@A300

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.A300-54-0075

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 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

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

MANPOWER 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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

5

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@A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

Material Effectivity 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

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

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

WEIGHT AND BALANCE Minor editorial or document structure change N

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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@A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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 540075A01R02 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

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 540075- 832-801-001-Inspection

Pre Repair and Pre Service Bulletin No.

A300-54-0081

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

Subtask 540075-910-001-001 Minor editorial or document structure change N

Subtask 540075-839-001-001 Minor editorial or document structure change N

Subtask 540075-910-001-001 Minor editorial or document structure change N

Subtask 540075-839-001-001 Minor editorial or document structure change N

Subtask 540075-910-001-001 Minor editorial or document structure change N

Subtask 540075-839-001-001 Minor editorial or document structure change N

Subtask 540075-941-001-001 Minor editorial or document structure change N

Subtask 540075-941-001-001 Minor editorial or document structure change N

Subtask 540075-941-001-001 Minor editorial or document structure change N

Subtask 540075-832-004-001 Minor editorial or document structure change N

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

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@A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 540075-832-004-001 Minor editorial or document structure change N

Subtask 540075-832-004-001 Minor editorial or document structure change N

Subtask 540075-942-002-001 Minor editorial or document structure change N

Subtask 540075-942-002-001 Minor editorial or document structure change N

Subtask 540075-942-002-001 Minor editorial or document structure change N

TASK 540075- 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

Subtask 540075-910-002-001 Minor editorial or document structure change N

Subtask 540075-839-002-001 Minor editorial or document structure change N

Subtask 540075-910-002-001 Minor editorial or document structure change N

Subtask 540075-839-002-001 Minor editorial or document structure change N

Subtask 540075-910-002-001 Minor editorial or document structure change N

Subtask 540075-839-002-001 Minor editorial or document structure change N

Subtask 540075-941-003-001 Minor editorial or document structure change N

Subtask 540075-941-003-001 Minor editorial or document structure change N

Subtask 540075-941-003-001 Minor editorial or document structure change N

Subtask 540075-832-002-001 Minor editorial or document structure change N

Subtask 540075-832-002-001 Minor editorial or document structure change N

Subtask 540075-832-002-001 Minor editorial or document structure change N

Subtask 540075-942-003-001 Minor editorial or document structure change N

Subtask 540075-942-003-001 Minor editorial or document structure change N

Subtask 540075-942-003-001 Minor editorial or document structure change N

TASK 540075- 832-803-001-Inspection

Post Service Bulletin No. A300-54-0081

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

Subtask 540075-910-003-001 Minor editorial or document structure change N

Subtask 540075-839-003-001 Minor editorial or document structure change N

Subtask 540075-910-003-001 Minor editorial or document structure change N

Subtask 540075-839-003-001 Minor editorial or document structure change N

Subtask 540075-910-003-001 Minor editorial or document structure change N

Subtask 540075-839-003-001 Minor editorial or document structure change N

Subtask 540075-941-004-001 Minor editorial or document structure change N

Subtask 540075-941-004-001 Minor editorial or document structure change N

Subtask 540075-941-004-001 Minor editorial or document structure change N

Subtask 540075-832-003-001 Minor editorial or document structure change N

Subtask 540075-832-003-001 Minor editorial or document structure change N

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

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@A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 540075-832-003-001 Minor editorial or document structure change N

Subtask 540075-942-004-001 Minor editorial or document structure change N

Subtask 540075-942-004-001 Minor editorial or document structure change N

Subtask 540075-942-004-001 Minor editorial or document structure change N

TASK 540075- 833-802-001-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

Subtask 540075-910-005-001 Minor editorial or document structure change N

Subtask 540075-839-004-001 Minor editorial or document structure change N

Subtask 540075-910-005-001 Minor editorial or document structure change N

Subtask 540075-839-004-001 Minor editorial or document structure change N

Subtask 540075-910-005-001 Minor editorial or document structure change N

Subtask 540075-839-004-001 Minor editorial or document structure change N

Subtask 540075-941-005-001 Minor editorial or document structure change N

Subtask 540075-941-005-001 Minor editorial or document structure change N

Subtask 540075-941-005-001 Minor editorial or document structure change N

Subtask 540075-833-016-001 Minor editorial or document structure change N

Subtask 540075-833-016-001 Minor editorial or document structure change N

Subtask 540075-833-016-001 Minor editorial or document structure change N

Subtask 540075-942-006-001 Minor editorial or document structure change N

Subtask 540075-942-006-001 Minor editorial or document structure change N

Subtask 540075-942-006-001 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. A300-54-0081

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Appendix 03: Inspection Report Post Service Bulletin No. A300-54-0081

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

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 andreplace R54610124 by SRM

54-10-00.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 6

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Aug 11/93

REVISION No.: 01 - Nov 09/07

REVISION No.: 02 - Jun 26/08

REVISION No. : 03 - Mar 27/13

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 7

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@A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 8

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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 visual and Eddy Current inspection of pylon side panels (upper

section) at rib8, in order to detect any crack.

