# Airbus Service Bulletin A300-57-6028

Copy: Revision 07 ("SB_A300-57-6028_Rev 07"), 24 pages: PDF https://openairdocs.org/files/sha256/3d/9a/3d9a2a81922a72f0eeeb2b49373b386834a41844f2ecc5a69821af12b9d969dd; text https://openairdocs.org/service-documents/airbus/a300-57-6028/file/3d9a2a81922a.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2015-4817; AD 2016-07-20 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A300-57-6028
- Latest revision known: A300-57-6028, Revision 07, dated June 6, 2011 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/airbus/a300-57-6028

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

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

- [AD 2016-07-20](https://openairdocs.org/ad/2016-07-20.md), effective May 16, 2016: Revisions 3, 04, 05, 06 and 07
- [AD 95-18-08](https://openairdocs.org/ad/95-18-08.md), effective Oct 16, 1995: Revision 3

Also cited in [2 proposed ADs](https://openairdocs.org/service-documents/airbus/a300-57-6028/proposed.md).

## Text (24 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2015-4817; AD 2016-07-20 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Some pages are 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

A300-600A300-600
SERVICE BULLETIN
REVISION TRANSMITT AL SHEET
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Tel : (33) 5 61 93 33 33
Telex : AIRBU 530526F
Fax : (33) 5 61 93 42 51
MANDATORY MANDATORY MANDATORY MANDATORY
ATA SYSTEM : 57
TITLE : WINGS - INSPECTION OF THE BOTTOM SKIN ADJACENT TO THE PYLON REAR ATTACHMENT
FITTING
MODIFICATION No. : None
This page transmits Revision No. 07 of Service Bulletin No. A300-57-6028.
ADDITIONAL WORK
No additional work is required by this revision for aircraft modified by any previous issue.
REASON
This Service Bulletin has been raised in issue to include revised thresholds and intervals (including
Flight Hour (FH) conversions as well as Flight Cycles (FC)) to support operation to ESG2.
CHANGES
SUMMARY :
- REASON/DESCRIPTION/OPERA TIONAL CONSEQUENCES
. AD reference has been removed and yes added to Evaluation T able.
- EFFECTIVITY
. Effectivity has been updated.
PLANNING INFORMA TION :
- EFFECTIVITY
. 1.A. Effectivity updated.
- REASON
- Objective/Action
. 1.C.(2) Minor correction.
- COMPLIANCE
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REVISION No. : 07 - Jun 06/11 Page : 1 of 3
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A300-600A300-600
SERVICE BULLETIN
REVISION TRANSMITT AL SHEET
- Accomplishment Timescale
. 1.E.(2)(a) AD reference revised.
. 1.E.(2)(b) T ables 1 thru 4 added.
- INDUSTRIAL SUPPORT
. 2.B. Standard sentence revised to latest standard.
ACCOMPLISHMENT INSTRUCTIONS :
- GENERAL
. 3.A. Caution revised to latest standard.
- INSPECTION
. 3.B.(1)(c) Reference to T ables 1 thru 4 added.
- REP AIR
. 3.C.(1)(a) Minor correction.
FILING INSTRUCTIONS
This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision T ransmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS
Revision 02 of this Service Bulletin was issued to add an aircraft effectivity list and delete Appendix 1
which contained the NTM procedure.
Revision 03 was issued to add the aircraft model F4-605R and update the effectivity .
Revision 04 was issued to add aircraft model C4-605R/F and MSN 0755 and 0758 to the effectivity .
Change notice 3A was also incorporated, this introduced the Airworthiness Directive 94-069-158(B).
Revision 05 was issued to add the aircraft model F4-622R and update the effectivity .
Revision 06 was issued to increase the effectivity to MSN 878. A reference was amended and the
opportunity was taken to update the MSN per operator list. Minor changes to the new Service Bulletin
format were also added.
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A300-600A300-600
SERVICE BULLETIN
REVISION TRANSMITT AL SHEET
REVISION SEQUENCE
ORIGINAL : May 31/91
REVISION No. : 01 - Sep 23/91
REVISION No. : 02 - Feb 22/94
REVISION No. : 03 - Sep 13/94
REVISION No. : 04 - Oct 25/99
REVISION No. : 05 - Jan 25/02
REVISION No. : 06 - May 17/06
