@A300-600

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.A300-54-6015

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

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

APPENDICES Minor editorial or document structure change N

Fig. A-FSAAA Minor editorial or document structure change N

Fig. A-FSAAA Sheet 01 Minor editorial or document structure change N

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

Material Effectivity 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

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

WEIGHT AND BALANCE Minor editorial or document structure change N

Minor editorial or document structure change N

ELECTRICAL LOAD DATA Minor editorial or document structure change N

REFERENCES Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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 546015A01R02 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

ACCOMPLISHMENT INSTRUCTIONS

TASK 546015- 832-801-001-Inspection

Pre Repair and Pre Service Bulletin No.

A300-54-6021

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

Subtask 546015-910-001-001 Minor editorial or document structure change N

Subtask 546015-839-001-001 Minor editorial or document structure change N

Subtask 546015-910-001-001 Minor editorial or document structure change N

Subtask 546015-839-001-001 Minor editorial or document structure change N

Subtask 546015-941-001-001 Minor editorial or document structure change N

Subtask 546015-941-001-001 Minor editorial or document structure change N

Subtask 546015-832-004-001 Minor editorial or document structure change N

Subtask 546015-832-004-001 Minor editorial or document structure change N

Subtask 546015-942-001-001 Minor editorial or document structure change N

Subtask 546015-942-001-001 Minor editorial or document structure change N

TASK 546015- 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

Subtask 546015-910-002-001 Minor editorial or document structure change N

Subtask 546015-839-003-001 Minor editorial or document structure change N

Subtask 546015-910-002-001 Minor editorial or document structure change N

Subtask 546015-839-003-001 Minor editorial or document structure change N

Subtask 546015-941-003-001 Minor editorial or document structure change N

Subtask 546015-941-003-001 Minor editorial or document structure change N

Subtask 546015-832-003-001 Minor editorial or document structure change N

Subtask 546015-832-003-001 Minor editorial or document structure change N

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 546015-942-003-001 Minor editorial or document structure change N

Subtask 546015-942-003-001 Minor editorial or document structure change N

TASK 546015- 832-804-001-Inspection

Post Service Bulletin No. A300-54-6021

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

Subtask 546015-910-003-001 Minor editorial or document structure change N

Subtask 546015-839-004-001 Minor editorial or document structure change N

Subtask 546015-910-003-001 Minor editorial or document structure change N

Subtask 546015-839-004-001 Minor editorial or document structure change N

Subtask 546015-941-004-001 Minor editorial or document structure change N

Subtask 546015-941-004-001 Minor editorial or document structure change N

Subtask 546015-832-002-001 Minor editorial or document structure change N

Subtask 546015-832-002-001 Minor editorial or document structure change N

Subtask 546015-942-004-001 Minor editorial or document structure change N

Subtask 546015-942-004-001 Minor editorial or document structure change N

TASK 546015- 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

Subtask 546015-910-004-001 Minor editorial or document structure change N

Subtask 546015-839-002-001 Minor editorial or document structure change N

Subtask 546015-910-004-001 Minor editorial or document structure change N

Subtask 546015-839-002-001 Minor editorial or document structure change N

Subtask 546015-941-002-001 Minor editorial or document structure change N

Subtask 546015-941-002-001 Minor editorial or document structure change N

Subtask 546015-833-020-001 Minor editorial or document structure change N

Subtask 546015-833-020-001 Minor editorial or document structure change N

Subtask 546015-942-002-001 Minor editorial or document structure change N

Subtask 546015-942-002-001 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. A300-54-6021

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-FRAAA Sheet 02 Minor editorial or document structure change N

Appendix 02 - Inspection Report Post repair

APPENDIX CONTENT Minor editorial or document structure change N

Fig. A-FRBAA Minor editorial or document structure change N

Fig. A-FRBAA Sheet 01 Minor editorial or document structure change N

Fig. A-FRBAA Sheet 02 Minor editorial or document structure change N

Appendix 03 - Inspection Report Post Service Bulletin No. A300-54-6021

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.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to inform the operators that this Service Bulletin is rendered mandatory. The

thresholds and intervals have also been reviewed.

Revision No. 02 is issued to replace the PN ASNA2001 by ASNA2314 and replace R54610124 by SRM

54-51-31.

REVISION SEQUENCE

ORIGINAL: Aug 11/93

REVISION No. : 01 - Nov 09/07

REVISION No. : 02 - Jun 26/08

REVISION No. : 03 - Apr 11/13

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 6

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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 Rib

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

this fastener hole.

This Service Bulletin requires a detailed and Eddy Current inspection of pylon side panels (upper

section) at Rib 8, in order to detect any crack.

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

extensive repair.

