# Airbus Service Bulletin A300-54-6015

Copy: Revision 02 ("A300-54-6015 R2_"), 23 pages: PDF https://openairdocs.org/files/sha256/f3/94/f394def056a3f14f504fd397f6c90f86cfdae8b59d9bd64721b27fc9349ad675; text https://openairdocs.org/service-documents/airbus/a300-54-6015/file/f394def056a3.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2009-0789, the docket of AD 2010-06-04. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A300-54-6015
- Latest revision known: A300-54-6015, Revision R03, dated April 11, 2013 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/airbus/a300-54-6015

## ADs that cite it (2) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2015-25-06](https://openairdocs.org/ad/2015-25-06.md), effective Feb 2, 2016: Revisions 01, 02 and 03
- [AD 2010-06-04](https://openairdocs.org/ad/2010-06-04.md), effective Apr 15, 2010: Revisions 01 and 02

Also cited in [2 proposed ADs](https://openairdocs.org/service-documents/airbus/a300-54-6015/proposed.md), [3 difficulty reports](https://openairdocs.org/service-documents/airbus/a300-54-6015/reports.md).

## Text (23 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2009-0789, the docket of AD 2010-06-04. Not covered by OpenAirDocs’ CC0 dedication. This text is OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1 (OCR)

• A300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
REVISION TRANSMITTAL SHEET  REVISION TRANSMITTAL SHEET
AIRBUS  - COMPLIANCE
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte  Para. 1.E. Accomplishment timescale updated.
31707 BLAGNAC CEDEX FRANCE
Tel : (33) 5 61 93 33 33  - WEIGHT AND BALANCE
Telex: AIRBU 530526F
Fax : (33) 5 61 93 42 51  Para. 1.H. Config. 02 and 03 added.
MANDATORY  MANDATORY  MANDATORY  MANDATORY  - REFERENCES
ATA SYSTEM: 54  Para. 1.J. R54610124 replaced by SRM 54-51-31. Reference to AMM 06-41-54 added.
TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.  MATERIAL INFORMATION:
MODIFICATION No. : None  - MATERIAL - PRICE AND AVAILABILITY
This page transmits Revision No. 02 of Service Bulletin No. A300-54-6015.  Para. 2.A. Kit price updated.
ADDITIONAL WORK  - LIST OF COMPONENTS
No additional work is required by this revision for aircraft modified by any previous issue.
REASON
Revision No. 02 is issued to replace the PN ASNA2001 by ASNA2314 and replace R54610124 by
SRM 54-51-31.
Para. 2.C. ASNA2001V4-13X becomes ASNA2314-4-13. ASNA2001V6-14X becomes
ASNA2314-6-14. ASNA2001V6-16X becomes ASNA2314-6-16.
LIST OF MATERIALS - OPERATOR SUPPLIED
Para. 2.D. Mat. No. 11-003 becomes 11-026.
CHANGES  ACCOMPLISHMENT INSTRUCTIONS:
SUMMARY :  - GENERAL
• REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES  Para. 3.A. Mat. No. 11-003 becomes 11-026. Removal of the pylon access panels added.
Kit price updated.  • INSPECTION
EFFECTIVITY  Para. 3.B. Text updated.
Operators updated. NOTE added.  • REPAIR
MATERIAL INFORMATION  Para. 3.C. ASNA2001 becomes ASNA2314. R54610124 replaced by SRM 54-51-31. Text
updated.
R54610124 replaced by SRM 54-51-31.
- CLOSE-UP
PLANNING INFORMATION •
Para. 3.E. Installation of the pylon access panels added.
EFFECTIVITY
- ILLUSTRATIONS
Para. 1.A. Operator 98W, aircraft MSN 0377 deleted. Effectivity updated. NOTE modified.
NOTE added.  Figure 4, Sheet 2: Modified.
DESCRIPTION  APPENDIY 1
Para. 1.D. Description modified.  - Para. 1. AIRBUS DEPT. updated.
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 1 of 3  REVISION No. : 02 - Jun 26/08  Page : 2
Printed in France @AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 2 (OCR)

© A300-600  GA300-600
SERVICE BULLETIN  SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
APPENDIX 2 :
- Para. 1. AIRBUS DEPT. updated.
- Figure 1, Sheets 1 and 2: R54610124 replaced by SRM 54-51-31.
APPENDIX 3 :
- Para. 1. AIRBUS DEPT. updated.
NOTE:  Lay-out changes due to computerization of this revision are not identified.
FILING INSTRUCTIONS
This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS
Revision No. 01 issued to inform the operators that this Service Bulletin is rendered mandatory. The  This Page Intentionally Left Blank
thresholds and intervals have also been reviewed.
REVISION SEQUENCE
ORIGINAL : Jul 13/07
REVISION No. : 01 - Nov 09/07
REVISION No. : 02 - Jun 26/08
DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 3  REVISION No. : 02 - Jun 26/08  Page : 4
Printed in France © AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 3 (OCR)