This inspection will make it possible to detect crack propagation at an early stage, thus avoiding an

extensive repair.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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@A300

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 540075A01R02 1 3,910.00 Doubler

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 540075A01R02 1 3,910.00 Doubler

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 540075A01R02 1 3,910.00 Doubler

EFFECTIVITY

**CONF ALL

This Service Bulletin is applicable to this (these) operator(s) :

72U ABR AFG F2I FLM IRA IRM MIX MSR NTR RUN

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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@A300

SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

Task 540075-832-802-001: Inspection Post Repair

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-833-802-001: Repair

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

**CONF 002

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

Task 540075-832-802-001: Inspection Post Repair

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-833-802-001: Repair

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

**CONF 003

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

Task 540075-832-802-001: Inspection Post Repair

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

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@A300

SERVICE BULLETIN

SUMMARY

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-833-802-001: Repair

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

APPENDICES

**CONF ALL

Appendix 01: Inspection Report Pre Repair and Pre Service Bulletin No. A300-54-0081

Appendix 02: Inspection Report Post Repair

Appendix 03: Inspection Report Post Service Bulletin No. A300-54-0081

Appendix 04: Non Destructive Testing Procedure

Appendix 05: Elapsed Time assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

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@A300

SERVICE BULLETIN

SUMMARY

**CONF ALL

AREAS TO BE

INSPECTED

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

A_SB_540075_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

Pre Repair and Pre SB No.A300-54-0081

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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@A300

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

A_SB_540075_5_SBAA_01_01

Figure A-FSBAA - Sheet 01

Post Repair

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 6

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@A300

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

A_SB_540075_5_SCAA_01_00

Figure A-FSCAA - Sheet 01

Post SB No. A300-54-0081

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 7

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 8

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

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.

No. 02434S3600 (NEW ENGINE PYLON-COMMON PARTS) is embodied or

Mod. No. 03599D9179 (REFERENCE MODIFICATION FOR ST2 (SN 207) is

embodied on one or both pylons.

(1) Models

B2-203 B2K-3C B4-103 B4-120 B4-203

(2) Effectivity by MSN

0079 0094 0128 0133 0135-0136 0154-0156 0160 0170 0173 0175-0176 0180

0183-0185 0187 0189 0199-0200 0203-0204 0226 0244

(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.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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@A300

SERVICE BULLETIN

OPERATOR MSN

72U 0079

ABR 0184 0189 0199

AFG 0180

F2I 0094 0128 0133 0135 0136 0156 0170

FLM 0176

IRA 0173 0185 0187 0226

IRM 0160 0175 0204 0244

MIX 0203

MSR 0200

NTR 0155

RUN 0154 0183

(4) Configuration by MSN

MSN CONFIGURATION

0079 0094 0128 0133 0135 0136 0156 0170 0184 0189 002

0154 0155 0173 0175 0180 0183 0199 0200 0203 0204 003

0160 0176 0185 0187 0226 0244 001

(5) Configuration definition

**CONF 001

Config. 001 is valid for A300 B2 aircraft.

**CONF 002

Config. 002 is valid for A300 B4-100 aircraft.

**CONF 003

Config. 003 is valid for A300 B4-200 aircraft.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 540075A01R02 1

Consumable CMLA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 540075A01R02 1

Consumable CMLA01 1

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 540075A01R02 1

Consumable CMLA01 1

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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@A300

SERVICE BULLETIN

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

On aircraft fitted with GE pylon, cracks have been reported on pylon side panels (upper

section) at rib8. The crack is starting from the hole at the top edge of the panel and

running up and downwards from this fastener hole.

(2) Objective/Action

This Service Bulletin requires a detailed visual and Eddy Current inspection of pylon side

panels (upper section) at rib8, in order to detect any crack.

(3) Advantages

This inspection will make it possible to detect crack propagation at an early stage, thus

avoiding an extensive repair.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

(1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair

and pre SB A300-54-0081

Task 540075-832-802-001: Inspection Post Repair

(1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2

Post-repair

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

(1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2

Post Service Bulletin No. A300-54-0081

Task 540075-833-802-001: Repair

(1) Repair

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

5

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@A300

SERVICE BULLETIN

**CONF 002

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

(1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair

and pre SB A300-54-0081

Task 540075-832-802-001: Inspection Post Repair

(1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2

Post-repair

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

(1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2

Post Service Bulletin No. A300-54-0081

Task 540075-833-802-001: Repair

(1) Repair

**CONF 003

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

(1) Do a Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Pre-repair

and pre SB A300-54-0081

Task 540075-832-802-001: Inspection Post Repair

(1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2

Post-repair

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

(1) Do a Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2

Post Service Bulletin No. A300-54-0081

Task 540075-833-802-001: Repair

(1) Repair

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

(2) Accomplishment Timescale

**CONF 001

This Service Bulletin has been classified mandatory by the issue of an Airworthiness

Directive No.Airworthiness Directive No. 2008-0181 published by the European Aviation

Safety Agency (EASA). The AD must be used as the reference document for 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. A300-54-0081

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Config.001 Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

5,350 FC None None

Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

None None 4,300 FC

Or

Apply SB

A300-54-0081

Before next flight None None

No crack found

and apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

Refer to table 3

Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

None None 4,300 FC

Or

Apply SB

A300-54-0081

Before next flight None None

Crack found but

not confirmed with

HFEC Inspection

and apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

Refer to table 3

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 5

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

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. A300-54-0081

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Apply TASK

540075-833-802

001 Repair

Crack found <20 Before 1000 FC None None

mm (0.787 in.) and

its length

confirmed with

Eddy current

inspection.

and apply TASK

540075-832-802

001 Inspection

Post Repair

Refer to table 2

Crack found >=20

mm (0.787 in.)

Contact Airbus Before next flight None None

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

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

Condition Action Compliance Time

Threshold (FH or

FC whichever

occurs first)

Grace period

Repetitive Interval

(FH or FC

whichever occurs

first)

Conf.001 Apply TASK

540075-832-802

001 Inspection

Post Repair

11,700 FC /13,300

FH from repair

embodiment

2,000 FC See

NOTE (*)

None

No crack found Apply SUBTASK

540075-832-002

001 Do a Special

Detailed Inspection

of the LH/RH side

Panels on the

Pylons 1 and 2

Post-repair

None None 3,700 FC /4,200

FH

Crack found Contact Airbus Before next flight None None

NOTE (*): For aircraft that have already exceeded or are close to exceed the threshold or the

scheduled interval, the inspection is to be accomplished within 2,000 FC after receipt of this Inspection

Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB.

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 6

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

Table 3: Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service

Bulletin No. A300-54-0081

Condition Action Compliance Time

Threshold (FH or

FC whichever

occurs first)

Grace period

Repetitive Interval

(FH or FC

whichever occurs

first)

Conf.001 Apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

10,400 FC /11,700

FH from SB No.