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.: A300-54-6015

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

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@A300-600

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 546015A01R02 1 3,910.00 Doubler, Shim

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 546015A01R02 1 3,910.00 Doubler, Shim

EFFECTIVITY

**CONF ALL

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

14S 34Z 83V ABD ABR BCS CES F2I FDX G8E IRA IRM KAC

KAL MON MSR OHY QTR RLB RUN SUD TAR THA UZB

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.: A300-54-6015

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

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SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 546015-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 2.50

Task 546015-832-802-001: Inspection Post Repair

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-832-804-001: Inspection Post Service Bulletin No. A300-54-6021

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-833-802-001: Repair

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF 002

Task 546015-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 2.50

Task 546015-832-802-001: Inspection Post Repair

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-832-804-001: Inspection Post Service Bulletin No. A300-54-6021

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-833-802-001: Repair

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

APPENDICES

**CONF ALL

Appendix 01 - Inspection Report Pre repair and Pre Service Bulletin No. A300-54-6021

Appendix 02 - Inspection Report Post repair

Appendix 03 - Inspection Report Post Service Bulletin No. A300-54-6021

Appendix 04: Non Destructive Testing Procedure

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

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SERVICE BULLETIN

SUMMARY

Appendix 05: Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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SERVICE BULLETIN

SUMMARY

**CONF ALL

AREAS TO BE

INSPECTED

RIB8

FWD B

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

B

B

A

RIB8

NOTES:

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A

A

D_SB_546015_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

- Pre Repair and Pre SB No. A300-54-6021

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 5

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SUMMARY

**CONF ALL

DETAILED INSPECTION AREA

RIB8

FWD B

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

B

B

A

RIB8

NOTES:

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A

A

CUT−OUT

D_SB_546015_5_SBAA_01_00

Figure A-FSBAA - Sheet 01

- Post Repair

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 6

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SUMMARY

**CONF ALL

DETAILED INSPECTION AREA

RIB8

FWD B

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

B

B

A

RIB8

NOTES:

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A

A

D_SB_546015_5_SCAA_01_00

Figure A-FSCAA - Sheet 01

- Post SB No. A300-54-6021

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 7

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SUMMARY

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 8

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 54

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

8.

MODIFICATION No.: None

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: This Service Bulletin is only applicable to aircraft listed above on which Mod.

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

Mod No. 03599D9179 (REFERENCE MODIFICATION FOR ST2 (SN207)) is

embodied on one or both pylons.

NOTE: The modification No. 10432S20461 (NACELLES/PYLONS - PANELS IN THE

UPPER CORNER AT RIB 8 - ADD A DOUBLER (PRODUCTION

SOLUTION)) is embodied prior to delivery on aircraft MSN 0723 , 0725-0728 ,

0731 , 0733 and subsequent.

NOTE: This modification is partially embodied on aircraft MSN 0732 (only on the right

pylon).

NOTE: Aircraft with modification No. 10432S20461 (NACELLES/PYLONS - PANELS

IN THE UPPER CORNER AT RIB 8 - ADD A DOUBLER (PRODUCTION

SOLUTION)) embodied are not affected by this inspection.

(1) Models

B4-603 B4-605R B4-620 B4-622 B4-622R C4-620

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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SERVICE BULLETIN

(2) Effectivity by MSN

0284 0294 0301 0307 0312 0321 0336 0344 0348 0351 0358 0361 0365 0380 0388

0401 0405 0408 0411 0414 0417 0462 0464-0466 0477 0479 0505-0506 0509 0514

0516 0518 0521 0525 0529-0530 0532 0536 0540 0543 0546 0553-0561 0563 0566

0569 0572 0575 0577 0579 0581-0582 0584 0602-0605 0607-0611 0613-0614

0617-0618 0621 0623 0625-0633 0635 0637 0641 0643 0657 0659 0662 0664 0666

0668 0670 0673 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703

0705 0707 0709 0711 0713 0715 0717 0719 0721-0722 0724 0729-0730

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

14S 0609

34Z 0685 0692

83V 0466

ABD 0529 0557

ABR 0683

BCS 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730

CES 0521 0525 0532 0707

F2I 0284 0294 0301 0307 0312 0321 0336 0348 0351 0518 0610

FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559

0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664

0668 0688 0709 0713 0715

G8E 0462 0465 0506 0509 0514 0516

IRA 0632 0696

IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701

KAC 0344 0673 0694 0699 0719 0721

KAL 0582 0627 0631 0662

MON 0540 0556 0604 0605

MSR 0561 0607

OHY 0584 0603

QTR 0554 0560 0614

RLB 0626 0643

RUN 0677

SUD 0666

TAR 0505 0558 0563

THA 0464 0566 0569 0577 0628 0629 0635 0681 0705

UZB 0717 0722

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0284 0294 0301 0307 0312 0321 0336 0344 0348 0351 0358

0361 0365 0388 0417 0477 0479 0529 0530 0536 0543 0554

0555 0557 0559 0560 0561 0566 0569 0572 0575 0577 0579

0581 0582 0602 0607 0609 0611 0613 0614 0617 0621 0625

0627 0628 0629 0630 0631 0633 0635 0637 0641 0657 0659

0662 0664 0666 0668 0670 0677 0679 0681 0683 0685 0688

0692 0703 0705 0711 0717 0722 0724 0729 0730

002

0380 0401 0405 0408 0411 0414 0462 0464 0465 0466 0505

0506 0509 0514 0516 0518 0521 0525 0532 0540 0546 0553

0556 0558 0563 0584 0603 0604 0605 0608 0610 0618 0623

0626 0632 0643 0673 0694 0696 0699 0701 0707 0709 0713

0715 0719 0721

001

(5) Configuration definition

**CONF 001

Config. 001 concerns aircraft equipped with GE engine.

