001 - 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 542018-910-001-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-31-00, 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 06-31-00, Page Block 001. (2) Subtask 542018-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 82 5

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# @A310 SERVICE BULLETIN
**CONF 003 (1) Subtask 542018-910-001-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-31-00, 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 06-31-00, Page Block 001. (2) Subtask 542018-839-001-001 - 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 542018-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 83 5

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# @A310 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-31-00, 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 06-31-00, Page Block 001. (2) Subtask 542018-839-001-001 - 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 542018-910-001-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-31-00, Page Block 001 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 84 5

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# @A310 SERVICE BULLETIN

References 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 06-31-00, Page Block 001. (2) Subtask 542018-839-001-001 - 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 006 (1) Subtask 542018-910-001-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-31-00, 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 85 5

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# @A310 SERVICE BULLETIN (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 06-31-00, Page Block 001. (2) Subtask 542018-839-001-001 - 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 007 (1) Subtask 542018-910-001-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 06-31-00, 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 06-31-00, Page Block 001. (2) Subtask 542018-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 86 5

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

# @A310 SERVICE BULLETIN 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 542018-941-004-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 002 (1) Subtask 542018-941-004-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 87 5

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

# @A310 SERVICE BULLETIN (b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 003 (1) Subtask 542018-941-004-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 88 5

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

# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 542018-941-004-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 005 (1) Subtask 542018-941-004-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 89 5

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

# @A310 SERVICE BULLETIN (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 006 (1) Subtask 542018-941-004-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 007 (1) Subtask 542018-941-004-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 90 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 542018-832-005-001 - Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 91 5

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# @A310 SERVICE BULLETIN
Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.5 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-20 Part 6 51-70-00 Part 7 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 51-10-20 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBBAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-802 001 Inspection Post Repair at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 002 (1) Subtask 542018-832-005-001 - Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 92 5

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

# @A310 SERVICE BULLETIN
Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.5 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-20 Part 6 51-70-00 Part 7 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 51-10-20 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBBAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-802 001 Inspection Post Repair at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 003 (1) Subtask 542018-832-005-001 - Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 93 5

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

# @A310 SERVICE BULLETIN
Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.5 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-20 Part 6 51-70-00 Part 7 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 51-10-20 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBBAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-802 001 Inspection Post Repair at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 004 (1) Subtask 542018-832-005-001 - Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 94 5

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

# @A310 SERVICE BULLETIN
Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.5 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-20 Part 6 51-70-00 Part 7 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 51-10-20 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBBAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-802 001 Inspection Post Repair at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 005 (1) Subtask 542018-832-005-001 - Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 95 5

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# @A310 SERVICE BULLETIN
Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.5 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-20 Part 6 51-70-00 Part 7 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 51-10-20 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBBAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-802 001 Inspection Post Repair at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 006 (1) Subtask 542018-832-005-001 - Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 96 5

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

# @A310 SERVICE BULLETIN
Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.5 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-20 Part 6 51-70-00 Part 7 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 51-10-20 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBBAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-802 001 Inspection Post Repair at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 007 (1) Subtask 542018-832-005-001 - Do a Detailed Inspection of the LH and RH Side Panels on the Pylons 1 and 2 Post Repair Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 97 5

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

# @A310 SERVICE BULLETIN
Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.5 Skills AIRFRAME NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-20 Part 6 51-70-00 Part 7 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 51-10-20 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBBAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-802 001 Inspection Post Repair at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF 003 None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 98 5

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# @A310 SERVICE BULLETIN
**CONF 004 None **CONF 005 None **CONF 006 None **CONF 007 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 542018-942-005-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 002 (1) Subtask 542018-942-005-001 - Close-up Manpower Resources Skills NON SPECIFIC DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 99 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 003 (1) Subtask 542018-942-005-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 100 5

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

# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 542018-942-005-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 005 (1) Subtask 542018-942-005-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 101 5

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# @A310 SERVICE BULLETIN
**CONF 006 (1) Subtask 542018-942-005-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 007 (1) Subtask 542018-942-005-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 102 5

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# @A310 SERVICE BULLETIN Task 542018-832-803-001 - Inspection Post Service Bulletin No. A310-54-2024 **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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 002 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 103 5

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# @A310 SERVICE BULLETIN
**CONF 003 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 004 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 005 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 006 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF 007 Zone From 410 to 420 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 104 5

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# @A310 SERVICE BULLETIN

Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 30.00 ELAPSED TIME (HOURS) 7.50 **CONF ALL A. GENERAL 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. **CONF 001 (1) Subtask 542018-910-003-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 105 5