9A300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
SUMMARY  SUMMARY
AIRBUS  EFFECTIVITY
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte  This Service Bulletin is applicable to these operators:
31707 BLAGNAC CEDEX FRANCE
Tel : (33) 5 61 93 33 33  AAL AAW ABD CES DLH EGN F2I FDX GXY IRA JAL KAC KAL LAA MON MSR OAL OHY QTR SUD
Telex: AIRBU 530526F  TAR THA
Fax : (33) 5 61 93 42 51
NOTE:  This Service Bulletin is only applicable to aircraft listed above on which Mod. No. 02434S3600
This summary is for information only and is  (NEW ENGINE PYLON - COMMON PARTS) is embodied or Mod No. 03599D9179
not approved for modification of the aircraft  (REFERENCE MODIFICATION FOR ST2 (SN207)) is embodied on one or both pylons.
MANDATORY  MANDATORY  MANDATORY  MANDATORY  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
ATA SYSTEM : 54  aircraft MSN 0723, 0725-0728, 0731, 0733 and subsequent.
TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.  NOTE:  This modification is partially embodied on aircraft MSN 0732 (only on the right pylon).
MODIFICATION No. : None  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
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES  by this inspection.
On aircraft fitted with GE pylon, cracks have been reported on pylon side panels (upper section) at rib8.  CONCURRENT REQUIREMENTS
The crack is starting from the hole at the top edge of the panel and running up and downwards from this
fastener hole.  None
This Service Bulletin requires a detailed visual and Eddy Current inspection of pylon side panels (upper  REFERENCES/REPERCUSSIONS
section) at rib8, in order to detect any crack.
TEU  : 54.51.31.001
This inspection will make it possible to detect crack propagation at an early stage, thus avoiding an extensive
repair.  OEB  : None
EVALUATION TABLE  AOT  : None
SILI  : None
COMPLIANCE  Mandatory  CANCELS INSPECTION SB  No
LIFE LIMIT  : None
AD  Yes  A/C OPERATION AFFECTED  No
LINE MAINTENANCE AFFECTED: No
RELIABILITY AFFECTED  No  PAX COMFORT AFFECTED  No  OTHERS  : None
NATURE OF THE WORK
COST SAVING  No  ETOPS AFFECTED  No
AIRCRAFT : YES
STRUCTURAL LIFE EXTN  No  VENDOR SB INVOLVED  No
EQUIPMENT: NO
KIT PRICE (USD) A01R00  2,975  HARD : NO
SOFT: NO
OBRM : NO
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 1 of 5  REVISION No. : 02 - Jun 26/08  Page : 2
RBUS 2008 All rights reserved

### Page 4 (OCR)

SA300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
SUMMARY  SUMMARY
MANPOWER
Config, 01
TOTAL MANHOURS  31.0
ELAPSED TIME (HOURS)  15.5
Config. 02
TOTAL MANHOURS  8.0
ELAPSED TIME (HOURS)  4.0
PECTION IDENTICAL FOR GE PYL
Config. 03
TOTAL MANHOURS  14.0
ELAPSED TIME (HOURS)  7.0
MATERIAL INFORMATION
AIRCRAFT DATA
Config. 01
Kit 546015A01R02
If repair: Refer to SRM 54-51-31.
APPENDICES
Appendix 1: Inspection report
Appendix 2: Inspection report
Appendix 3: Inspection report
CONFIG. 01
D_SB_546015_5_SUXX 01_00
DATE : Ju! 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 3  REVISION No. : 02 - Jun 26/08  Page : 4
Printed in France © AIRBUS 2008 All rights reserved

### Page 5 (OCR)

• A300-600  GA300-600
SERVICE BULLETIN  SERVICE BULLETIN
SUMMARY
INSPECTION
This Page Intentionally Left Blank
DETAILED VISUAL INSPECTION AREA
CONFIG, 02 OR CONFIG. 03
D_SB_546015_5_SVXX_01_00
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 5  REVISION No. : 02 - Jun 26/08  Page: 6
Printed in France @AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights raserved