**CONF 002

Config. 002 concerns aircraft equipped with PW engine.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 546015A01R02 1

Consumable CMLA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 546015A01R02 1

Consumable CMLA01 1

**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 Rib 8. The crack is starting from the hole at the top edge of the panel and

running up and downwards from this fastener hole.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

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SERVICE BULLETIN

(2) Objective/Action

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

panels (upper section) at Rib 8, in order to detect any crack.

(3) Advantages

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

avoiding an extensive repair.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 546015-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

(1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylon 1 and 2 Pre

Repair and Pre SB No. A300-54-6021

Task 546015-832-802-001: Inspection Post Repair

(1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylon 1 and 2 Post

Repair

Task 546015-832-804-001: Inspection Post Service Bulletin No. A300-54-6021

(1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylon 1 and 2 Post

SB No. A300-54-6021

Task 546015-833-802-001: Repair

(1) Repair the Side Panel of the Pylon

**CONF 002

Task 546015-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

(1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylon 1 and 2 Pre

Repair and Pre SB No. A300-54-6021

Task 546015-832-802-001: Inspection Post Repair

(1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylon 1 and 2 Post

Repair

Task 546015-832-804-001: Inspection Post Service Bulletin No. A300-54-6021

(1) Do a Detailed Inspection of the LH and RH Side Panels on the Pylon 1 and 2 Post

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SB No. A300-54-6021

Task 546015-833-802-001: Repair

(1) Repair the Side Panel of the Pylon

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the thresholds and

intervals given below but reference should be made to the AD for confirmation of the

mandated accomplishment timescale.

Table 1: Detailed Inspection of the LH/RH Side Panels on the Pylon 1 and 2 Pre-repair and pre SB

No. A300-54-6021

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Config. 001 Apply TASK

546015-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-6021

4,200FC None None

Apply TASK

546015-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-6021

None None 3,600FC

Or

Apply SB

A300-54-6021

Before next flight None None

No crack found

and

Apply TASK

546015-832-804

001 Inspection

Post Service

Bulletin No.

A300-54-6021

Refer to table 3

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 5

5

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@A300-600

SERVICE BULLETIN

Table 1: Detailed Inspection of the LH/RH Side Panels on the Pylon 1 and 2 Pre-repair and pre SB

No. A300-54-6021

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Apply TASK

546015-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-6021

None None 3,600FC

Or

Apply SB

A300-54-6021

Before next flight None None

Crack found but

not confirmed with

HFEC inspection

and

Apply TASK

546015-832-804

001 Inspection

Post Service

Bulletin No.

A300-54-6021

Refer to table 3

Apply TASK

546015-833-802

001 Repair

Crack found <20 Before 1000FC None None

mm (0.787 in.) and

its length

confirmed with

eddy current

inspection.

and apply TASK

546015-832-802

001 Inspection

Post Repair

Refer to table 2

Crack found >=20

mm (0.787 in.) and

its length

confirmed with

eddy current

inspection.

Contact Airbus Before next flight None None

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

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

Config. 001 Apply TASK

546015-832-802

001 Inspection

Post Repair

9,300FC from

repair embodiment

2,000FC see

NOTE (*)

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 6

5

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@A300-600

SERVICE BULLETIN

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

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

For SR:

4,100FC / 6,200FH

No crack found Apply SUBTASK

546015-832-003

001 Do a Detailed

Inspection of the

LH and RH Side

Panels on the

Pylon 1 and 2 Post

Repair

None None

For LR:

3,800FC / 8,200FH

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 2,000FC after receipt of this Inspection

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

NOTE: For Average Time (AFT - limit between Short Range (SR) and Long

Range (LR) mission) configuration refer to ALI Document Section B.

Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.

A300-54-6021

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

Config. 001 Apply TASK

546015-832-804

001 Inspection

Post Service

Bulletin No.

A300-54-6021

10,100FC from SB

No. A300-54-6021

accomplishment

1,000FC see

NOTE (*)

500FC see NOTE

(**)

None

For SR:

4,100FC / 6,200FH

No crack found Apply SUBTASK

546015-832-002

001 Do a Detailed

Inspection of the

LH and RH Side

Panels on the

Pylon 1 and 2 Post

SB No.

A300-54-6021

None None

For LR:

3,800FC / 8,200FH

Crack found Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 7

5

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@A300-600

SERVICE BULLETIN

Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.

A300-54-6021

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

NOTE (*): For A300-600 with SB A300-54-6021 applied with less than 19,500FC:

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

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

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

NOTE (**): For A300-600 with SB A300-54-6021 applied with more than 19,500FC:

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

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

without exceeding the requirements of previous issue of this ISB.

NOTE: For Average Time (AFT - limit between Short Range (SR) and Long

Range (LR) mission) configuration refer to ALI Document Section B.

**CONF 002

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the thresholds and

intervals given below but reference should be made to the AD for confirmation of the

mandated accomplishment timescale.

Table 1: Detailed Inspection of the LH/RH Side Panels on the Pylon 1 and 2 Pre-repair and pre SB

No. A300-54-6021

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Config. 002 Apply TASK

546015-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-6021

4,200FC None None

Apply TASK

546015-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-6021

None None 3,600FC

Or

Apply SB

A300-54-6021

Before next flight None None

No crack found

and apply TASK

546015-832-804

001 Inspection

Post Service

Bulletin No.