A300-54-0081

accomplishment

1,000 FC see

NOTE (*)

500 FC see NOTE

(**)

None

No crack found Apply SUBTASK

540075-832-003

001 Do a Special

Detailed Inspection

of the LH/RH side

Panels on the

Pylons 1 and 2

Post Service

Bulletin No.

A300-54-0081

None None 3,700 FC /4,200

FH

Crack found Contact Airbus Before next flight None None

NOTE (*): A300 aircraft with SB A300-54-0081 applied with less than 20,900 FC from Service Bulletin

accomplishment:

For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval,

the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin

(ISB) without exceeding the requirements of previous issue of this ISB.

NOTE (**): A300 aircraft with SB A300-54-0081 applied with more than 20,900 FC from Service

Bulletin accomplishment:

For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval,

the inspection is to be accomplished within 500 FC after receipt of this Inspection Service Bulletin

(ISB) without exceeding the requirements of previous issue of this ISB.

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

**CONF 002

This Service Bulletin has been classified mandatory by the issue of an Airworthiness

Directive No.Airworthiness Directive No. 2008-0181 published by the European Aviation

Safety Agency (EASA). The AD must be used as the reference document for the

mandated accomplishment timescale.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 7

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

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. A300-54-0081

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Config.002 Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

5,350 FC None None

Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

None None 4,300 FC

Or

Apply SB

A300-54-0081

Before next flight None None

No crack found

and apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

Refer to table 3

Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

None None 4,300 FC

Or

Apply SB

A300-54-0081

Before next flight None None

Crack found but

not confirmed with

HFEC Inspection

and apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

Refer to table 3

Apply TASK

540075-833-802

001 Repair

Crack found <20 Before 1000 FC None None

mm (0.787 in.) and

its length

confirmed with

Eddy current

inspection

and apply TASK

540075-832-802

001 Inspection

Post Repair

Refer to table 2

Crack found >=20

mm (0.787 in.)

Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 8

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

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

Threshold (FC or

FH whichever

occurs first)

Conf.002 Apply TASK

540075-832-802

001 Inspection

Post Repair

11,700 FC /16,100

FH from repair

embodiment

2,000 FC see

NOTE (*)

None

No crack found Apply SUBTASK

540075-832-002

001 Do a Special

Detailed Inspection

of the LH/RH side

Panels on the

Pylons 1 and 2

Post-repair

None None 3,700 FC /5,100

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

scheduled interval, the inspection is to be accomplished within 2,000 FC after receipt of this Inspection

Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB.

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

Table 3: Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service

Bulletin No. A300-54-0081

Condition Action Compliance Time

Threshold (FH or

FC whichever

occurs first)

Grace period

Repetitive Interval

(FH or FC

whichever occurs

first)

Conf.002 Apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

10,400 FC /14,200

FH from SB No.

A300-54-0081

accomplishment

1,000 FC see

NOTE (*)

500 FC see NOTE

(**)

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 9

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

Table 3: Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service

Bulletin No. A300-54-0081

Condition Action Compliance Time

Threshold (FH or

FC whichever

occurs first)

Grace period

Repetitive Interval

(FH or FC

whichever occurs

first)

No crack found Apply SUBTASK

540075-832-003

001 Do a Special

Detailed Inspection

of the LH/RH side

Panels on the

Pylons 1 and 2

Post Service

Bulletin No.

A300-54-0081

None None 3,700 FC /5,100

FH

Crack found Contact Airbus Before next flight None None

NOTE (*): A300 aircraft with SB A300-54-0081 applied with less than 20,900 FC from Service Bulletin

accomplishment:

For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval,

the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin

(ISB) without exceeding the requirements of previous issue of this ISB.

NOTE (**): A300 aircraft with SB A300-54-0081 applied with more than 20,900 FC from Service

Bulletin accomplishment:

For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval,

the inspection is to be accomplished within 500 FC after receipt of this Inspection Service Bulletin

(ISB) without exceeding the requirements of previous issue of this ISB.

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

**CONF 003

This Service Bulletin has been classified mandatory by the issue of an Airworthiness

Directive No.Airworthiness Directive No. 2008-0181 published by the European Aviation

Safety Agency (EASA). The AD must be used as the reference document for the

mandated accomplishment timescale.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 10

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

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. A300-54-0081

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Config.003 Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

5,350 FC None None

Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

None None 4,300 FC

Or

Apply SB

A300-54-0081

Before next flight None None

No crack found

and apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

Refer to table 3

Apply TASK

540075-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-0081

None None 4,300 FC

Or

Apply SB

A300-54-0081

Before next flight None None

Crack found but

not confirmed with

HFEC Inspection

and apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081

Refer to table 3

Apply TASK

540075-833-802

001 Repair

Crack found <20 Before 1000 FC None None

mm (0.787 in.) and

its length

confirmed with

Eddy current

inspection.

and apply TASK

540075-832-802

001 Inspection

Post Repair

Refer to table 2

Crack found >=20

mm (0.787 in.)

Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 11

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

Table 2: Special 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:11,800 FC from

repair embodiment

Conf.003 Apply TASK

540075-832-802

001 Inspection

Post Repair LR:11,700 FC

/26,700 FH from

repair embodiment

2,000 FC see

NOTE (*)

None

SR:4,000 FC

/5,500 FH

No crack found Apply SUBTASK

540075-832-002

001 Do a Special

Detailed Inspection

of the LH/RH side

Panels on the

Pylons 1 and 2

Post-repair

None None

LR:3,700 FC

/8,400 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

scheduled interval, the inspection is to be accomplished within 2,000 FC after receipt of this Inspection

Service Bulletin (ISB) without exceeding the requirements of previous issue of this ISB.