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# @A310 SERVICE BULLETIN (2) Subtask 542018-839-002-001 - 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 542018-910-003-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 106 5

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# @A310 SERVICE BULLETIN
**CONF 003 (1) Subtask 542018-910-003-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-002-001 - 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 004 (1) Subtask 542018-910-003-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 107 5

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# @A310 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-002-001 - 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 005 (1) Subtask 542018-910-003-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-31-00, Page Block 001 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 108 5

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# @A310 SERVICE BULLETIN

References 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-002-001 - 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 006 (1) Subtask 542018-910-003-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 109 5

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# @A310 SERVICE BULLETIN (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-002-001 - 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 007 (1) Subtask 542018-910-003-001 - 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 Solvent General Purpose 11-026 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 the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (d) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 110 5

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# @A310 SERVICE BULLETIN 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 542018-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 002 (1) Subtask 542018-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 111 5

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# @A310 SERVICE BULLETIN (b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 003 (1) Subtask 542018-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 112 5

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# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 542018-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 005 (1) Subtask 542018-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 113 5

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# @A310 SERVICE BULLETIN (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 006 (1) Subtask 542018-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 007 (1) Subtask 542018-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 114 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 542018-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.50 Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 115 5

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# @A310 SERVICE BULLETIN

References Non Destructive Test Manual (NTM) 51-70-00 Part 7 54-50-34 Part 6 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBCAA Inspection Area: Post Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 54-50-34 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBCAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 002 (1) Subtask 542018-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.50 Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 116 5

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# @A310 SERVICE BULLETIN

References Non Destructive Test Manual (NTM) 51-70-00 Part 7 54-50-34 Part 6 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBCAA Inspection Area: Post Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 54-50-34 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBCAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 003 (1) Subtask 542018-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.50 Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 117 5

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# @A310 SERVICE BULLETIN

References Non Destructive Test Manual (NTM) 51-70-00 Part 7 54-50-34 Part 6 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBCAA Inspection Area: Post Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 54-50-34 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBCAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 004 (1) Subtask 542018-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.50 Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 118 5

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# @A310 SERVICE BULLETIN

References Non Destructive Test Manual (NTM) 51-70-00 Part 7 54-50-34 Part 6 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBCAA Inspection Area: Post Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 54-50-34 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBCAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 005 (1) Subtask 542018-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.50 Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 119 5

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# @A310 SERVICE BULLETIN

References Non Destructive Test Manual (NTM) 51-70-00 Part 7 54-50-34 Part 6 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBCAA Inspection Area: Post Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 54-50-34 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBCAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 006 (1) Subtask 542018-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.50 Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 120 5

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# @A310 SERVICE BULLETIN

References Non Destructive Test Manual (NTM) 51-70-00 Part 7 54-50-34 Part 6 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBCAA Inspection Area: Post Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 54-50-34 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBCAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF 007 (1) Subtask 542018-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.A310-54-2024 Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 18.00 Minimum number of person 4 Subtask elapsed time 4.50 Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 121 5

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# @A310 SERVICE BULLETIN

References Non Destructive Test Manual (NTM) 51-70-00 Part 7 54-50-34 Part 6 Fig. A-FFAAA Flow Chart Sheet 01 Fig. A-FBCAA Inspection Area: Post Service Bulletin No. A310-54-2024 Sheet 01 Fig. A-FBBAA Inspection Area: Post repair Sheet 01 At the threshold given in the PLANNING INFORMATION Paragraph E.(2): (a) Do a detailed inspection, (refer to NTM 51-70-00 Part 7), an HFEC inspection (refer to NTM 54-50-34 Part 6) and an Ultrasonic Inspection of holes (refer to Appendix 04: Non Destructive Testing Procedure ). Refer toFig. A-FFAAA Sheet 01 andFig. A-FBCAA Sheet 01 1 If no crack is found: - Re-inspect the area as described in TASK 542018-832-803 001 Inspection Post Service Bulletin No. A310-54-2024 at the interval given in PLANNING INFORMATION Paragraph E.(2). 2 If crack is found: - Contact Airbus before next flight. **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF 003 None **CONF 004 None **CONF 005 None
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 122 5

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# @A310 SERVICE BULLETIN
**CONF 006 None **CONF 007 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 542018-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 002 (1) Subtask 542018-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 123 5

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# @A310 SERVICE BULLETIN (b) Install the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 003 (1) Subtask 542018-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 004 (1) Subtask 542018-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 124 5