A300-54-6021

Refer to table 3

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 8

5

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@A300-600

SERVICE BULLETIN

Table 1: Detailed Inspection of the LH/RH Side Panels on the Pylon 1 and 2 Pre-repair and pre SB

No. A300-54-6021

Condition Action Compliance Time

Threshold Grace period

Repetitive Interval

Apply TASK

546015-832-801

001 Inspection Pre

Repair and Pre

Service Bulletin

No. A300-54-6021

None None 3,600FC

Or

Apply SB

A300-54-6021

Before next flight None None

Crack found but

not confirmed with

HFEC inspection

and apply TASK

546015-832-804

001 Inspection

Post Service

Bulletin No.

A300-54-6021

Refer to table 3

Apply TASK

546015-833-802

001 Repair

Crack found <20 Before 1000FC None None

mm (0.787 in.) and

its length

confirmed with

eddy current

inspection.

and apply TASK

546015-832-802

001 Inspection

Post Repair

Refer to table 2

Crack found >=20

mm (0.787 in.) and

its length

confirmed with

eddy current

inspection.

Contact Airbus Before next flight None None

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

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

For SR:

9,300FC /

17,800FH from

repair embodiment

Config. 002 Apply TASK

546015-832-802

001 Inspection

Post Repair

For LR:

9,300FC /

23,700FH from

repair embodiment

2,000FC see

NOTE (*)

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 9

5

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@A300-600

SERVICE BULLETIN

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

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

For SR:

3,700FC / 5,600FH

No crack found Apply SUBTASK

546015-832-003

001 Do a Detailed

Inspection of the

LH and RH Side

Panels on the

Pylon 1 and 2 Post

Repair

None None

For LR:

3,400FC / 7,500FH

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 2,000FC after receipt of this Inspection

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

NOTE: For Average Time (AFT - limit between Short Range (SR) and Long

Range (LR) mission) configuration refer to ALI Document Section B.

Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.

A300-54-6021

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

For SR:

10,100FC /

15,700FH from SB

No. A300-54-6021

accomplishment

Config. 002 Apply TASK

546015-832-804

001 Inspection

Post Service

Bulletin No.

A300-54-6021 For LR:

9,700FC /

20,900FH from SB

No. A300-54-6021

accomplishment

1,000FC see

NOTE (*)

500FC see NOTE

(**)

None

For SR:

3,700FC / 5,600FH

No crack found Apply SUBTASK

546015-832-002

001 Do a Detailed

Inspection of the

LH and RH Side

Panels on the

Pylon 1 and 2 Post

SB No.

A300-54-6021

None None

For LR:

3,400FC / 7,500FH

Crack found Contact Airbus Before next flight None None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 10

5

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@A300-600

SERVICE BULLETIN

Table 3: Detailed Inspection of the LH/RH side Panels on the Pylons 1 and 2 Post Service Bulletin No.

A300-54-6021

Condition Action Compliance Time

Threshold (FC or

FH whichever

occurs first)

Grace period

Repetitive Interval

(FC or FH

whichever occurs

first)

NOTE (*): For A300-600 with SB A300-54-6021 applied with less than 19,500FC:

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

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

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

NOTE (**): For A300-600 with SB A300-54-6021 applied with more than 19,500FC:

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

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

without exceeding the requirements of previous issue of this ISB.

NOTE: For Average Time (AFT - limit between Short Range (SR) and Long

Range (LR) mission) configuration refer to ALI Document Section B.

**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 546015-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

Get Access 3.00

On Aircraft

Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Pre Repair and Pre SB

No. A300-54-6021

4.00

Close-Up 3.00

TOTAL MANHOURS 10.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Task 546015-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

ELAPSED TIME (HOURS) 2.50

Task 546015-832-802-001: Inspection Post Repair

Get Access 3.00

On Aircraft

Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post Repair

18.00

Close-Up 3.00

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-832-804-001: Inspection Post Service Bulletin No. A300-54-6021

Get Access 3.00

On Aircraft

Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post SB No.

A300-54-6021

18.00

Close-Up 3.00

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-833-802-001: Repair

Get Access 3.00

On Aircraft

Repair the Side Panel of the Pylon 24.00

Close-Up 3.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF 002

Task 546015-832-801-001: Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

Get Access 3.00

On Aircraft

Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Pre Repair and Pre SB

No. A300-54-6021

4.00

Close-Up 3.00

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 2.50

Task 546015-832-802-001: Inspection Post Repair

Get Access 3.00

On Aircraft

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 12

5

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@A300-600

SERVICE BULLETIN

Task 546015-832-802-001: Inspection Post Repair

Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post Repair

18.00

Close-Up 3.00

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-832-804-001: Inspection Post Service Bulletin No. A300-54-6021

Get Access 3.00

On Aircraft

Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post SB No.