### Page 6 (OCR)

• A300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
AIRBUS  NOTE:  The modification No. 10432S20461 (NACELLES/PYLONS - PANELS IN
CUSTOMER SERVICES DIRECTORATE  THE UPPER CORNER AT RIB 8 - ADD A DOUBLER (PRODUCTION
1 Rond Point Maurice Bellonte  SOLUTION)) is embodied prior to delivery on aircraft MSN 0723,
31707 BLAGNAC CEDEX FRANCE  0725-0728, 0731, 0733 and subsequent.
Tel : (33) 5 61 93 33 33
Telex : AIRBU 530526F  NOTE:  This modification is partially embodied on aircraft MSN 0732 (only on
Fax : (33) 5 61 93 42 51  the right pylon).
MANDATORY  MANDATORY  MANDATORY  MANDATORY
ATA SYSTEM: 54
TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.
MODIFICATION No. : None
This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property
of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information
contained in it. It is delivered on the express condition that said document and the information contained in
it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby
delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any
manner (except for the purposes of performing the tasks described hereunder and provided that any recipient
of such document shall comply with the conditions herein), without AIRBUS' prior written consent.
PLANNING INFORMATION
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.
(b)  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
AAL  0423 0459 0460 0461 0462 0463 0465 0466 0469 0470 0471 0474
0506 0507 0508 0509 0510 0511 0512 0513 0514 0515 0516 0517
0606 0610 0612 0615 0619 0626 0639 0643 0645 0675
EFFECTIVITY  AAW  0354
(1) Models  ABD  0529 0557
B4-601 B4-603 B4-605R B4-620 B4-622 B4-622R C4-620  CES  0521 0525 0532 0707 0732
(2)  Aircraft  DLH  0380 0391 0401 0405 0408 0411 0414 0546 0553 0608 0618
0623 0701
(a)  Effectivity by MSN
EGN  0555 0625
' This Service Bulletin is applicable to aircraft MSN:
F2I  0284 0294 0301 0307 0312 0317 0321 0336 0341 0348 0351
0252 0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348 0351 0354 0358
0361 0365 0368 0380 0384 0388 0391 0395 0398 0401 0405 0408 0411 0414 0417  FDX
0423 0459-0466 0469-0471 0474 0477 0479 0505-0518 0521 0525 0529 0530 0532
0533 0536 0540 0543 0546 0553-0561 0563 0566 0569 0572 0575 0577 0579 0581
0582 0584 0601-0619 0621 0623 0625-0633 0635 0637 0639 0641 0643 0645 0657  GXY
0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685 0688 0692
0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721  IRA
0722 0724 0729 0730 0732
0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0559 0572
0575 0579 0581 0611 0613 0633 0657 0659 0668 0709 0713 0715
0533
0632 0696
JAL  0602 0617 0621 0637 0641 0670 0679 0683 0703 0711 0724
NOTE:  This Service Bulletin is only applicable to aircraft listed above on which  0729 0730
Mod. No. 02434S3600 (NEW ENGINE PYLON - COMMON PARTS) is
embodied or Mod No. 03599D9179 (REFERENCE MODIFICATION  KAC  0344 0673 0694 0699 0719 0721
FOR ST2 (SN207)) is embodied on one or both pylons.
KAL  0582 0609 0627 0631 0662 0685 0692 0717 0722
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 1 of 22  REVISION No. : 02 - Jun 26/08  Page : 2
IRBUS 2008 All rights reserved  Printed in France © AIRBUS 2009 All richis reserved

### Page 7 (OCR)

• A300-600  •A300-600
SERVICE BULLETIN  SERVICE BULLETIN
OPERATOR  MSN  None
LAA  0601 0616  B. CONCURRENT REQUIREMENTS
MON  0540 0556 0604 0605  None
MSR  0561 0607  c.  REASON
OAL  0603  (1)  History
OHY  0584 0677  On aircraft fitted with GE pylon, cracks have been reported on pylon side panels (upper
section) at rib8. The crack is starting from the hole at the top edge of the panel and running
QTR  0554 0560 0614 0630 0664 0688  up and downwards from this fastener hole.
SUD  0252 0666  (2)  Objective/Action
TAR  0505 0558 0563  This Service Bulletin requires a detailed visual and Eddy Current inspection of pylon side
panels (upper section) at rib&, in order to detect any crack.
THA  0368 0384 0395 0398 0464 0518 0566 0569 0577 0628 0629
0635 0681 0705  (3)  Advantages
(c)  Effectivity by MSN and Kit/Configuration  This inspection will make it possible to detect crack propagation at an early stage, thus
avoiding an extensive repair.
The Kits and configurations applicable to these MSNs are given at the end of this list
(4) Operational/Maintenance Consequences
0252 0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348 0351 0354 0358  0361 0365 0368 0380 0384 0388 0391 0395 0398 0401 0405 0408 0411 0414 0417  None
0423 0459-0466 0469-0471 0474 0477 0479 0505-0518 0521 0525 0529-0530  0532-0533 0536 0540 0543 0546 0553-0561 0563 0566 0569 0572 0575 0577 0579  D.  DESCRIPTION
0581-0582 0584 0601-0619 0621 0623 0625-0633 0635 0637 0639 0641 0643 0645  0657 0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685  To accomplish this Service Bulletin it is necessary to :
0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717  0719 0721-0722 0724 0729-0730 0732  (1)  Config. 01
KIT No.  QTY PER A/C CONFIGURATION  (a) Inspection
None  02  1 On pylons 1 and 2, do a detailed visual inspection on pylon side panel (upper  section) at rib 8.
None  03  (b) Repair
546015A01R02  01  1 Repair if necessary installing a doubler.
NOTE :  Config. 01 concerns aircraft without repair and without embodiment ol  SB A300-54-6021 (Mod. No. 10431S20462)  (2)  Config. 02
NOTE :  Config. 02 concerns aircraft with repair and without embodiment of SB  (a)  Inspection
A300-54-6021 (Mod. No. 10431S20462).
1 On pylons 1 and 2, do a repetitive detailed visual inspection on pylon side
NOTE:  Config. 03 concerns aircraft without repair and with embodiment of SB  panel (upper section) at rib 8.
A300-54-6021 (Mod. No. 10431S20462)  (b) Repair
(3) Spares  1 If crack detected, contact AIRBUS.
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 3  REVISION No. : 02 - Jun 26/08  Page : 4
Printed in France © AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 8 (OCR)