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# @A310 SERVICE BULLETIN (b) Install the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 005 (1) Subtask 542018-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 006 (1) Subtask 542018-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 125 5

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# @A310 SERVICE BULLETIN (b) Install the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 007 (1) Subtask 542018-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 126 5

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# @A310 SERVICE BULLETIN Task 542018-833-803-001 - 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 002 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 127 5

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# @A310 SERVICE BULLETIN
**CONF 003 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 004 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 005 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 006 Zone From 410 to 420 Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF 007 Zone From 410 to 420 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 128 5

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# @A310 SERVICE BULLETIN

Access Panel 413CL or 413GL and 413EL 414CR or 414GR and 414ER 423CL or 423GL and 423EL 424CR or 424GR and 424ER Manpower TOTAL MANHOURS 58.00 ELAPSED TIME (HOURS) 14.50 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 542018-910-004-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (b) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-003-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 129 5

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 542018-910-004-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (b) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-003-001 - 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 542018-910-004-001 - 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 Solvent General Purpose 11-026 As required

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 130 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (b) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-003-001 - 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 004 (1) Subtask 542018-910-004-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (b) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 131 5

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# @A310 SERVICE BULLETIN (2) Subtask 542018-839-003-001 - 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 005 (1) Subtask 542018-910-004-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (b) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-003-001 - 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 006 (1) Subtask 542018-910-004-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 132 5

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# @A310 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML. (b) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-003-001 - 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 007 (1) Subtask 542018-910-004-001 - 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 Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the material numbers (Mat. No.) given in this Service Bulletin, refer to the CML.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 133 5

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# @A310 SERVICE BULLETIN (b) Clean the surfaces to seal with Solvent General Purpose 11-026 As required

and refer to AMM 20-31-00, Page Block 001. (2) Subtask 542018-839-003-001 - 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 542018-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 134 5

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 542018-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 003 (1) Subtask 542018-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 135 5

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# @A310 SERVICE BULLETIN (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 004 (1) Subtask 542018-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 005 (1) Subtask 542018-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 136 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 006 (1) Subtask 542018-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 137 5

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# @A310 SERVICE BULLETIN (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF 007 (1) Subtask 542018-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (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 the access platforms in position. (d) Remove the LH side access panels for the pylon 1, 413CL and 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (e) Remove the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the LH side access panels for the pylon 2, 423CL and 423EL or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (g) Remove the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 542018-833-016-001 - Repair the Side Panel of the Pylon Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 138 5

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# @A310 SERVICE BULLETIN
Manpower Resources Manhours 46.00 Minimum number of person 4 Subtask elapsed time 11.50 Skills AIRFRAME NON DESTRUCTIVE TESTING Material necessary to do the job Kit 542018A01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD 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 NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim References Non Destructive Test Manual (NTM) 51-10-20 Part 6 Structural Repair Manual (SRM) 54-51-31 (a) Perform repair in accordance with SRM 54-51-31. (b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally removed, refer to NTM 51-10-20 Part 6. (c) Install : 1 Doubler A5461255220000 1 Doubler A5461255220100 2 Shim R5461012420200 with : 8 Washer A5461255320000 6 Washer A5461255420000
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 139 5

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# @A310 SERVICE BULLETIN

4 Screw ASNA2314-6-14 8 Screw ASNA2314-6-16 6 Screw ASNA2314-4-13 2 Screw NAS1154-13 4 Screw NAS1153E3 8 Nut NAS1726-6E 8 Nut NAS1726-4E 16 Rivet NSA5414-36-20 (d) Do a new inspection program as described in TASK 542018-832-802 001 Inspection Post Repair . **CONF 002 (1) Subtask 542018-833-016-001 - Repair the Side Panel of the Pylon Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 46.00 Minimum number of person 4 Subtask elapsed time 11.50 Skills AIRFRAME NON DESTRUCTIVE TESTING Material necessary to do the job Kit 542018A01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES A5461255220000 1 Doubler A5461255220100 1 Doubler A5461255320000 8 Washer A5461255420000 6 Washer ASNA2314-4-13 6 Screw DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 140 5