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 12

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

Table 3: Special Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service

Bulletin No. A300-54-0081

Condition Action Compliance Time

Threshold (FH or

FC whichever

occurs first)

Grace period

Repetitive Interval

(FH or FC

whichever occurs

first)

SR:11,200 FC

/15,400 FH from

SB No.

A300-54-0081

accomplishment

Conf.003 Apply TASK

540075-832-803

001 Inspection

Post Service

Bulletin No.

A300-54-0081 LR:10,400 FC

/23,600 FH from

SB No.

A300-54-0081

accomplishment

1,000 FC see

NOTE (*)

500 FC see NOTE

(**)

None

SR:4,000 FC

/5,500 FH

No crack found Apply SUBTASK

540075-832-003

001 Do a Special

Detailed Inspection

of the LH/RH side

Panels on the

Pylons 1 and 2

Post Service

Bulletin No.

A300-54-0081

None None

LR:3,700 FC

/8,400 FH

Crack found Contact Airbus Before next flight None None

NOTE (*): A300 aircraft with SB A300-54-0081 applied with less than 20,900 FC from Service Bulletin

accomplishment:

For aircraft that have already exceeded or are close to exceed the threshold or the scheduled interval,

the inspection is to be accomplished within 1,000 FC after receipt of this Inspection Service Bulletin

(ISB) without exceeding the requirements of previous issue of this ISB.

NOTE (**): A300 aircraft with SB A300-54-0081 applied with more than 20,900 FC from Service

Bulletin accomplishment:

For aircraft that have already exceeded or are close to exceed the threshold or the sheduled interval,

the inspection is to be accomplished within 500 FC after receipt of this Inspection Service Bulletin

(ISB) without exceeding the requirements of previous issue of this ISB.

NOTE: A300 B2 aircraft model concerns aircraft models A300 B2-203, A300

B2K-3C.

NOTE: A300 B4-100 aircraft model concerns aircraft models A300 B4-103, A300

B4-120.

NOTE: A300 B4-200 aircraft model concerns aircraft models A300 B4-203.

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 13

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

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 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

Get Access 6.00

On Aircraft

Do a Detailed Inspection of the LH/RH side Panels on

the Pylons 1 and 2 Pre-repair and pre SB

A300-54-0081

4.00

Close-Up 6.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

Task 540075-832-802-001: Inspection Post Repair

Get Access 6.00

On Aircraft

Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post-repair

18.00

Close-Up 6.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

Get Access 6.00

On Aircraft

Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post Service Bulletin No.

A300-54-0081

18.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 14

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

Close-Up 6.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-833-802-001: Repair

Get Access 6.00

On Aircraft

Repair 46.00

Close-Up 6.00

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

**CONF 002

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

Get Access 6.00

On Aircraft

Do a Detailed Inspection of the LH/RH side Panels on

the Pylons 1 and 2 Pre-repair and pre SB

A300-54-0081

4.00

Close-Up 6.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

Task 540075-832-802-001: Inspection Post Repair

Get Access 6.00

On Aircraft

Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post-repair

18.00

Close-Up 6.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

Get Access 6.00

On Aircraft

Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post Service Bulletin No.

A300-54-0081

18.00

Close-Up 6.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-833-802-001: Repair

Get Access 6.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 15

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300

SERVICE BULLETIN

Task 540075-833-802-001: Repair

On Aircraft

Repair 46.00

Close-Up 6.00

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

**CONF 003

Task 540075-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

Get Access 6.00

On Aircraft

Do a Detailed Inspection of the LH/RH side Panels on

the Pylons 1 and 2 Pre-repair and pre SB

A300-54-0081

4.00

Close-Up 6.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

Task 540075-832-802-001: Inspection Post Repair

Get Access 6.00

On Aircraft

Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post-repair

18.00

Close-Up 6.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-832-803-001: Inspection Post Service Bulletin No. A300-54-0081

Get Access 6.00

On Aircraft

Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post Service Bulletin No.

A300-54-0081

18.00

Close-Up 6.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

Task 540075-833-802-001: Repair

Get Access 6.00

On Aircraft

Repair 46.00

Close-Up 6.00

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 16

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SERVICE BULLETIN

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001 thru 002

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

For TASK 540075-833-802 001 Repair:

Manufacturers Empty Weight +0.85 KG (+1.8739 LB)

Effect on Balance +23.15 KGM (+167.44 LB.FT )

**CONF 003

Not Changed

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Airworthiness Directive (AD) Airworthiness Directive No.

2008-0181

Aircraft Maintenance Manual (AMM) 06-21-00 06-21-54 20-31-00

24-00-00 24-41-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-55-00

Non Destructive Test Manual (NTM) 51-31-11 51-40-00 54-40-03

Service Bulletin (SB) A300-54-0081

Standards Manual (SM)

Structural Repair Manual (SRM) 54-10-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

Service Bulletin No. A300-54-0081

**CONF 002

Airworthiness Directive (AD) Airworthiness Directive No.

2008-0181

Aircraft Maintenance Manual (AMM) 06-21-00 06-21-54 20-31-00

24-00-00 24-41-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-55-00

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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SERVICE BULLETIN

Non Destructive Test Manual (NTM) 51-31-11 51-40-00 54-40-03

Service Bulletin (SB) A300-54-0081

Standards Manual (SM)

Structural Repair Manual (SRM) 54-10-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

Service Bulletin No. A300-54-0081

**CONF 003

Airworthiness Directive (AD) Airworthiness Directive No.