A300-54-6021

18.00

Close-Up 3.00

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

Task 546015-833-802-001: Repair

Get Access 3.00

On Aircraft

Repair the Side Panel of the Pylon 24.00

Close-Up 3.00

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF ALL

H. WEIGHT AND BALANCE

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

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

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

For TASK 546015-833-802 001 Repair:

Manufacturers Empty Weight +0.85 KG (+1.8739 LB)

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

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-54 20-31-00 23-31-00

24-00-00 24-41-00

Consumable Material List (CML)

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

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

Non Destructive Test Manual (NTM) 51-10-20 51-70-00 54-50-34

Service Bulletin (SB) A300-54-6021

Standards Manual (SM)

Structural Repair Manual (SRM) 54-51-31

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-54 20-31-00 23-31-00

24-00-00 24-41-00

Consumable Material List (CML)

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

Non Destructive Test Manual (NTM) 51-10-20 51-70-00 54-50-34

Service Bulletin (SB) A300-54-6021

Standards Manual (SM)

Structural Repair Manual (SRM) 54-51-31

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Maintenance Planning Document (MPD) 545043-01-1

545043-01-2

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 14

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@A300-600

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 546015A01R02 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 546015A01R02

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 546015A01R02

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.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 15

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@A300-600

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

None

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 16

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@A300-600

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 546015-832-801-001 - Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021

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 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 2.50

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 2.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 17

5

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@A300-600

SERVICE BULLETIN

**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 546015-910-001-001 - 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) 23-31-00, Page Block 001

Consumable Material List (CML)

(a) For the specification of the material numbers (Mat. No.), refer to the CML.

(b) Clean the surfaces to seal with:

Solvent General

Purpose

11-026 As required

and refer to AMM 23-31-00, Page Block 001.

(2) Subtask 546015-839-001-001 - Administrative

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

Service Bulletin.

**CONF 002

(1) Subtask 546015-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 18

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

References

Aircraft Maintenance Manual (AMM) 23-31-00, Page Block 001

Consumable Material List (CML)

(a) For the specification of the material numbers (Mat. No.), refer to the CML.

(b) Clean the surfaces to seal with:

Solvent General

Purpose

11-026 As required

and refer to AMM 23-31-00, Page Block 001.

(2) Subtask 546015-839-001-001 - 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 546015-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 19

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@A300-600

SERVICE BULLETIN

(e) Put the access platforms in position.

**CONF 002

(1) Subtask 546015-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(e) Put the access platforms in position.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 546015-832-004-001 - Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Pre Repair and Pre SB No. A300-54-6021

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 20

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-20 Part 6

51-70-00 Part 7

Service Bulletin (SB) A300-54-6021

Fig. A-FBAAA

Inspection Area: Pre repair and Pre

Service Bulletin No. A300-54-6021

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

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

(a) Do a detailed inspection (Refer to NTM 51-70-00 Part 7) on pylon side panel (upper

section) at Rib 8.

Refer to Fig. A-FBAAA Sheet 01

Refer to Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 546015-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021 , at the

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

or

b Accomplish Service Bulletin No. A300-54-6021.

and

Do a detailed inspection as described in TASK 546015-832-804 001

Inspection Post Service Bulletin No. A300-54-6021 , at the threshold

given in PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

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

(Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 21

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SERVICE BULLETIN

a If crack is not confirmed:

<1> Re-inspect the area as described in TASK 546015-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021 ,

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

or

<2> Accomplish Service Bulletin No. A300-54-6021.

and

Do a detailed inspection as described in TASK 546015-832-804 001

Inspection Post Service Bulletin No. A300-54-6021 , at the threshold

given in PLANNING INFORMATION Paragraph E.(2).

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

<1> Do the repair before 1000FC, refer to TASK 546015-833-802 001

Repair .

and

Do a detailed inspection as described in TASK 546015-832-802

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 546015-832-004-001 - Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Pre Repair and Pre SB No. A300-54-6021

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 22

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-20 Part 6

51-70-00 Part 7

Service Bulletin (SB) A300-54-6021

Fig. A-FBAAA

Inspection Area: Pre repair and Pre

Service Bulletin No. A300-54-6021

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

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

(a) Do a detailed inspection (Refer to NTM 51-70-00 Part 7) on pylon side panel (upper

section) at Rib 8.

Refer to Fig. A-FBAAA Sheet 01

Refer to Fig. A-FFAAA Sheet 01

1 If no crack is found:

a Re-inspect the area as described in TASK 546015-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021 , at the

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

or

b Accomplish Service Bulletin No. A300-54-6021.

and

Do a detailed inspection as described in TASK 546015-832-804 001

Inspection Post Service Bulletin No. A300-54-6021 , at the threshold

given in PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

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

(Refer to NTM 51-10-20 Part 6).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 23

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SERVICE BULLETIN

a If crack is not confirmed:

<1> Re-inspect the area as described in TASK 546015-832-801 001

Inspection Pre Repair and Pre Service Bulletin No. A300-54-6021 ,

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

or

<2> Accomplish Service Bulletin No. A300-54-6021.

and

Do a detailed inspection as described in TASK 546015-832-804 001

Inspection Post Service Bulletin No. A300-54-6021 , at the threshold

given in PLANNING INFORMATION Paragraph E.(2).

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

<1> Do the repair before 1000FC, refer to TASK 546015-833-802 001

Repair .

and

Do a detailed inspection as described in TASK 546015-832-802

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 ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 546015-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 24

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@A300-600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

**CONF 002

(1) Subtask 546015-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 25

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 26

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@A300-600

SERVICE BULLETIN

Task 546015-832-802-001 - 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 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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@A300-600

SERVICE BULLETIN

**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 546015-910-002-001 - 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

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.), 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 546015-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 546015-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 28

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026

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.), 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 546015-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 546015-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 29

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@A300-600

SERVICE BULLETIN

(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(e) Put the access platforms in position.