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2314-6-14 4 Screw ASNA2314-6-16 8 Screw NAS1153E3 4 Screw NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim References Non Destructive Test Manual (NTM) 51-10-20 Part 6 Structural Repair Manual (SRM) 54-51-31 (a) Perform repair in accordance with SRM 54-51-31. (b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally removed, refer to NTM 51-10-20 Part 6. (c) Install : 1 Doubler A5461255220000 1 Doubler A5461255220100 2 Shim R5461012420200 with : 8 Washer A5461255320000 6 Washer A5461255420000 4 Screw ASNA2314-6-14 8 Screw ASNA2314-6-16 6 Screw ASNA2314-4-13 2 Screw NAS1154-13 4 Screw NAS1153E3 8 Nut NAS1726-6E 8 Nut NAS1726-4E 16 Rivet NSA5414-36-20

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 141 5

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# @A310 SERVICE BULLETIN (d) Do a new inspection program as described in TASK 542018-832-802 001 Inspection Post Repair . **CONF 003 (1) Subtask 542018-833-016-001 - Repair the Side Panel of the Pylon Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 46.00 Minimum number of person 4 Subtask elapsed time 11.50 Skills AIRFRAME NON DESTRUCTIVE TESTING Material necessary to do the job Kit 542018A01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD 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 NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim References Non Destructive Test Manual (NTM) 51-10-20 Part 6 Structural Repair Manual (SRM) 54-51-31 (a) Perform repair in accordance with SRM 54-51-31.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 142 5

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# @A310 SERVICE BULLETIN (b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally removed, refer to NTM 51-10-20 Part 6. (c) Install : 1 Doubler A5461255220000 1 Doubler A5461255220100 2 Shim R5461012420200 with : 8 Washer A5461255320000 6 Washer A5461255420000 4 Screw ASNA2314-6-14 8 Screw ASNA2314-6-16 6 Screw ASNA2314-4-13 2 Screw NAS1154-13 4 Screw NAS1153E3 8 Nut NAS1726-6E 8 Nut NAS1726-4E 16 Rivet NSA5414-36-20 (d) Do a new inspection program as described in TASK 542018-832-802 001 Inspection Post Repair . **CONF 004 (1) Subtask 542018-833-016-001 - Repair the Side Panel of the Pylon Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 143 5

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# @A310 SERVICE BULLETIN
Manpower Resources Manhours 46.00 Minimum number of person 4 Subtask elapsed time 11.50 Skills AIRFRAME NON DESTRUCTIVE TESTING Material necessary to do the job Kit 542018A01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD 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 NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim References Non Destructive Test Manual (NTM) 51-10-20 Part 6 Structural Repair Manual (SRM) 54-51-31 (a) Perform repair in accordance with SRM 54-51-31. (b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally removed, refer to NTM 51-10-20 Part 6. (c) Install : 1 Doubler A5461255220000 1 Doubler A5461255220100 2 Shim R5461012420200 with : 8 Washer A5461255320000 6 Washer A5461255420000
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 144 5

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# @A310 SERVICE BULLETIN

4 Screw ASNA2314-6-14 8 Screw ASNA2314-6-16 6 Screw ASNA2314-4-13 2 Screw NAS1154-13 4 Screw NAS1153E3 8 Nut NAS1726-6E 8 Nut NAS1726-4E 16 Rivet NSA5414-36-20 (d) Do a new inspection program as described in TASK 542018-832-802 001 Inspection Post Repair . **CONF 005 (1) Subtask 542018-833-016-001 - Repair the Side Panel of the Pylon Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 46.00 Minimum number of person 4 Subtask elapsed time 11.50 Skills AIRFRAME NON DESTRUCTIVE TESTING Material necessary to do the job Kit 542018A01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES A5461255220000 1 Doubler A5461255220100 1 Doubler A5461255320000 8 Washer A5461255420000 6 Washer ASNA2314-4-13 6 Screw DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 145 5

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2314-6-14 4 Screw ASNA2314-6-16 8 Screw NAS1153E3 4 Screw NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim References Non Destructive Test Manual (NTM) 51-10-20 Part 6 Structural Repair Manual (SRM) 54-51-31 (a) Perform repair in accordance with SRM 54-51-31. (b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally removed, refer to NTM 51-10-20 Part 6. (c) Install : 1 Doubler A5461255220000 1 Doubler A5461255220100 2 Shim R5461012420200 with : 8 Washer A5461255320000 6 Washer A5461255420000 4 Screw ASNA2314-6-14 8 Screw ASNA2314-6-16 6 Screw ASNA2314-4-13 2 Screw NAS1154-13 4 Screw NAS1153E3 8 Nut NAS1726-6E 8 Nut NAS1726-4E 16 Rivet NSA5414-36-20

