# @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



# MANDATORYMANDATORYMANDATORY ATA SYSTEM: 54 

### TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. MODIFICATION No.: None This page transmits Revision No.03 of Service Bulletin No.A300-54-6015 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASONRevision No. 03 issued to update the threshold and intervals as per analysis improvement and inservice crack findings consistency. CHANGES SUMMARY MODIFICATIONS Minor editorial or document structure change N REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Minor editorial or document structure change N GENERAL EVALUATION Minor editorial or document structure change N MATERIAL PRICE INFORMATION Minor editorial or document structure change N Minor editorial or document structure change N 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

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

# @A300-600 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 5

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

# @A300-600 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 5

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

# @A300-600 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 5

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

# @A300-600 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 5

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

# @A300-600 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 5

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

# @A300-600 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORYMANDATORYMANDATORY ATA SYSTEM: 54 

### TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES On aircraft fitted with GE pylon, cracks have been reported on pylon side panels (upper section) at 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 5

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

# @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 5

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

# @A300-600 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 5

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

# @A300-600 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 5

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

# @A300-600 SERVICE BULLETIN SUMMARY

**CONF ALL

AREAS TO BE INSPECTED

RIB8 

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

### B **B**



## A RIB8

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

### A **A**

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 5

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

# @A300-600 SERVICE BULLETIN SUMMARY

**CONF ALL

DETAILED INSPECTION AREA RIB8 

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

### B **B**



## A RIB8

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

### A **A**

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 5

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

# @A300-600 SERVICE BULLETIN SUMMARY

**CONF ALL

DETAILED INSPECTION AREA RIB8 

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

### B **B**



## A RIB8

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

### A **A**

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 5

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

# @A300-600 SERVICE BULLETIN SUMMARY

This Page Intentionally Left Blank

DATE: Aug 11/93 SERVICE BULLETIN No.: A300-54-6015 REVISION No.: 03 - Apr 11/13 Page: 8 5

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

# @A300-600 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY ATA SYSTEM: 54 

### TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8. MODIFICATION No.: None This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE: This Service Bulletin is only applicable to aircraft listed above on which Mod. 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 5

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

# @A300-600 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 5

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

# @A300-600 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 5

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

# @A300-600 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 Compliance Time Condition Action 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

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

# @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 Compliance Time Condition Action 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 Before 1000FC None None Crack found <20 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 Compliance Time Condition Action 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

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

# @A300-600 SERVICE BULLETIN Table 2: Detailed Inspection of the LH/RH Side Panels on the Pylons 1 and 2 Post-repair Compliance Time Condition Action Threshold 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 Compliance Time Condition Action 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

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

# @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 Compliance Time Condition Action 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 Compliance Time Condition Action 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

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

# @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 Compliance Time Condition Action 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 Before 1000FC None None Crack found <20 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 Compliance Time Condition Action 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

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

# @A300-600 SERVICE BULLETIN Table 2: Detailed Inspection of the LH/RH Side Panels on the Pylons 1 and 2 Post-repair Compliance Time Condition Action Threshold (FC or FH whichever occurs first) Grace period Repetitive Interval (FC or FH whichever occurs first) 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 Compliance Time Condition Action 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

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

# @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 Compliance Time Condition Action 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

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

# @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

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

# @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 5

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

# @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 5

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

# @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 5

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

# @A300-600 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 546015-832-801-001 - Inspection Pre Repairand 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

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @A300-600 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 5

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

# @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 5

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

# @A300-600 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 5

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

# @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 5

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

# @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: 26 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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

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

# @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 5

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

# @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 5

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

# @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

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

# @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

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

# @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 5

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

# @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

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

# @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 REVISION No.: 03 - Apr 11/13 Page: 37 5

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

# @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 546015-941-004-001 - 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 5

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

# @A300-600 SERVICE BULLETIN 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 5

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

# @A300-600 SERVICE BULLETIN 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 5

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

# @A300-600 SERVICE BULLETIN
**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 5

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

# @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: 42 5

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

# @A300-600 SERVICE BULLETIN 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 5

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

# @A300-600 SERVICE BULLETIN
**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 5

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

# @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) 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 5

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

# @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 546015-941-002-001 - 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 5

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

# @A300-600 SERVICE BULLETIN 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 REVISION No.: 03 - Apr 11/13 Page: 47 5

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

# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Apr 11/13 Page: 48 5

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

# @A300-600 SERVICE BULLETIN

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 5

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

# @A300-600 SERVICE BULLETIN
**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 5

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

# @A300-600 SERVICE BULLETIN (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 5

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

# @A300-600 SERVICE BULLETIN

**CONF ALL

AREAS TO BE INSPECTED LENGTH



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

### B **B**



## A RIB8

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

### A **A**

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 5

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

# @A300-600 SERVICE BULLETIN

**CONF ALL

INSPECTION EDDY CURRENT DETAILED INSPECTION DOUBLER

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

### A **A**

RIB8 

## B **A A** 

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

### B **B**



## A RIB8

**NOTES:** ULTRASONIC INSPECTION HOLE
ULTRASONIC INSPECTION HOLE 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 5

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

# @A300-600 SERVICE BULLETIN

**CONF ALL

INSPECTION EDDY CURRENT DETAILED INSPECTION DOUBLER

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

### A **A**

RIB8 

## B **A A** 

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

### B **B**



## A RIB8

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

### A **A**

DOUBLER

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 5

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

# @A300-600 SERVICE BULLETIN

**CONF ALL

QUESTION FINDING
ACTION NO CRACK FINDING

OR

CONTACT AIRBUS BEFORE NEXT FLIGHT YES DO A DETAILED INSPECTION OF THE SIDE PANELS ON THE PYLONS 1 AND 2 REFER TO TASK 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 5

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

# @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: 56 5

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

# @A300-600 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 5

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

# @A300-600 SERVICE BULLETIN Appendix 01 - Inspection Report Pre repair and Pre Service Bulletin No. A300-54-6021

**CONF ALL

AREAS TO BE INSPECTED LENGTH



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

### B **B**



## A RIB8

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

### A **A**

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 5

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

# @A300-600 SERVICE BULLETIN 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

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

# @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

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

# @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

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

# @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 5

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

# @A300-600 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

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

# @A300-600 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 5

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

# @A300-600 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

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

# @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

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

# @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.

# @A300-600 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

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

# @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

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

# @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

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

# @A300-600 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

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

# @A300-600 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

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

# @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

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

# @A300-600 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

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

# @A300-600 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

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

# @A300-600 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

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

# @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

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

# @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

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

# @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

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

# @A300-600 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

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

# @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

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

# @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

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

# @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

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

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

# @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

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

# @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 5

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

# @A300-600 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 5

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

# @A300-600 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 5

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