© A300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
(3)  Config. 03  New inspection program after repair (SRM 54-51-31) :
(a)  Inspection  Threshold  Interval
1 On pylons 1 and 2, do a repetitive Eddy Current inspection and a detailed visual  Engine type  FC  FC
inspection on pylon side panel (upper section) at rib 8.  GENERAL
ELECTRIC
(b)  Repair  CF6-80
1 If crack detected, contact AIRBUS.  PRATT &  Post repair  9,300  5,300
WHITNEY 4000
COMPLIANCE
PRATT &
(1)  Classification  WHITNEY JT9D
Mandatory  NOTE:  Thresholds counted from accomplishment of the repair.
(2)  Accomplishment Timescale  NOTE:  The following grace periods apply:
Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue  - The inspection is to be done within 250 FC following receipt of this Service Bulletin.
(EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals and/or  of an Airworthiness Directive (AD) published by the European Aviation Safety Agency  NOTE: The Inspection Service Bulletin is required at the given threshold/interval in  Flight Cycle/Flight Hour whichever occurs first.
date) given above but reference should be made to the AD for confirmation of the mandated
accomplishment timescale.  Config. 03
- Config. 01  Inspection program after accomplishment of SB A300-54-6021 (Mod. No. 10431S20462)
Threshold  Interval
Engine type
FC  FC  Threshold  Interval
Engine type
GENERAL  FC  FC
ELECTRIC  CF6-80  Service Bulletin No. A300-54-6021  GENERAL
ELECTRIC
not accomplished :  CF6-80  Service Bulletin No. A300-54-6021
PRATT &  4,200  3,600
WHITNEY 4000  Pre Mod No. 10431S20462  PRATT &  accomplished:  10,100  18,300
WHITNEY 4000
WHITNEY JT9D  PRATT &  Pre repair  PRATT &  Post Mod No. 10431S20462
WHITNEY JT9D
NOTE :  The following grace periods apply:
- The inspection is to be done within 2,000 FC without exceeding  20.000FC/40,000FH from first flight. If the threshold of 20,000FC/40.000FH  from first flight or scheduled interval (see Tables) havé been exceeded, the first  NOTE: Thresholds counted from accomplishment of Service Bulletin No.  A300-54-6021 (Mod. No. 10431S20462).
inspection is to be performed within 250 FC after réceipt of this Inspection Service  Bulletin (ISB).  NOT The inspectioving be done with 250 following receipt of this Service Bulletin.
NOTE:  The Inspection Service Bulletin is required at the given threshold/interval in  Flight Cycle/Flight Hour whichever occurs first.  NOTE: Accomplishment of Service Bulletin No. A300-54-6021 (Mod. No.  10431S20462) increases the inspection thresholds and intervals.
• Config. 02  NOTE: The Inspection Service Bulletin is required at the given threshold/interval in
Flight Cycle/Flight Hour whichever occurs first.
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 5  REVISION No. : 02 - Jun 26/08  Page : 6
Printed in France © AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 9 (OCR)

9A300-600  9A300-600
SERVICE BULLETIN  SERVICE BULLETIN
F. APPROVAL  Close-up  1.0
Approved under EASA Design Organisation Approval No. EASA.21J.031.  TOTAL MANHOURS  4.0
If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS  ELAPSED TIME (HOURS)  2.0
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  Config. 03
of the Service Bulletin.
Inspection for one pylon
G.  MANPOWER
Get access  3.0
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  Visual inspection  2.0
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  Eddy current inspection  6.0
times for paints, sealants, etc, and general administration work are also not included.
Close-up  3.0
Config. 01
TOTAL MANHOURS  14.0
Inspection per aircraft
ELAPSED TIME (HOURS)  7.0
Get access  1.0
H. WEIGHT AND BALANCE
Visual inspection  2.0
Config. 01 if repaired
Close-up  1.0
Manufacturers Empty Weight: +0.85 kg (+1.8739 Ib)
TOTAL MANHOURS  4.0
Effect on Balance  : +23.15 kgm (+167.44 lb.ft)
ELAPSED TIME (HOURS)  2.0
Config. 02 and Config. 03
Confia. 01
Not changed
Repair for one pylon
ELECTRICAL LOAD DATA
Eddy Current inspection of the cut-out  2.0
Not changed
Installation of the doubler  22.0
J. REFERENCES
Close-up  2.0
Aircraft Maintenance Manual (AMM)  : 06-41-54 20-31-00 24-00-00 24-41-00
TOTAL MANHOURS  26.0
Consumable Material List (CML)
ELAPSED TIME (HOURS)  15.0
Elec. Std. Practices Manual (ESPM)  : 20-55-00
Confia. 02
Non destructive Testing Manual (NTM)  : 51-10-20 51-70-00 54-50-34
Inspection for one pylon
Structural Repair Manual (SRM)  • 54-51-31
Get access  1.0
Appendix 1
Visual inspection  2.0
Appendix 2
DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. • A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 7  REVISION No. : 02 - Jun 26/08  Page : 8
Printed in France © AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 10 (OCR)