**CONF 002

(1) Subtask 546015-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(e) Put the access platforms in position.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 546015-832-003-001 - Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post Repair

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 30

5

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@A300-600

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) 51-10-20 Part 6

51-70-00 Part 7

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBBAA

Inspection Area: Post repair

Sheet 01

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

(a) Do a detailed inspection (Refer to NTM 51-70-00 Part 7), an ultrasonic inspection

(refer to Appendix 04: Non Destructive Testing Procedure ) and an HFEC

inspection (Refer to NTM 51-10-20 Part 6).

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 546015-832-802 001

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 546015-832-003-001 - Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post Repair

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 31

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@A300-600

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) 51-10-20 Part 6

51-70-00 Part 7

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBBAA

Inspection Area: Post repair

Sheet 01

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

(a) Do a detailed inspection (Refer to NTM 51-70-00 Part 7), an ultrasonic inspection

(refer to Appendix 04: Non Destructive Testing Procedure ) and an HFEC

inspection (Refer to NTM 51-10-20 Part 6).

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 546015-832-802 001

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 32

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@A300-600

SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 546015-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

**CONF 002

(1) Subtask 546015-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 33

5

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@A300-600

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 34

5

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@A300-600

SERVICE BULLETIN

Task 546015-832-804-001 - Inspection Post Service Bulletin No. A300-54-6021

**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 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 24.00

ELAPSED TIME (HOURS) 6.00

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 35

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@A300-600

SERVICE BULLETIN

**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 546015-910-003-001 - 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

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.), 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 546015-839-004-001 - 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 546015-910-003-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 36

5

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026

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.), 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 546015-839-004-001 - 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 546015-941-004-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(e) Put the access platforms in position.

**CONF 002

(1) Subtask 546015-941-004-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(e) Put the access platforms in position.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 546015-832-002-001 - Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post SB No. A300-54-6021

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 38

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Manpower Resources

Manhours 18.00

Minimum number of person 4

Subtask elapsed time 4.50

Skills AIRFRAME

References

Non Destructive Test Manual (NTM) 51-70-00 Part 7

54-50-34 Part 6

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBCAA

Inspection Area: Post Service Bulletin

No. A300-54-6021

Sheet 01

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

(a) Do a detailed inspection (Refer to NTM 51-70-00 Part 7), an HFEC inspection

(Refer to NTM 54-50-34 Part 6) and an ultrasonic inspection (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 546015-832-804 001

Inspection Post Service Bulletin No. A300-54-6021 at the interval given in

PLANNING INFORMATION Paragraph E.(2).

2 If crack is found:

- Contact Airbus before next flight.

**CONF 002

(1) Subtask 546015-832-002-001 - Do a Detailed Inspection of the LH and RH Side

Panels on the Pylon 1 and 2 Post SB No. A300-54-6021

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 39

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Manpower Resources

Manhours 18.00

Minimum number of person 4

Subtask elapsed time 4.50

Skills AIRFRAME

References

Non Destructive Test Manual (NTM) 51-70-00 Part 7

54-50-34 Part 6

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FBCAA

Inspection Area: Post Service Bulletin

No. A300-54-6021

Sheet 01

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

(a) Do a detailed inspection (Refer to NTM 51-70-00 Part 7), an HFEC inspection

(Refer to NTM 54-50-34 Part 6) and an ultrasonic inspection (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 546015-832-804 001

Inspection Post Service Bulletin No. A300-54-6021 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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 40

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**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 546015-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

**CONF 002

(1) Subtask 546015-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 41

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This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 42

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Task 546015-833-802-001 - 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 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

**CONF 002

Zone

From 410 to 420

Access

Panel 413CL 413EL 414CR 414ER 423CL 423EL 424CR 424ER

Manpower

TOTAL MANHOURS 30.00

ELAPSED TIME (HOURS) 7.50

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 43

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**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 546015-910-004-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

References

Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001

Consumable Material List (CML)

(a) For the specification of the material numbers (Mat. No.), 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 546015-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 546015-910-004-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 44

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Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

References

Aircraft Maintenance Manual (AMM) 20-31-00, Page Block 001

Consumable Material List (CML)

(a) For the specification of the material numbers (Mat. No.), 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 546015-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 546015-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 45

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(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(e) Put the access platforms in position.

**CONF 002

(1) Subtask 546015-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00 Page Block 301).

(c) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(e) Put the access platforms in position.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 546015-833-020-001 - Repair the Side Panel of the Pylon

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 46

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Manpower Resources

Manhours 24.00

Minimum number of person 4

Subtask elapsed time 6.00

Skills AIRFRAME

Material necessary to do the job

Kit 546015A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

A5461255220000 1 Doubler

A5461255220100 1 Doubler

A5461255320000 8 Washer

A5461255420000 6 Washer

ASNA2314-4-13 6 Screw

ASNA2314-6-14 4 Screw

ASNA2314-6-16 8 Screw

NAS1153E3 4 Screw

NAS1154-13 2 Screw

NAS1726-4E 8 Nut

NAS1726-6E 8 Nut

NSA5414-36-20 16 Rivet

R5461012420200 2 Shim

References

Non Destructive Test Manual (NTM) 51-10-20 Part 6

Structural Repair Manual (SRM) 54-51-31

(a) Perform repair in accordance with SRM 54-51-31.