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 146 5

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# @A310 SERVICE BULLETIN (d) Do a new inspection program as described in TASK 542018-832-802 001 Inspection Post Repair . **CONF 006 (1) Subtask 542018-833-016-001 - Repair the Side Panel of the Pylon Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8 Manpower Resources Manhours 46.00 Minimum number of person 4 Subtask elapsed time 11.50 Skills AIRFRAME NON DESTRUCTIVE TESTING Material necessary to do the job Kit 542018A01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD 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 NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim References Non Destructive Test Manual (NTM) 51-10-20 Part 6 Structural Repair Manual (SRM) 54-51-31 (a) Perform repair in accordance with SRM 54-51-31.
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 147 5

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# @A310 SERVICE BULLETIN (b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally removed, refer to NTM 51-10-20 Part 6. (c) Install : 1 Doubler A5461255220000 1 Doubler A5461255220100 2 Shim R5461012420200 with : 8 Washer A5461255320000 6 Washer A5461255420000 4 Screw ASNA2314-6-14 8 Screw ASNA2314-6-16 6 Screw ASNA2314-4-13 2 Screw NAS1154-13 4 Screw NAS1153E3 8 Nut NAS1726-6E 8 Nut NAS1726-4E 16 Rivet NSA5414-36-20 (d) Do a new inspection program as described in TASK 542018-832-802 001 Inspection Post Repair . **CONF 007 (1) Subtask 542018-833-016-001 - Repair the Side Panel of the Pylon Work Zones and Access Panels Zone Access/Work location From 410 Access Panel 413CL or 413GL and 413EL, Panel 414CR or 414GR and 414ER Work location Rib 8 To 420 Access Panel 423CL or 423GL and 423EL, Panel 424CR or 424GR and 424ER Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 148 5

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# @A310 SERVICE BULLETIN
Manpower Resources Manhours 46.00 Minimum number of person 4 Subtask elapsed time 11.50 Skills AIRFRAME NON DESTRUCTIVE TESTING Material necessary to do the job Kit 542018A01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD 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 NAS1154-13 2 Screw NAS1726-4E 8 Nut NAS1726-6E 8 Nut NSA5414-36-20 16 Rivet R5461012420200 2 Shim References Non Destructive Test Manual (NTM) 51-10-20 Part 6 Structural Repair Manual (SRM) 54-51-31 (a) Perform repair in accordance with SRM 54-51-31. (b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally removed, refer to NTM 51-10-20 Part 6. (c) Install : 1 Doubler A5461255220000 1 Doubler A5461255220100 2 Shim R5461012420200 with : 8 Washer A5461255320000 6 Washer A5461255420000
DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 149 5

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# @A310 SERVICE BULLETIN

4 Screw ASNA2314-6-14 8 Screw ASNA2314-6-16 6 Screw ASNA2314-4-13 2 Screw NAS1154-13 4 Screw NAS1153E3 8 Nut NAS1726-6E 8 Nut NAS1726-4E 16 Rivet NSA5414-36-20 (d) Do a new inspection program as described in TASK 542018-832-802 001 Inspection Post Repair . **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF 003 None **CONF 004 None **CONF 005 None **CONF 006 None **CONF 007 None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 150 5

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# @A310 SERVICE BULLETIN
**CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 542018-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 002 (1) Subtask 542018-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 151 5

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# @A310 SERVICE BULLETIN (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 003 (1) Subtask 542018-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 004 (1) Subtask 542018-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 152 5

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# @A310 SERVICE BULLETIN (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 005 (1) Subtask 542018-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 006 (1) Subtask 542018-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 153 5

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# @A310 SERVICE BULLETIN (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms. **CONF 007 (1) Subtask 542018-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-54, 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 413EL or 413GL and 413EL (Refer to AMM 06-41-54, Page Block 001). (c) Install the RH side access panels for the pylon 1, 414ER and 414CR or 414GR and 414ER (Refer to AMM 06-41-54, Page Block 001). (d) Install the LH side access panels for the pylon 2, 423CL and 423DE or 423GL and 423EL (Refer to AMM 06-41-54, Page Block 001). (e) Install the RH side access panels for the pylon 2, 424ER and 424CR or 424GR and 424ER (Refer to AMM 06-41-54, Page Block 001). (f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 154 5