DA300-600  9A300-600
SERVICE BULLETIN  SERVICE BULLETIN
Appendix 3
Service Bulletin No. A300-54-6021
PUBLICATIONS AFFECTED
Impact on Scheduled Maintenance: refer to
Maintenance Planning Document (MPD)
INTERCHANGEABILITY/MIXABILITY
Not applicable
This Page Intentionally Left Blank
DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 9  REVISION No. : 02 - Jun 26/08  Page : 10
Printed in France ® AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 11 (OCR)

© A300-600  © A300-600
SERVICE BULLETIN  SERVICE BULLETIN
2. MATERIAL INFORMATION  ITEM NEW PART No.  QTY UM KEYWORD ITEM OLD PART No.  INT INST DISP
A.  MATERIAL - PRICE AND AVAILABILITY  NAS1726-6E  Nut
Material  NSA5414-36-20  R5461012420200  16  Rivet  Shim
purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is :  Customers with aircraft shown in the effectivity of this Service Bulletin should send a  NOTE: Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware  components in the related kit(s) which you cannot identify in the LIST OF
Weg beim Jaeger 150  AIRBUS Spares Support and Services  COMPONENTS of this Service Bulletin. The SM will give you the correct part number  to part number relationship.
D-22335 HAMBURG
GERMANY  D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
For ordering by internet: http://spares.airbus.com
DESCRIPTION  REFERENCE TO CML  QTY PER A/C INST/DISP
For ordering by fax: +49 40 50 76 25 90  MAT No.
(2)  Price and Availability  Solvent General Purpose  Mat. No. 11-026  As required
Kit 546015A01R02  (2)  Components
Cost  : 2,975.00 US dollars  None
Availability: 90 calendar days from receipt of order  E. PARTS TO BE RE-IDENTIFIED BY THE OPERATOR
The Kit availability given above is the standard lead time from the date of your purchase  None
order. If you require the Kit(s) before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.  F.  TOOLING - PRICE AND AVAILABILITY
The sales terms (costs and availability) are estimated in relation to economic conditions  at the issue date of the Service Bulletin.  (1) To accomplish this Service Bulletin it is necessary to use the following tools and equipment:
B. INDUSTRY SUPPORT INFORMATION  (a)  For inspection program after accomplishment of Service Bulletin No. A300-54-6021,  equipment and material for control by eddy current as per NTM 54-50-34 Part 6.
AIRBUS will not provide industry support for accomplishment of this Service Bulletin.  (b)  For inspection program during accomplishment of repair, equipment and material for
c.  LIST OF COMPONENTS  control by eddy current as per NTM 51-10-20 Part 6.
Kit 546015A01R02  G.  SPECIAL TOOLS
ITEM NEW PART No.  QTY UM KEYWORD ITEM OLD PART No.  INT INST DISP  None
A5461255220000  1  Doubler
A5461255220100  Doubler
A5461255320000  Washer
A5461255420000  Washer
ASNA2314-4-13  Screw
ASNA 2314-6-14  Screw
ASNA2314-6-16  Screw
NAS1153E3  Screw
NAS1154-13  Screw
NAS1726-4E  Nut
DATE • Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 11  REVISION No. : 02 - Jun 26/08  Page : 12
Printed in France @AIRBUS 2008 All rights reserved