(b) Do a one time Eddy Current inspection of cut-out (Refer to NTM 51-10-20 Part 6)

to ensure that the crack is totally removed.

(c) Install :

1 Doubler A5461255220000

1 Doubler A5461255220100

2 Shim R5461012420200

with :

8 Washer A5461255320000

6 Washer A5461255420000

4 Screw ASNA2314-6-14

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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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 detailed inspection TASK 546015-832-802 001 Inspection Post Repair at the

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

**CONF 002

(1) Subtask 546015-833-020-001 - Repair the Side Panel of the Pylon

Work Zones and Access Panels

Zone Access/Work location

From 410 Access Panel 413EL, Panel 413CL, Panel 414ER, Panel

414CR

Work location Rib 8

To 420 Access Panel 423EL, Panel 423CL, Panel 424ER, Panel

424CR

Work location Rib 8

Manpower Resources

Manhours 24.00

Minimum number of person 4

Subtask elapsed time 6.00

Skills AIRFRAME

Material necessary to do the job

Kit 546015A01R02

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.: A300-54-6015

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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) 51-10-20 Part 6

Structural Repair Manual (SRM) 54-51-31

(a) Perform repair in accordance with SRM 54-51-31.

(b) Do a one time Eddy Current inspection of cut-out (Refer to NTM 51-10-20 Part 6)

to ensure that the crack is totally removed.

(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 detailed inspection TASK 546015-832-802 001 Inspection Post Repair at the

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 49

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**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 546015-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

**CONF 002

(1) Subtask 546015-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

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

equipment.

(b) Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR

(Refer to AMM 06-41-54 Page Block 001).

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 50

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(c) Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR

(Refer to AMM 06-41-54 Page Block 001).

(d) Remove the access platforms.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 51

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**CONF ALL

AREAS TO BE

INSPECTED

LENGTH

FWD B

RIB8

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

B

B

A

RIB8

NOTES:

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A

A

D_SB_546015_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Inspection Area: Pre repair and Pre Service Bulletin No. A300-54-6021

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 52

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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

CUT−OUT

A

A

DOUBLER

D_SB_546015_5_BBAA_01_00

Figure A-FBBAA - Sheet 01

Inspection Area: Post repair

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 53

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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

DOUBLER

D_SB_546015_5_BCAA_01_00

Figure A-FBCAA - Sheet 01

Inspection Area: Post Service Bulletin No. A300-54-6021

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 54

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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 546015−832−801−001

AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

APPLY THE

SERVICE BULLETIN

A300−54−6021

(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 546015−832−801−001

REFER TO TASK 546015−832−802−001

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 546015−832−804−001

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 546015−833−802−001

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 546015−832−804−001

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 546015−832−802−001

D_SB_546015_5_FAAA_01_03

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 55

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This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 56

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SERVICE BULLETIN

Appendix 01 - Inspection Report Pre repair and Pre Service Bulletin No. A300-54-6021

**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.: A300-54-6015

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

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SERVICE BULLETIN

Appendix 01 - Inspection Report Pre repair and Pre Service Bulletin No. A300-54-6021

**CONF ALL

AREAS TO BE

INSPECTED

LENGTH

FWD B

RIB8

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

B

B

A

RIB8

NOTES:

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A

A

D_SB_546015_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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Appendix 01 - Inspection Report Pre repair and Pre Service Bulletin No. A300-54-6021

**CONF ALL

NO

CRACK

RH SIDE

RH SIDE

DETAILED

INSPECTION

LH SIDE

LH SIDE

CRACK

LENGHT

LH

PYLON

RH

PYLON

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRCTURE − ENGINE PYLON

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 36 14

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−54−6015

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION

EDDY CURRENT

EDDY CURRENT

INSPECTION

SB A300−54−6021

APPLIED

REPAIR

APPLIED

D_SB_546015_5_RAAA_02_00

Figure A-FRAAA - Sheet 02

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

5

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@A300-600

SERVICE BULLETIN

Appendix 01 - Inspection Report Pre repair and Pre Service Bulletin No. A300-54-6021

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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@A300-600

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.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 02 - Inspection Report Post repair

**CONF ALL

INSPECTION EDDY

CURRENT

DETAILED

INSPECTION DOUBLER

20mm (0.787in.) FROM

DOUBLER EDGE

DETAILED INSPECTION AREA

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A

A

RIB8

B

A A

FWD

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

B

B

A

RIB8

NOTES:

ULTRASONIC

INSPECTION HOLE 2

ULTRASONIC

INSPECTION HOLE 1

CUT−OUT

A

A

DOUBLER

D_SB_546015_5_RBAA_01_00

Figure A-FRBAA - Sheet 01

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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SERVICE BULLETIN

Appendix 02 - Inspection Report Post repair

**CONF ALL

NO

CRACK

RH SIDE

RH SIDE

DETAILED

INSPECTION

LH SIDE

LH SIDE

CRACK

LENGHT

LH

PYLON

RH

PYLON

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRCTURE − ENGINE PYLON

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 36 14

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−54−6015

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION

EDDY CURRENT

EDDY CURRENT

INSPECTION

ULTRASONIC INSPECTION

ULTRASONIC

INSPECTION

CRACK FOUND

(GIVE HOLES No.)