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# @A310 SERVICE BULLETIN

**CONF ALL

AREAS TO BE INSPECTED LENGTH



## B **FWD** RIB8 PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON 

### B **B**



## A RIB8

**NOTES:** RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION 

### A **A**

B_SB_542018_5_BAAA_01_00 Figure A-FBAAA - Sheet 01 Inspection Area: Pre repair and Pre Service Bulletin No. A310-54-2024 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 155 5

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# @A310 SERVICE BULLETIN

**CONF ALL

INSPECTION EDDY CURRENT DETAILED INSPECTION DOUBLER

20mm (0.787in.) FROM DOUBLER EDGE DETAILED INSPECTION AREA RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION 

### A **A**

RIB8 

## B **A A** 

**FWD** PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON 

### B **B**



## A RIB8

**NOTES:** ULTRASONIC INSPECTION HOLE
ULTRASONIC INSPECTION HOLE 

### A **A**

CUT−OUT

DOUBLER

B_SB_542018_5_BBAA_01_01 Figure A-FBBAA - Sheet 01 Inspection Area: Post repair DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 156 5

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# @A310 SERVICE BULLETIN

**CONF ALL

INSPECTION EDDY CURRENT DETAILED INSPECTION DOUBLER

20mm (0.787in.) FROM DOUBLER EDGE DETAILED INSPECTION AREA RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION 

### A **A**

RIB8 

## B **A A** 

**FWD** PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON 

### B **B**



## A RIB8

**NOTES:** ULTRASONIC INSPECTION HOLE
ULTRASONIC INSPECTION HOLE 

### A **A**

DOUBLER

B_SB_542018_5_BCAA_01_01 Figure A-FBCAA - Sheet 01 Inspection Area: Post Service Bulletin No. A310-54-2024 DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 157 5

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# @A310 SERVICE BULLETIN

**CONF ALL

QUESTION FINDING
ACTION NO CRACK FINDING

OR

CONTACT AIRBUS BEFORE NEXT FLIGHT YES DO A DETAILED INSPECTION OF THE SIDE PANELS ON THE PYLONS 1 AND 2 REFER TO TASK 542018−832−801−001 AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

APPLY THE SERVICE BULLETIN

A310−54−2024 (MOD No. 10431S20462)

DO A DETAILED INSPECTION, AN ULTRASONIC INSPECTION OF HOLES AND AN HFEC INSPECTION AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2) RE−INSPECT BY A DETAILED INSPECTION AT THE INTERVAL GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2) REFER TO TASK 542018−832−801−001

REFER TO TASK 542018−832−802−001

RE−INSPEC BY HFEC INSPECTION, A DETAILED INSPECTION AND AN ULTRASONIC INSPECTION OF HOLES AT THE INTERVAL GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2) REFER TO TASK 542018−832−803−001 NO CRACK FINDING YES COMFIRM CRACK WITH HFEC INSPECTION

NO CRACK CONFIRMED YES

OR
CRACK 20 mm (0.787 in) CRACK 20 mm (0.787 in)

REPAIR BEFORE 1000 FC REFER TO TASK 542018−833−803−001

CONTACT AIRBUS BEFORE NEXT FLIGHT NO CRACK FINDING YES DO AN HFEC INSPECTION, A DETAILED INSPECTION AND AN ULTRASONIC INSPECTION OF HOLES AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2) REFER TO TASK 542018−832−803−001

RE−INSPECT BY DETAILED INSPECTION, AN ULTRASONIC INSPECTION OF HOLES AND AN HFEC INSPECTION AT THE INTERVAL GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2) REFER TO TASK 542018−832−802−001

B_SB_542018_5_FAAA_01_02 Figure A-FFAAA - Sheet 01 Flow Chart DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 158 5

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# @A310 SERVICE BULLETIN Appendix 01: Inspection Report Pre repair and Pre Service Bulletin No. A310-54-2024 **CONF ALL (1) Inspection Report The results of the inspection, including no findings, replacement or actions to be done, must be forwarded to AIRBUS DepartmentSEES2, on theattached inspection report sheet.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN Appendix 01: Inspection Report Pre repair and Pre Service Bulletin No. A310-54-2024

**CONF ALL

AREAS TO BE INSPECTED LENGTH



## B **FWD** RIB8 PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON 

### B **B**



## A RIB8

**NOTES:** RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION 

### A **A**

B_SB_542018_5_RAAA_01_00 Figure A-FRAAA - Sheet 01 Inspection Report DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN Appendix 01: Inspection Report Pre repair and Pre Service Bulletin No. A310-54-2024