2008-0181

Aircraft Maintenance Manual (AMM) 06-21-00 06-21-54 20-31-00

24-00-00 24-41-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-55-00

Non Destructive Test Manual (NTM) 51-31-11 51-40-00 54-40-03

Service Bulletin (SB) A300-54-0081

Standards Manual (SM)

Structural Repair Manual (SRM) 54-10-00

Service Bulletin No. A300-54-0081

**CONF ALL

K. PUBLICATION AFFECTED

Maintenance Planning Document (MPD) 543002-0602-4/5

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 18

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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 540075A01R02 AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 2590

For ordering by E-mail: airbus.kit@airbus.com

(2) Price and Availability

Kit 540075A01R02

Cost 3,910.00 USD

Availability 90 calendar days from receipt of order

The 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 540075A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

A5461255220000 1 Doubler

A5461255220100 1 Doubler

A5461255320000 8 Washer

A5461255420000 6 Washer

ASNA2314-4-13 6 Screw

ASNA2314-6-14 4 Screw

ASNA2314-6-16 8 Screw

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 19

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

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.

A300-54-0081, equipment and material for control by eddy current as per NTM

54-40-03 Part 6.

- For inspection program during accomplishment of repair, equipment and material for

control by eddy current as per NTM 51-31-11 Part 1.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 20

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SERVICE BULLETIN

(2) Tools

None

(3) Special Tools

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 21

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This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 22

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 540075-832-801-001 - Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE, TO DO

THIS :

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 23

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SERVICE BULLETIN

**CONF 003

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 4.00

**CONF ALL

A. GENERAL

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 540075-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 24

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SERVICE BULLETIN

(2) Subtask 540075-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF 002

(1) Subtask 540075-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

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 540075-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 25

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SERVICE BULLETIN

**CONF 003

(1) Subtask 540075-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

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 540075-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 540075-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 26

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-54, 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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF 002

(1) Subtask 540075-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 27

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SERVICE BULLETIN

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF 003

(1) Subtask 540075-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 540075-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels

on the Pylons 1 and 2 Pre-repair and pre SB A300-54-0081

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413EL , Panel 413DL, Panel

414DR or 414ER , Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 28

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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) 51-31-11

51-40-00 Part 1

Service Bulletin (SB) A300-54-0081

Fig. A-FBAAA

Inspection Area: Pre Repair and Pre

Service Bulletin No. A300-54-0081

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, refer to NTM 51-40-00 Part 1 of the side panels on the

Pylons 1 and 2 in the upper section at rib 8.

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

1 If no crack is found:

a Re-inspect the area as described in TASK 540075-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the

interval given in PLANNING INFORMATION Paragraph E.(2).

or

b Accomplish Service Bulletin No.A300-54-0081

and

Do a Special Detailed Inspection as described in TASK 540075-832-803

001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold

given in PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

- Confirm crack length with High Frequency Eddy Current (HFEC)

Inspection (Refer to NTM 51-31-11).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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a If crack is not confirmed:

<1> Re-inspect the area as described in TASK 540075-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at

the interval given in PLANNING INFORMATION Paragraph E.(2).

or

<2> Accomplish Service Bulletin No.A300-54-0081

and

Do a Special Detailed Inspection as described in TASK

540075-832-803 001 Inspection Post Service Bulletin No.

A300-54-0081 at the threshold given in PLANNING INFORMATION

Paragraph E.(2).

b If crack < 20 mm (0.787 in.):

<1> Do the repair before 1000 flights cycles, refer to TASK

540075-833-802 001 Repair

and

Do a Special Detailed Inspection the area as described in TASK

540075-832-802 001 Inspection Post Repair at the threshold given

in PLANNING INFORMATION Paragraph E.(2).

c If crack >=20 mm (0.787 in.):

<1> Contact Airbus before next flight.

**CONF 002

(1) Subtask 540075-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels

on the Pylons 1 and 2 Pre-repair and pre SB A300-54-0081

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413EL , Panel 413DL, Panel

414DR or 414ER , Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 30

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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) 51-31-11

51-40-00 Part 1

Service Bulletin (SB) A300-54-0081

Fig. A-FBAAA

Inspection Area: Pre Repair and Pre

Service Bulletin No. A300-54-0081

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, refer to NTM 51-40-00 Part 1 of the side panels on the

Pylons 1 and 2 in the upper section at rib 8.

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

1 If no crack is found:

a Re-inspect the area as described in TASK 540075-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the

interval given in PLANNING INFORMATION Paragraph E.(2).

or

b Accomplish Service Bulletin No.A300-54-0081

and

Do a Special Detailed Inspection as described in TASK 540075-832-803

001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold

given in PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

- Confirm crack length with High Frequency Eddy Current (HFEC)

Inspection (Refer to NTM 51-31-11).

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a If crack is not confirmed:

<1> Re-inspect the area as described in TASK 540075-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at

the interval given in PLANNING INFORMATION Paragraph E.(2).

or

<2> Accomplish Service Bulletin No.A300-54-0081

and

Do a Special Detailed Inspection as described in TASK

540075-832-803 001 Inspection Post Service Bulletin No.

A300-54-0081 at the threshold given in PLANNING INFORMATION

Paragraph E.(2).

b If crack < 20 mm (0.787 in.):

<1> Do the repair before 1000 flights cycles, refer to TASK

540075-833-802 001 Repair

and

Do a Special Detailed Inspection the area as described in TASK

540075-832-802 001 Inspection Post Repair at the threshold given

in PLANNING INFORMATION Paragraph E.(2).

c If crack >=20 mm (0.787 in.):

<1> Contact Airbus before next flight.

**CONF 003

(1) Subtask 540075-832-004-001 - Do a Detailed Inspection of the LH/RH side Panels

on the Pylons 1 and 2 Pre-repair and pre SB A300-54-0081

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413EL , Panel 413DL, Panel

414DR or 414ER , Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 32

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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) 51-31-11

51-40-00 Part 1

Service Bulletin (SB) A300-54-0081

Fig. A-FBAAA

Inspection Area: Pre Repair and Pre

Service Bulletin No. A300-54-0081

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, refer to NTM 51-40-00 Part 1 of the side panels on the

Pylons 1 and 2 in the upper section at rib 8.