D_SB_546015_5_RBAA_02_01

Figure A-FRBAA - Sheet 02

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

5

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SERVICE BULLETIN

Appendix 02 - Inspection Report Post repair

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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SERVICE BULLETIN

Appendix 03 - Inspection Report Post Service Bulletin No. A300-54-6021

**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.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 03 - Inspection Report Post Service Bulletin No. A300-54-6021

**CONF ALL

INSPECTION EDDY

CURRENT

DETAILED

INSPECTION DOUBLER

20mm (0.787in.) FROM

DOUBLER EDGE

DETAILED INSPECTION AREA

RIGHT PYLON SHOWN

LEFT PYLON SYMMETRICAL

PW PYLON SHOWN

IDENTICAL FOR GE PYLON INSPECTION

A

A

RIB8

B

A A

FWD

PW PYLON SHOWN

INSPECTION IDENTICAL FOR GE PYLON

B

B

A

RIB8

NOTES:

ULTRASONIC

INSPECTION HOLE 2

ULTRASONIC

INSPECTION HOLE 1

A

A

DOUBLER

D_SB_546015_5_RCAA_01_00

Figure A-FRCAA - Sheet 01

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 03 - Inspection Report Post Service Bulletin No. A300-54-6021

**CONF ALL

NO

CRACK

RH SIDE

RH SIDE

DETAILED

INSPECTION

LH SIDE

LH SIDE

CRACK

LENGHT

LH

PYLON

RH

PYLON

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRCTURE − ENGINE PYLON

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 36 14

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−54−6015

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD : DETAILED INSPECTION

EDDY CURRENT

EDDY CURRENT

INSPECTION

ULTRASONIC INSPECTION

AFTER EMBODIMENT OF THE SERVICE BULLETIN No. A300−54−6021

ULTRASONIC

INSPECTION

CRACK FOUND

(GIVE HOLE No.)

D_SB_546015_5_RCAA_02_00

Figure A-FRCAA - Sheet 02

Inspection Report

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

5

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

Appendix 03 - Inspection Report Post Service Bulletin No. A300-54-6021

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

This document contains the Non-Destructive inspection procedure related to the "Pylon - Lateral panel

at RIB 8 area after doubler installation"

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_01_01

Figure A-FAAAA - Sheet 01

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_02_01

Figure A-FAAAA - Sheet 02

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_03_01

Figure A-FAAAA - Sheet 03

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_04_01

Figure A-FAAAA - Sheet 04

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 5

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_05_01

Figure A-FAAAA - Sheet 05

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 6

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_06_01

Figure A-FAAAA - Sheet 06

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 7

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_07_01

Figure A-FAAAA - Sheet 07

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 8

5

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@A300-600

SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_08_01

Figure A-FAAAA - Sheet 08

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 9

5

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@A300-600

SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_09_01

Figure A-FAAAA - Sheet 09

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 10

5

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@A300-600

SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_10_01

Figure A-FAAAA - Sheet 10

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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SERVICE BULLETIN

Appendix 04: Non Destructive Testing Procedure

**CONF ALL

D_SB_546015_5_AAAA_11_00

Figure A-FAAAA - Sheet 11

Ultrasonic Inspection Procedure of lateral panel at Rib 8 after doubler installation.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 12

5

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@A300-600

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.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 05: Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−6015

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

10.00

2.50

STEPS

3.00 0.75

0

DO A DETAILED INSPECTION OF THE LH/RH

4.00 1.00

CLOSE−UP 3.00 0.75

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)

123

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 A300−54−6021

D_SB_546015_5_ABAA_01_00

Figure A-FABAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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SERVICE BULLETIN

Appendix 05: Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−6015

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

24.00

6.00

STEPS

3.00 0.75

0

DO A DETAILED INSPECTION OF THE LH/RH

18.00 4.50

CLOSE−UP 3.00 0.75

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)

246

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

135

D_SB_546015_5_ACAA_01_00

Figure A-FACAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 3

5

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@A300-600

SERVICE BULLETIN

Appendix 05: Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−6015

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

24.00

6.00

STEPS

3.00 0.75

DO A DETAILED INSPECTION OF THE LH/RH

18.00 4.50

CLOSE−UP 3.00 0.75

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

PER

4

4

4

:

:

SB ELAPSED TIME

(HOURS)

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

SIDE PANELS ON THE PYLONS 1 AND 2

POST SB No. A300−54−6021

02 4 6 135

D_SB_546015_5_ADAA_01_00

Figure A-FADAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

5

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@A300-600

SERVICE BULLETIN

Appendix 05: Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−54−6015

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

30.00

7.50

STEPS

3.00 0.75

0

24.00 6.00

CLOSE−UP 3.00 0.75

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

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

REPAIR THE SIDE PANEL OF THE PYLON

1357 8

D_SB_546015_5_AEAA_01_00

Figure A-FAEAA - Sheet 01

Elapsed Time Assumption

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 Page: 5

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SERVICE BULLETIN

REPORTING SHEET

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

8.

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

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

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

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

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

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

Or : Intermediate revision YES/NO

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

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

the next feasible revision, this will result in

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

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

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

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

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

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

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

REVISION No.: 03 - Apr 11/13 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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015

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

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