**CONF ALL

AIRBUS CUSTOMER SERVICES ENGINEERING − SEES2 WING FIX STRCTURE − ENGINE PYLON 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 36 14 **INSPECTION REPORT** SERVICE BULLETIN No. : A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : A310−54−2018

DATE OF INSPECTION : RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION EDDY CURRENT

NO CRACK

RH SIDE

RH SIDE DETAILED INSPECTION

LH SIDE

LH SIDE CRACK LENGHT

LH PYLON

RH PYLON EDDY CURRENT INSPECTION

SB A310−54−2024 APPLIED REPAIR APPLIED

B_SB_542018_5_RAAA_02_01 Figure A-FRAAA - Sheet 02 Inspection Report DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN Appendix 01: Inspection Report Pre repair and Pre Service Bulletin No. A310-54-2024

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN Appendix 02: Inspection Report Post repair **CONF ALL (1) Inspection Report The results of the inspection, including no findings, replacement or actions to be done, must be forwarded to AIRBUS DepartmentSEES2, on theattached inspection report sheet.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN Appendix 02: Inspection Report Post repair

**CONF ALL

INSPECTION EDDY CURRENT DETAILED INSPECTION DOUBLER

20mm (0.787in.) FROM DOUBLER EDGE DETAILED INSPECTION AREA RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION 

### A **A**

RIB8 

## B **A A** 

**FWD** PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON 

### B **B**



## A RIB8

**NOTES:** ULTRASONIC INSPECTION HOLE 2
ULTRASONIC INSPECTION HOLE 1 

### A **A**

CUT−OUT

DOUBLER

B_SB_542018_5_RBAA_01_01 Figure A-FRBAA - Sheet 01 Inspection Report DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN Appendix 02: Inspection Report Post repair

**CONF ALL

NO CRACK RH SIDE

RH SIDE DETAILED INSPECTION

LH SIDE

LH SIDE CRACK LENGHT

LH PYLON

RH PYLON AIRBUS CUSTOMER SERVICES ENGINEERING − SEES2 WING FIX STRCTURE − ENGINE PYLON 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 36 14 **INSPECTION REPORT** SERVICE BULLETIN No. : A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : A310−54−2018

DATE OF INSPECTION : RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION EDDY CURRENT

EDDY CURRENT INSPECTION ULTRASONIC INSPECTION

ULTRASONIC INSPECTION CRACK FOUND (GIVE HOLE No.)

B_SB_542018_5_RBAA_02_02 Figure A-FRBAA - Sheet 02 Inspection Report DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN Appendix 02: Inspection Report Post repair

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN Appendix 03: Inspection Report Post Service Bulletin No. A310-54-2024 **CONF ALL (1) Inspection Report The results of the inspection, including no findings, replacement or actions to be done, must be forwarded to AIRBUS DepartmentSEES2, on theattached inspection report sheet.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN Appendix 03: Inspection Report Post Service Bulletin No. A310-54-2024

**CONF ALL

INSPECTION EDDY CURRENT DETAILED INSPECTION DOUBLER

20mm (0.787in.) FROM DOUBLER EDGE DETAILED INSPECTION AREA RIGHT PYLON SHOWN LEFT PYLON SYMMETRICAL PW PYLON SHOWN IDENTICAL FOR GE PYLON INSPECTION 

### A **A**

RIB8 

## B **A A** 

**FWD** PW PYLON SHOWN INSPECTION IDENTICAL FOR GE PYLON 

### B **B**



## A RIB8

**NOTES:** ULTRASONIC INSPECTION HOLE 2
ULTRASONIC INSPECTION HOLE 1 

### A **A**

DOUBLER

B_SB_542018_5_RCAA_01_01 Figure A-FRCAA - Sheet 01 Inspection Report DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN Appendix 03: Inspection Report Post Service Bulletin No. A310-54-2024

**CONF ALL

NO CRACK RH SIDE

RH SIDE DETAILED INSPECTION

LH SIDE

LH SIDE CRACK LENGHT

LH PYLON

RH PYLON AIRBUS CUSTOMER SERVICES ENGINEERING − SEES2 WING FIX STRCTURE − ENGINE PYLON 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 36 14 **INSPECTION REPORT** SERVICE BULLETIN No. : A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : A310−54−2018

DATE OF INSPECTION : RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION EDDY CURRENT

EDDY CURRENT INSPECTION ULTRASONIC INSPECTION

AFTER EMBODIMENT OF THE SERVICE BULLETIN No. A310−54−2024

ULTRASONIC INSPECTION CRACK FOUND (GIVE HOLE No.)