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

1 If no crack is found:

a Re-inspect the area as described in TASK 540075-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at the

interval given in PLANNING INFORMATION Paragraph E.(2).

or

b Accomplish Service Bulletin No.A300-54-0081

and

Do a Special Detailed Inspection as described in TASK 540075-832-803

001 Inspection Post Service Bulletin No. A300-54-0081 at the threshold

given in PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

- Confirm crack length with High Frequency Eddy Current (HFEC)

Inspection (Refer to NTM 51-31-11).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 33

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a If crack is not confirmed:

<1> Re-inspect the area as described in TASK 540075-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-0081 at

the interval given in PLANNING INFORMATION Paragraph E.(2).

or

<2> Accomplish Service Bulletin No.A300-54-0081

and

Do a Special Detailed Inspection as described in TASK

540075-832-803 001 Inspection Post Service Bulletin No.

A300-54-0081 at the threshold given in PLANNING INFORMATION

Paragraph E.(2).

b If crack < 20 mm (0.787 in.):

<1> Do the repair before 1000 flights cycles, refer to TASK

540075-833-802 001 Repair

and

Do a Special Detailed Inspection the area as described in TASK

540075-832-802 001 Inspection Post Repair at the threshold given

in PLANNING INFORMATION Paragraph E.(2).

c If crack >=20 mm (0.787 in.):

<1> Contact Airbus before next flight.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 34

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**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 540075-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 002

(1) Subtask 540075-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 35

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SERVICE BULLETIN

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 003

(1) Subtask 540075-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 36

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SERVICE BULLETIN

Task 540075-832-802-001 - Inspection Post Repair

**CONF ALL

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 37

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SERVICE BULLETIN

**CONF 003

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF ALL

A. GENERAL

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 540075-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 38

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SERVICE BULLETIN

(2) Subtask 540075-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 540075-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

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 540075-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 39

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SERVICE BULLETIN

**CONF 003

(1) Subtask 540075-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

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 540075-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 540075-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 40

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-54, 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 413DL or413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF 002

(1) Subtask 540075-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 41

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SERVICE BULLETIN

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF 003

(1) Subtask 540075-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 540075-832-002-001 - Do a Special Detailed Inspection of the LH/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 413EL, Panel 413DL, Panel

414DR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 42

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SERVICE BULLETIN

Manpower Resources

Manhours 18.00

Minimum number of person 4

Subtask elapsed time 4.50

Skills AIRFRAME

NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-31-11

51-40-00 Part 1

Service Bulletin (SB) A300-54-0081

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBBAA

Inspection Area: Post Repair

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, (refer to NTM 51-40-00 Part 1) an HFEC Inspection, (refer

to NTM 51-31-11) 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 540075-832-802 001

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 540075-832-002-001 - Do a Special Detailed Inspection of the LH/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 413EL, Panel 413DL, Panel

414DR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 43

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SERVICE BULLETIN

Manpower Resources

Manhours 18.00

Minimum number of person 4

Subtask elapsed time 4.50

Skills AIRFRAME

NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-31-11

51-40-00 Part 1

Service Bulletin (SB) A300-54-0081

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBBAA

Inspection Area: Post Repair

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, (refer to NTM 51-40-00 Part 1) an HFEC Inspection, (refer

to NTM 51-31-11) 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 540075-832-802 001

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 540075-832-002-001 - Do a Special Detailed Inspection of the LH/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 413EL, Panel 413DL, Panel

414DR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 44

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SERVICE BULLETIN

Manpower Resources

Manhours 18.00

Minimum number of person 4

Subtask elapsed time 4.50

Skills AIRFRAME

NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-31-11

51-40-00 Part 1

Service Bulletin (SB) A300-54-0081

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBBAA

Inspection Area: Post Repair

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, (refer to NTM 51-40-00 Part 1) an HFEC Inspection, (refer

to NTM 51-31-11) 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 540075-832-802 001

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 45

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 540075-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 002

(1) Subtask 540075-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 46

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@A300

SERVICE BULLETIN

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 003

(1) Subtask 540075-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 47

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This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 48

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SERVICE BULLETIN

Task 540075-832-803-001 - Inspection Post Service Bulletin No. A300-54-0081

**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 413DL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL or 413DL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 49

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SERVICE BULLETIN

**CONF 003

Zone

From 410 to 420

Access

Panel 413CL or 413DL 413DL 414CR or 414EL 414DR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF ALL

A. GENERAL

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 540075-910-003-001 - 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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 50

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SERVICE BULLETIN

(2) Subtask 540075-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 540075-910-003-001 - 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 540075-839-003-001 - 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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 51

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@A300

SERVICE BULLETIN

**CONF 003

(1) Subtask 540075-910-003-001 - 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 540075-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 540075-941-004-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 52

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@A300

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-54, 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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF 002

(1) Subtask 540075-941-004-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 53

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@A300

SERVICE BULLETIN

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF 003

(1) Subtask 540075-941-004-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 540075-832-003-001 - Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413DL, Panel 413DL, Panel

414DR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 54

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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) 51-31-11

51-40-00 Part 1

54-40-03 Part 6

Service Bulletin (SB) A300-54-0081

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBCAA

Inspection Area: Post Service Bulletin

No. A300-54-0081

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, (refer to NTM 51-40-00 Part 1), an HFEC Inspection,

(refer to NTM 54-40-03 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 540075-832-803 001

Inspection Post Service Bulletin No. A300-54-0081 at the interval given in

PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

- Contact Airbus before next flight.

**CONF 002

(1) Subtask 540075-832-003-001 - Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413DL, Panel 413DL, Panel

414DR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 55

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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) 51-31-11

51-40-00 Part 1

54-40-03 Part 6

Service Bulletin (SB) A300-54-0081

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBCAA

Inspection Area: Post Service Bulletin

No. A300-54-0081

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, (refer to NTM 51-40-00 Part 1), an HFEC Inspection,

(refer to NTM 54-40-03 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 540075-832-803 001

Inspection Post Service Bulletin No. A300-54-0081 at the interval given in

PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

- Contact Airbus before next flight.