### Page 12 (OCR)

DA300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
3.  ACCOMPLISHMENT INSTRUCTIONS  B.  INSPECTION
GENERAL
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:
NOTE :  Inspection results must be reported to AIRBUS after completion, on the recording
forms attached in Appendix.
- In case of findings, this reporting has to be made in accordance with Service Bulletin
instructions, that is to say:
Immediately (maximum within 48 hours) in case of damage which exceeds allowable or
rework limits for further action(s) before next flight.
After completion of the corrective action when damage is either within allowable or rework
limits or repaired in accordance with Service bulletin instructions.
PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS
NECESSARY ON WIRING AND COMPONENTS.
REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER
CONTAMINATION.
- In case of no findings, inspection record has to be sent as soon as maintenance check or
visit report which involves subject Service Bulletin has been established.
(1)  Config. 01
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND  (a)  For the inspection area, refer to Figure 1, Sheet 1.
DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
(b) Do a detailed visual inspection, refer to Figure 4, Sheets 1 and 2.
IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.
1 On pylons 1 and 2, do a detailed visual inspection (Refer to NTM 51-70-00, Page
(1)  Preparation  block 7) on pylon side panel (upper section) at rib 8.
(a)  Config. 01 thru Config. 03  (c)  For the inspection report, refer to Appendix 1.
1 Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00,  (2)  Config. 02
Page block 301).
(a)  For the inspection area, refer to Figure 2, Sheet 1.
2 De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page block
301).  (b)  Do a detailed visual inspection, refer to Figure 4, Sheet 2.
3 Remove the access panels of the pylon 1, 413EL, 413CL, 414ER and 414CR  1 On pylons 1 and 2, do a repetitive detailed visual inspection (Refer to NTM
(Refer to AMM 06-41-54, Page block 001).  51-70-00, Page block 7) on pylon side panel (upper section) at rib 8.
4 Remove the access panels of the pylon 2, 423EL, 423CL, 424ER and 424CR  (c) For the inspection report, refer to Appendix 2.
(Refer to AMM 06-41-54, Page block 001)
(3)  Config. 03
5 Put the access platforms in position.
(a) For the inspection area, refer to Figure 3, Sheet 1.
(2)  Standard Practices
(b) Do a detailed visual and an Eddy Current inspection, refer to Figure 4, Sheets 1.
(a)  Config. 01 thru Config. 03
1 On pylons 1 and 2, do a repetitive detailed visual inspection (Refer to NTM
1 For the specification of the material numbers (Mat. No.), refer to the CML.  51-70-00, Page block 7) and an Eddy Current inspection (Refer to NTM 54-50-34
Part 6) on pylon side panel (upper section) at rib 8.
Clean the surfaces to seal with Solvent General Purpose (Mat. No. 11-026) and
refer to AMM 20-31-00, Page block 001.  (c)  For the inspection report, refer to Appendix 3.
c.  REPAIR
(1) Config. 01
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 13  REVISION No. : 02 - Jun 26/08  Page: 14
Printed in France © AIRBUS 2008 All rights reserved

### Page 13 (OCR)

• A300-600  ©A300-600
SERVICE BULLETIN  SERVICE BULLETIN
(a)  Perform cut-out refer to SRM 54-51-31.  F. DOCUMENTATION
(b)  Do a one time Eddy Current inspection of cut-out (Refer to NTM 51-10-20 Part 6) to  Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.
ensure that the crack is totally removed.
(c)  Install :
Doubler  A5461255220000
Doubler  A5461255220100
Shim  R5461012420200
with :
Washer  A5461255320000
Washer  A5461255420000
Screw  ASNA2314-6-14
Screw  ASNA2314-6-16
Screw  ASNA2314-4-13
Screw  NAS1154-13
4 -  Screw  NAS1153E3
Nut  NAS1726-6E
Nut  NAS1726-4E
16  Rivet  NSA5414-36-20
(d)  New inspection program after embodiment of the repair.
1 Do a detailed visual inspection (Refer to NTM 51-70-00 Part 7) of doubler, only
at ribB, refer to Figure 2, Sheet 1.
(2)  Config. 02 thru Config, 03
(a)  If crack detected, contact AIRBUS.
D. TEST
None
E.  CLOSE UP
(1) Config. 01 thru Config. 03
(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: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
• REVISION No. : 02 - Jun 26/08  Page : 15  REVISION No. : 02 - Jun 26/08  Page : 16
Printed in France @ AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 14 (OCR)

•A300-600  SA300-600
SERVICE BULLETIN  SERVICE BULLETIN
PW PYLON SHOWN
INSPECTION IDENTICAL FOW GE PYLON  INSPECTION IDENTICAL FOR GE PYLON
EAS TO I
CUT-OUT
777 DETAILED VISUAL INSPECTION AREA
D_SB_546015_5_AFXX_01_00  D_SB_546015_5_AGXX_01_00
Figure 1, Sheet 1  Figure 2, Sheet 1
Config. 01: Inspection Area  Config. 02: Inspection Area
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. • A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 17  REVISION No. : 02 - Jun 26/08  Page : 18
Printed in France © AIRBUS 2008 All robis reserved

### Page 15 (OCR)

•A300-600  © A300-600
SERVICE BULLETIN  SERVICE BULLETIN
DO A DETAILED VISUAL INSPECTION
SIDE PANELS ON THE PYLONS 1 AND 2
ER TO NTM 51-70-00 PART 7) AT THE THRESHOLL
IVEN IN PLANNING INFORMATION PARAGRAPH E.(2)
SEE SHEET 2
VISUAL DETAILED  ISPECTION DOUBLER  INSPECTION I  SEND TO AIRBU  SERVICE BULLETIN  APPLY THE
EFER TO APPENDI  1300-54-6021
W0000 1008120059
ISPECTION EDD
CURREN
RE-INSPECT AT THE
O FART 7
ARAGRAPH E.(2)
CONTACT AIRBUS
BEFORE
A-A  NEXT FLIGHT
HE IN A DETAILED ENTAL
51-70-00 PART 7)
ARAGRAPH E.(2)
FINDING
RIGHT PYLON SHOWN
EFT PYLON SYMMETRICAL  ACTION
W PYLON SHOWN.  DENTICAL FOR GE PYLON INSPECTION
DETAILED VISUAL INSPECTION AREA  QUESTION
D_SB_546015_5_AHXX_01_00  D_SB_546015_5_ABXX_01_00
Figure 3, Sheet 1  Figure 4, Sheet 1
Config. 03: Inspection Area  Config. 01 thru 03: Flow Chart
DATE: Jul 13/07  SERVICE BULLETIN No.: A300-54-6015  DATE • Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page: 19  REVISION No. : 02 - Jun 26/08  Page : 20
Printed in France © AIRBUS 2008 All rights reserved

