@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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 54

TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB

8.

MODIFICATION No.: None

This page transmits Revision No.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.

REASON

Revision 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

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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

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REVISION No.: 03 - Apr 11/13 Page: 2

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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

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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

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Subtask 542018-910-005-001 Minor editorial or document structure change N

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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

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REVISION No.: 03 - Apr 11/13 Page: 4

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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

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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

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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

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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

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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

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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

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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

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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.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 54

TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB

8.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

On aircraft fitted with GE pylon, cracks have been reported on pylon side panels (upper section) at rib8.

The crack is starting from the hole at the top edge of the panel and running up and downwards from

this fastener hole.

This Service Bulletin requires a detailed 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

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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

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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

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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

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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

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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

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SERVICE BULLETIN

SUMMARY

**CONF ALL

AREAS TO BE

INSPECTED

RIB8

FWD B

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

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SERVICE BULLETIN

SUMMARY

**CONF ALL

DETAILED INSPECTION AREA

RIB8

FWD B

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

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SERVICE BULLETIN

SUMMARY

**CONF ALL

DETAILED INSPECTION AREA

RIB8

FWD B

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

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 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

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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

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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

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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

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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

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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

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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

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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

Condition Action Compliance Time

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

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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

Condition Action Compliance Time

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

Crack found None None

<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.

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SERVICE BULLETIN

Table 2: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post-repair

Condition Action Compliance Time

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Crack found None None

<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

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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Crack found None None

<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

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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Crack found None None

<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

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

Crack found None None

<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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Crack found None None

<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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Crack found None None

<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

Condition Action Compliance Time

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

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

Condition Action Compliance Time

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

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

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

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

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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

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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

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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

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**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

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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

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This Page Intentionally Left Blank

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Kit 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

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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

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(2) Tools

None

(3) Special Tools

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 542018-832-801-001 - Inspection Pre Repair and 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

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**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

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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.

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(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.

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**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

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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

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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.

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(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

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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

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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 to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 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

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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

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 to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 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

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 to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 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 to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 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

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 to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 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

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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 to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 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).

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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

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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 to Fig. A-FBAAA Sheet 01 and Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 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).

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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

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**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.

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(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.

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(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.

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(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

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This Page Intentionally Left Blank

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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

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**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

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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.

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(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.

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**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

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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

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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.

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(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

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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

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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

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@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

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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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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.
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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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

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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

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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

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**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

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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

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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

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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

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(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

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**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

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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

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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

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(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

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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

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(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

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**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

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(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

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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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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 to Fig. A-FFAAA Sheet 01 and Fig. 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

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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

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(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

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(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

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(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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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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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

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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

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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

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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

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(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

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(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

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(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

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**CONF ALL

AREAS TO BE

INSPECTED

LENGTH

FWD B

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

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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

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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

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**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

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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 Department SEES2, on the attached inspection report sheet.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018

REVISION No.: 03 - Apr 11/13 Page: 1

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

**CONF ALL

AREAS TO BE

INSPECTED

LENGTH

FWD B

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

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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

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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

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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 Department SEES2, on the attached inspection report sheet.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018

REVISION No.: 03 - Apr 11/13 Page: 1

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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

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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

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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

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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 Department SEES2, on the attached inspection report sheet.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018

REVISION No.: 03 - Apr 11/13 Page: 1

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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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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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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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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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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

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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

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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

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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

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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

0 5 10

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

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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 BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Aug 11/93 SERVICE BULLETIN No.: A310-54-2018

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