B_SB_542018_5_RCAA_02_01 Figure A-FRCAA - Sheet 02 Inspection Report DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN Appendix 03: Inspection Report Post Service Bulletin No. A310-54-2024

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure **CONF ALL (1) Non Destructive Testing Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. This document contains the Non-Destructive inspection procedure related to the "Pylon - Lateral panel at RIB 8 area after doubler installation"

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_01_01 Figure A-FAAAA - Sheet 01 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_02_01 Figure A-FAAAA - Sheet 02 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_03_01 Figure A-FAAAA - Sheet 03 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_04_01 Figure A-FAAAA - Sheet 04 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 5 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_05_01 Figure A-FAAAA - Sheet 05 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 6 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_06_01 Figure A-FAAAA - Sheet 06 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 7 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_07_01 Figure A-FAAAA - Sheet 07 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 8 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_08_01 Figure A-FAAAA - Sheet 08 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 9 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_09_01 Figure A-FAAAA - Sheet 09 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 10 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_10_01 Figure A-FAAAA - Sheet 10 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 11 5

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# @A310 SERVICE BULLETIN Appendix 04: Non Destructive Testing Procedure

**CONF ALL

B_SB_542018_5_AAAA_11_00 Figure A-FAAAA - Sheet 11 Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation. DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 12 5

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# @A310 SERVICE BULLETIN Appendix 05: Elapsed Time Assumption **CONF ALL The following charts are only proposal. Operators may determine that another way to do the work is more suitable for them.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN Appendix 05: Elapsed Time Assumption

**CONF ALL

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A310−54−2018**

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 16.00 4.00 STEPS

6.00 1.50

0 DO A DETAILED INSPECTION OF THE LH/RH 4.00 1.00

CLOSE−UP 6.00 1.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01

02 **NOTE:** PER

4

4

4

: : SB ELAPSED TIME (HOURS) 1 2 3 4

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. SIDE PANELS ON THE PYLONS 1 AND 2 PRE−REPAIR AND PRE SB A310−54−2024

B_SB_542018_5_ABAA_01_00 Figure A-FABAA - Sheet 01 Elapsed Time Assumption DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 2 5

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# @A310 SERVICE BULLETIN Appendix 05: Elapsed Time Assumption

**CONF ALL

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A310−54−2018**

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 30.00 7.50 STEPS

6.00 1.50

DO A DETAILED INSPECTION OF THE LH/RH 18.00 4.50

CLOSE−UP 6.00 1.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01

02 **NOTE:** PER

4

4

4

: : SB ELAPSED TIME (HOURS)

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. SIDE PANELS ON THE PYLONS 1 AND 2 POST REPAIR

024 6 1357 8

B_SB_542018_5_ACAA_01_00 Figure A-FACAA - Sheet 01

Elapsed Time Assumption DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 3 5

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# @A310 SERVICE BULLETIN Appendix 05: Elapsed Time Assumption

**CONF ALL

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A310−54−2018**

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 30.00 7.50 STEPS

6.00 1.50

DO A DETAILED INSPECTION OF THE LH/RH 18.00 4.50

CLOSE−UP 6.00 1.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01

02 **NOTE:** PER

4

4

4

: : SB ELAPSED TIME (HOURS)

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. SIDE PANELS ON THE PYLONS 1 AND 2 POST SB No. A310−54−2024

024 6 1357 8

B_SB_542018_5_ADAA_01_00 Figure A-FADAA - Sheet 01

Elapsed Time Assumption DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 4 5

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# @A310 SERVICE BULLETIN Appendix 05: Elapsed Time Assumption

**CONF ALL

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A310−54−2018**

SB ELAPSED TIME (HOURS) GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 58.00 14.50 STEPS

6.00 1.50

5 10 0 REPAIR THE SIDE PANEL 46.00 11.50

CLOSE−UP 6.00 1.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01

02 **NOTE:** PER

4

4

4

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. OF THE PYLON

15

B_SB_542018_5_AEAA_01_00 Figure A-FAEAA - Sheet 01 Elapsed Time Assumption DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 5 5

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# @A310 SERVICE BULLETIN REPORTING SHEET 

### TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. MODIFICATION No.: None Please complete the appropriate item (A or B): A - SB WILL BEembodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEENembodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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# @A310 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018 REVISION No.: 03 - Apr 11/13 Page: 1 5

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