### Page 16 (OCR)

• A300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
FROM SHEET 1
- YES
REPAIR AS PER SRM
DURING REPAIR EMBO
DO ONE TIME HFEC INSPECTION OF CUT OUT
This Page Intentionally Left Blank
CONTACT AIRBUS
BEFORE
NEXT FLIGHT
SEND TO AIRBUS
INCBECTION REPORT
REFER TO APPENDIX 2
QUESTION
ACTION
FINDING
D_SB_546015_5_ABXX_02_00
Figure 4, Sheet 2
Config. 01 thru 03 : Flow Chart
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page: 21  REVISION No. : 02 - Jun 26/08  Page : 22
Printed in France © AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 17 (OCR)

GA300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
APPENDIX 1  APPENDIX 1
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
ATA SYSTEM: 54
TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.
MODIFICATION No. : None
W PYLON SHOWI
INSPECTION REPORT  ISPECTION IDENTICAL FOR GE PYLOI
THE RESULTS OF THE INSPECTION, INCLUDING NO FINDINGS, REPLACEMENT OR ACTIONS
TO BE DONE, MUST BE FORWARDED TO AIRBUS DEPT. AI/SBWST, ON THE ATTACHED
INSPECTION REPORT SHEET.
LENGTH  + + + +
+ + t
D_SB_546015_5_ACXX_01_00
Figure 1, Sheet 1
Config. 01: Inspection Report
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 1  REVISION No. : 02 - Jun 26/08  Page : 2
Printed in France @AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 18 (OCR)

© A300-600  SA300-600
SERVICE BULLETIN  SERVICE BULLETIN
APPENDIX 1  APPENDIX 1
INSPECTION REPORT
SERVICE BULLETIN No.: A300-54-6015
A/C MSN:  DATE OF INSPECTION:
FLIGHT CYCLES:  INSPECTION METHOD; C VISUAL DETAILED
FLIGHT HOURS:  FINDINGS:  YES O  NO O
INSPECTION  VISUAL  CHACK  CRACK LENGHT  REPAIR
< 25mm (0.984in.)  > 25mm (0,984(n.)
RH SIDE
PYLON
LH SIDE
This Page Intentionally Left Blank
RH SIDE
PYLON
LH SIDE
IF REPAIR, FILL IN THE TABLE BELOW
ONE TIME EDDY CURRENT INSPECTION
NO CRACK  CRACK LENGTH
RH SIDE
PYLON
LH SIDE
RH SIDE
PYLON
LH SIDE
D_SB_546015_5_ACXX_02_00
Figure 1, Sheet 2
Config. 01: Inspection Report
DATE: Jul 13/07  SERVICE BULLETIN No. • A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 3  REVISION No. : 02 - Jun 26/08  Page : 4
Printed in France © AIRBUS 2008 All rights reservad  Printed in France @AIRBUS 2008 All rights raserved

### Page 19 (OCR)

• A300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
APPENDIX 2  APPENDIX 2
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
ATA SYSTEM: 54
TITLE : NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.
MODIFICATION No. : None
W PYLON SHOWI
INSPECTION REPORT  ISPECTION IDENTICAL FOR GE PYLO
THE RESULTS OF THE INSPECTION, INCLUDING NO FINDINGS, REPLACEMENT OR ACTIONS
TO BE DONE, MUST BE FORWARDED TO AIRBUS DEPT. AI/SBWST, ON THE ATTACHED
INSPECTION REPORT SHEET.
CUT-OUT
/ DETAILED VISUAL INSPECTION AREA
D_SB_546015 5 ADXX 01_00
Figure 1, Sheet 1
Config. 02: Inspection Report After Repair (Refer to SRM 54-51-31).
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 1  REVISION No. : 02 - Jun 26/08  Page : 2
Printed in France © AIRBUS 2008 All rights reserved  Prinied in France © AIRBUS 2008 All rights reserved

### Page 20 (OCR)

©A300-600  SA300-600
SERVICE BULLETIN  SERVICE BULLETIN
APPENDIX 2  APPENDIX 2
INSPECTION REPORT AFTER REPAIR IN ACCORDANCE WITH SRM 54-51-31
SERVICE BULLETIN No.: A300-54-6015
A/C MSN :  DATE OF INSPECTION:
FLIGHT CYCLES:  INSPECTION METHOD: C VISUAL DETAILED
FLIGHT HOURS:  FINDINGS:  YES O  NO •
M PECTOM  CRACK
AH SIDE
PYLON
LH SIDE  This Page Intentionally Left Blank
AH SIDE
PRON
LH SIDE
D_SB SB_546015_5_ADXX_02_01
Figure 1, Sheet 2
Config. 02 : Inspection Report After Repair (Refer to SRM 54-51-31).
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 3  REVISION No. : 02 - Jun 26/08  Page : 4
Printed in France ® AIRBUS 2008 All rights reserved