**CONF 003

(1) Subtask 540075-832-003-001 - Do a Special Detailed Inspection of the LH/RH side

Panels on the Pylons 1 and 2 Post Service Bulletin No. A300-54-0081

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413DL, Panel 413DL, Panel

414DR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 56

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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) 51-31-11

51-40-00 Part 1

54-40-03 Part 6

Service Bulletin (SB) A300-54-0081

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBCAA

Inspection Area: Post Service Bulletin

No. A300-54-0081

Sheet 01

At the threshold given in PLANNING INFORMATION paragraph E.(2)

(a) Do a detailed inspection, (refer to NTM 51-40-00 Part 1), an HFEC Inspection,

(refer to NTM 54-40-03 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 540075-832-803 001

Inspection Post Service Bulletin No. A300-54-0081 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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 57

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 540075-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 002

(1) Subtask 540075-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 58

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SERVICE BULLETIN

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 003

(1) Subtask 540075-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 59

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 60

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SERVICE BULLETIN

Task 540075-833-802-001 - 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.

IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DDR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DDR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 61

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SERVICE BULLETIN

**CONF 003

Zone

From 410 to 420

Access

Panel 413CL or 413EL 413DL 414CR or 414EL 414DDR or 414ER

423CL or 423EL 423DL 424CR or 424EL 424DR or 424ER

Manpower

TOTAL MANHOURS 58.00

ELAPSED TIME (HOURS) 14.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 540075-910-005-001 - 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) 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 540075-839-004-001 - Administrative

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 62

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SERVICE BULLETIN

**CONF 002

(1) Subtask 540075-910-005-001 - 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) 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 540075-839-004-001 - Administrative

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF 003

(1) Subtask 540075-910-005-001 - 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) 20-31-00, Page Block 001

Consumable Material List (CML)

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 63

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SERVICE BULLETIN

(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 540075-839-004-001 - Administrative

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 540075-941-005-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 64

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SERVICE BULLETIN

**CONF 002

(1) Subtask 540075-941-005-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF 003

(1) Subtask 540075-941-005-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 65

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SERVICE BULLETIN

(d) Remove the LH side access panels for the pylon 1, 413CL and 413DL or 413DL

and 413EL (Refer to AMM 06-21-54, Page Block 001).

(e) Remove the RH side access panels for the pylon 1, 414DR and 414CR or 414ER

and 414EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the LH side access panels for the pylon 2, 423CL and 423DL or 423DL

and 423EL (Refer to AMM 06-21-54, Page Block 001).

(g) Remove the RH side access panels for the pylon 2, 424DR and 424CR or 424ER

and 424EL (Refer to AMM 06-21-54, Page Block 001).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 540075-833-016-001 - Repair

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413EL, Panel 413DL, Panel

414DDR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

Manpower Resources

Manhours 46.00

Minimum number of person 4

Subtask elapsed time 11.50

Skills AIRFRAME

NON DESTRUCTIVE

TESTING

Material necessary to do the job

Kit 540075A01R02

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

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) 51-31-11

Structural Repair Manual (SRM) 54-10-00

(a) Perform repair in accordance with SRM 54-10-00.

(b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally

removed, refer to NTM 51-31-11.

(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 540075-832-802 001

Inspection Post Repair .

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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**CONF 002

(1) Subtask 540075-833-016-001 - Repair

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413EL, Panel 413DL, Panel

414DDR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

Manpower Resources

Manhours 46.00

Minimum number of person 4

Subtask elapsed time 11.50

Skills AIRFRAME

NON DESTRUCTIVE

TESTING

Material necessary to do the job

Kit 540075A01R02

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) 51-31-11

Structural Repair Manual (SRM) 54-10-00

(a) Perform repair in accordance with SRM 54-10-00.

(b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally

removed, refer to NTM 51-31-11.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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(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 540075-832-802 001

Inspection Post Repair .

**CONF 003

(1) Subtask 540075-833-016-001 - Repair

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413CL or 413EL, Panel 413DL, Panel

414DDR or 414ER, Panel 414CR or 414EL

Work location Rib 8

To 420 Access Panel 423CL or 423EL, Panel 423DL, Panel

424DR or 424ER, Panel 424CR or 424EL

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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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 540075A01R02

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) 51-31-11

Structural Repair Manual (SRM) 54-10-00

(a) Perform repair in accordance with SRM 54-10-00.

(b) Do a one time Eddy Current inspection of cut-out to ensure that the crack is totally

removed, refer to NTM 51-31-11.

(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.: A300-54-0075

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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 540075-832-802 001

Inspection Post Repair .

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 540075-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

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(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 002

(1) Subtask 540075-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

**CONF 003

(1) Subtask 540075-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-54, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

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(b) Install the LH side access panels for the pylon 1, 413CL and 413DL or 413DL and

413EL (Refer to AMM 06-21-54, Page Block 001).

(c) Install the RH side access panels for the pylon 1, 414DR and 414CR or 414ER and

414EL (Refer to AMM 06-21-54, Page Block 001).

(d) Install the LH side access panels for the pylon 2, 423CL and 423DL or 423DL and

423EL (Refer to AMM 06-21-54, Page Block 001).

(e) Install the RH side access panels for the pylon 2, 424DR and 424CR or 424ER and

424EL (Refer to AMM 06-21-54, Page Block 001).

(f) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 73

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**CONF ALL

AREAS TO BE

INSPECTED

LENGTH

FWD B

RIB8

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

A

A

B

B

A

RIB8

NOTES:

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A_SB_540075_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Inspection Area: Pre Repair and Pre Service Bulletin No. A300-54-0081

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 74

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**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

A_SB_540075_5_BBAA_01_01

Figure A-FBBAA - Sheet 01

Inspection Area: Post Repair

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 75

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**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

A

A

B

B

A

RIB8

NOTES:

ULTRASONIC

INSPECTION HOLE

ULTRASONIC

INSPECTION HOLE

DOUBLER

A_SB_540075_5_BCAA_01_01

Figure A-FBCAA - Sheet 01

Inspection Area: Post Service Bulletin No. A300-54-0081

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 76

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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 540075−832−801−001

AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

APPLY THE

SERVICE BULLETIN

A300−54−0081

(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 540075−832−801−001

REFER TO TASK 540075−832−802−001

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 540075−832−803−001

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 540075−833−802−001

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 540075−832−803−001

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 540075−832−802−001

A_SB_540075_5_FAAA_01_01

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 77

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This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 78

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SERVICE BULLETIN

Appendix 01: Inspection Report Pre Repair and Pre Service Bulletin No. A300-54-0081

**CONF ALL

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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Appendix 01: Inspection Report Pre Repair and Pre Service Bulletin No. A300-54-0081

**CONF ALL

AREAS TO BE

INSPECTED

LENGTH

FWD B

RIB8

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

A

A

B

B

A

RIB8

NOTES:

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A_SB_540075_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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Appendix 01: Inspection Report Pre Repair and Pre Service Bulletin No. A300-54-0081

**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 :

A300−54−0075

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 A300−54−0081

APPLIED

REPAIR

APPLIED

A_SB_540075_5_RAAA_02_01

Figure A-FRAAA - Sheet 02

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

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Appendix 01: Inspection Report Pre Repair and Pre Service Bulletin No. A300-54-0081

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

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SERVICE BULLETIN

Appendix 02: Inspection Report Post Repair

**CONF ALL

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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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

A

A

B

B

A

RIB8

NOTES:

ULTRASONIC

INSPECTION HOLE 2

ULTRASONIC

INSPECTION HOLE 1

CUT−OUT

DOUBLER

A_SB_540075_5_RBAA_01_01

Figure A-FRBAA - Sheet 01

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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Appendix 02: Inspection Report Post Repair

**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 :

A300−54−0075

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION

EDDY CURRENT

ULTRASONIC INSPECTION

NO

CRACK

RH SIDE

RH SIDE

DETAILED

INSPECTION

LH SIDE

LH SIDE

CRACK

LENGHT

LH

PYLON

RH

PYLON

EDDY CURRENT

INSPECTION

ULTRASONIC

INSPECTION

CRACK FOUND

(GIVE HOLE No.)

A_SB_540075_5_RBAA_02_02

Figure A-FRBAA - Sheet 02

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

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Appendix 02: Inspection Report Post Repair

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

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SERVICE BULLETIN

Appendix 03: Inspection Report Post Service Bulletin No. A300-54-0081

**CONF ALL

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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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SERVICE BULLETIN

Appendix 03: Inspection Report Post Service Bulletin No. A300-54-0081

**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

A

A

B

B

A

RIB8

NOTES:

ULTRASONIC

INSPECTION HOLE 2

ULTRASONIC

INSPECTION HOLE 1

DOUBLER

A_SB_540075_5_RCAA_01_01

Figure A-FRCAA - Sheet 01

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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Appendix 03: Inspection Report Post Service Bulletin No. A300-54-0081

**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 :

A300−54−0075

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION

EDDY CURRENT

ULTRASONIC INSPECTION

AFTER EMBODIMENT OF THE SERVICE BULLETIN No. A300−54−0081

NO

CRACK

RH SIDE

RH SIDE

DETAILED

INSPECTION

LH SIDE

LH SIDE

CRACK

LENGHT

LH

PYLON

RH

PYLON

EDDY CURRENT

INSPECTION

ULTRASONIC

INSPECTION

CRACK FOUND

(GIVE HOLE No.)

A_SB_540075_5_RCAA_02_01

Figure A-FRCAA - Sheet 02

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

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Appendix 03: Inspection Report Post Service Bulletin No. A300-54-0081

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area 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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_01_01

Figure A-FAAAA - Sheet 01

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_02_01

Figure A-FAAAA - Sheet 02

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

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Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_03_01

Figure A-FAAAA - Sheet 03

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_04_01

Figure A-FAAAA - Sheet 04

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_05_01

Figure A-FAAAA - Sheet 05

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 6

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_06_01

Figure A-FAAAA - Sheet 06

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 7

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_07_01

Figure A-FAAAA - Sheet 07

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 8

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_08_01

Figure A-FAAAA - Sheet 08

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 9

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_09_01

Figure A-FAAAA - Sheet 09

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 10

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_10_01

Figure A-FAAAA - Sheet 10

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 11

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

A_SB_540075_5_AAAA_11_00

Figure A-FAAAA - Sheet 11

Ultrasonic Inspection Procedure of lateral panel at RIB 8 area after doubler installation

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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SERVICE BULLETIN

Appendix 05: Elapsed Time assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−0075

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 A300−54−0081

A_SB_540075_5_ABAA_01_00

Figure A-FABAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 2

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SERVICE BULLETIN

Appendix 05: Elapsed Time assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−0075

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

30.00

7.50

STEPS

6.00 1.50

0

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)

24 6 8

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

1357

A_SB_540075_5_ACAA_01_00

Figure A-FACAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 3

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SERVICE BULLETIN

Appendix 05: Elapsed Time assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−0075

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

30.00

7.50

STEPS

6.00 1.50

0

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)

24 6 8

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 A300−54−0081

1357

A_SB_540075_5_ADAA_01_00

Figure A-FADAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 4

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SERVICE BULLETIN

Appendix 05: Elapsed Time assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−0075

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 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.

15

A_SB_540075_5_AEAA_01_00

Figure A-FAEAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 5

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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.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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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

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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

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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

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Comments:

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Please return this form to:

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CUSTOMER SERVICES DIRECTORATE

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31707 BLAGNAC CEDEX FRANCE

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FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-0075

REVISION No.: 03 - Mar 27/13 Page: 1

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