### Page 21 (OCR)

• A300-600  © A300-600
SERVICE BULLETIN  SERVICE BULLETIN
APPENDIX 3  APPENDIX 3
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
ATA SYSTEM : 54
TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.
MODIFICATION No. : None
INSPECTION REPORT  VISUAL DETAILED  SPECTION DOUBLER  NSPECTION IDENTICAL FOR GE PYLON  A PALON SHOWN
THE RESULTS OF THE INSPECTION, INCLUDING NO FINDINGS, REPLACEMENT OR ACTIONS
TO BE DONE, MUST BE FORWARDED TO AIRBUS DEPT. AI/SBWST ON THE ATTACHED
INSPECTION REPORT SHEET.  INSPECTION EDDY  CURRENT
A-A
RIBB
777 DETAILED VISUAL INSPECTION AREA
D_SB_546016_5_AEXX_01_00
Figure 1, Sheet 1
Config. 03: Inspection Report After Embodiment of the Service Bulletin No. A300-54-6021
DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 1  REVISION No. : 02 - Jun 26/08  Page : 2
Printed in France © AIRBUS 2008 All rights reserved

### Page 22 (OCR)

SA300-600  © A300-600
SERVICE BULLETIN  SERVICE BULLETIN
APPENDIX 3  APPENDIX 3
INSPECTION REPORT
AFTER EMBODIMENT OF THE SERVICE BULLETIN No. A300-54-6015
AVC MSN :  DATE OF INSPECTION:
FLIGHT CYCLES:  INSPECTION METHOD: • VISUAL DETAILED
FLIGHT HOURS:  FINDINGS:  YES D  • EDDY CURRENT  NO •
CURRENT INSFECTION  ONE TIME EY  VISUAL DETAILED INSPECTION
CRACK  LENGHT  CAĂCK
RH SIDE  This Page Intentionally Left Blank
PYLON
LH SIDE
RH SIDE
PYLON
LH SIDE
D SB 546015 5 AEXX 02 00
Figure 1, Sheet 2
Config. 03: Inspection Report After Embodiment of the Service Bulletin No. A300-54-6021
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page : 3  REVISION No. : 02 - Jun 26/08  Page : 4
Printed in France © AIRBUS 2008 All rights reserved  Printed in France © AIRBUS 2008 All rights reserved

### Page 23 (OCR)

• A300-600  • A300-600
SERVICE BULLETIN  SERVICE BULLETIN
REPORTING SHEET  REPORTING QUALITY
TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.  TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB 8.
MODIFICATION No. : None  MODIFICATION No. : None
Please complete the appropriate item (A or B):  Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you
A - SB WILL BE embodied..........  .... YES/NO (if NO please comment)  provide us will be used to analyse areas of difficulties and to take corrective action to futher improve the quality
If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiement:  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)
B - SB HAS BEEN embodied on aircraft:
-Quality rating of this SB  4321
-Quality rating of the Accomplishment Instructions  4321
Operator comments:  -Quality rating of the Illustrations  4321
-Is this SB easy to understand?  Y/N
From Airline:..
Name/Title:.  If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short
Signature:  Date: .  description of the issue.
If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next  Material  Instructions
normal revision or prior to SB embodiment, please indicate required service(s):  X Effectivity  X Kit Content  X Preparation
Either  YES/NO  X Reason  X List of Materials  X Mod/Inspection
Or  : Intermediate/Temporary revision...  YES/NO  X Manpower  Operator Supplied  X Test
X References  X Re-identification  X Close-up
Important Information: This SB will only be incorporated in your maintenance and operational documentation  X Publication  X Tooling  X Illustrations
if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible
revision, this will result in  Comments :
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  Operator :  Date:
1 Rond Point Maurice Bellonte  31707 BLAGNAC CEDEX FRANCE  Name/Title :
Attn: SEDCC1 Technical Data and Documentation Services  Please return this form to:
FAX: (+33) 5 61 93 28 06
e-mail: sb.reporting@airbus.com  AIRBUS
Or via your Resident Customer Support Office.  CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
Alternatively, SB lists via letters or fax are also accepted.  31707 BLAGNAC CEDEX FRANCE
Attr: SEMB Service Bulletins Management
FAX: (+33) 5 61 93 42 51
Or via your Resident Customer Support Office.
DATE: Jul 13/07  SERVICE BULLETIN No. : A300-54-6015  DATE : Jul 13/07  SERVICE BULLETIN No. : A300-54-6015
REVISION No. : 02 - Jun 26/08  Page: 1 of 1  REVISION No. : 02 - Jun 26/08  Page : 1 of 1
Printed in France ® AIRBUS 2008 All righis reserved  Printed in France @AIRBUS 2008 All rights reserved

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