REVISION No. : 07 - Jun 06/11
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A300-600A300-600
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
MANDATORY MANDATORY MANDATORY MANDATORY
ATA SYSTEM : 57
TITLE : WINGS - INSPECTION OF THE BOTTOM SKIN ADJACENT TO THE PYLON REAR ATTACHMENT
FITTING
MODIFICATION No. : None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
During full scale fatigue testing, a crack was discovered in the bottom skin adjacent to the aft pylon attachment
fitting at approximately 58,650 simulated flights.
There is a possibility of a similar crack appearing in service which would require extensive repairs.
EVALUA TION T ABLE
COMPLIANCE Mandatory CANCELS INSPECTION SB No
AD Ye s A/C OPERA TION AFFECTED No
RELIABILITY AFFECTED Ye s P AX COMFORT AFFECTED No
COST SAVING No ETOPS AFFECTED No
STRUCTURAL LIFE EXTN No VENDOR SB INVOL VED No
KIT PRICE (USD) No AIRBUS kit
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A300-600A300-600
SERVICE BULLETIN
SUMMARY
EFFECTIVITY
This Service Bulletin is applicable to this (these) operator(s) :
66U AAL AAW ABD AHK AMU CES CSN DLH F2I FDX G8E IRA IRM JAL KAC KAL LAA MNB MON MSR
MXU OHY QTR SUD T AR THA TMA UPS UZB
CONCURRENT REQUIREMENTS
None
REFERENCES/REPERCUSSIONS
TFU : None
OEB : None
AOT : None
SIL : None
LIFE LIMIT : None
LINE MAINTENANCE AFFECTED : No
OTHERS : None
NATURE OF THE WORK
AIRCRAFT : Y es
EQUIPMENT : No
HARD : No
SOFT : No
OBRM : No
MANPOWER
Config. 01
TOTAL MANHOURS 6.0
ELAPSED TIME (HOURS) 3.0
MATERIAL INFORMATION
AIRCRAFT DA T A
None
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A300-600A300-600
SERVICE BULLETIN
SUMMARY
APPENDICES
None
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A300-600A300-600
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
MANDATORY MANDATORY MANDATORY MANDATORY
ATA SYSTEM : 57
TITLE : WINGS - INSPECTION OF THE BOTTOM SKIN ADJACENT TO THE PYLON REAR ATTACHMENT
FITTING
MODIFICATION No. : None
This document contains AIRBUS PROPRIET ARY INFORMA TION 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. P LANNING INFORMATION
A. E FFECTIVITY
(1) Models
B4-601 B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/F C4-620 F4-605R F4-622R
(2) Aircraft
(a) Effectivity by MSN
This Service Bulletin is applicable to aircraft MSN :
0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348 0351 0354 0358 0361
0365 0368 0380 0388 0398 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469
0470 0474 0477 0479 0505-0518 0521 0525 0529 0530 0532 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 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 0721-0750 0752-0764 0766-0775
0777-0794 0797 0799-0841 0845-0878
(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
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A300-600A300-600
SERVICE BULLETIN
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.
OPERA TOR MSN
66U 0762
AAL 0423 0459 0460 0461 0463 0466 0469 0470 0474 0506 0507 0508
0509 0510 0511 0512 0513 0514 0515 0516 0517 0606 0610 0612
0615 0619 0626 0639 0643 0645 0675
AAW 0354
ABD 0529 0557 0755
AHK 0855 0856 0857 0858 0859 0860 0870 0871
AMU 0677 0743
CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763
CSN 0733 0734 0739 0750 0756
DLH 0380 0401 0405 0623 0701 0773
F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0408 0618
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 0726 0728 0735 0736 0738 0742 0745
0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774
0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799
0800 0801 0802 0803 0804 0873 0874 0875 0876 0877 0878
G8E 0462 0465
IRA 0632 0696 0723 0727
IRM 0411 0414 0546 0553 0608
JAL 0602 0617 0621 0637 0641 0670 0679 0683 0703 0711 0724 0729
0730 0737 0740 0753 0770 0783 0797 0836 0837 0838
KAC 0344 0673 0694 0699 0719 0721
KAL 0582 0609 0627 0631 0662 0685 0692 0731
LAA 0601 0616
MNB 0758
MON 0540 0556 0604 0605
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A300-600A300-600
SERVICE BULLETIN
OPERA TOR MSN
MSR 0561 0607
MXU 0767 0788
OHY 0584 0603 0744 0747 0749 0764
QTR 0554 0560 0614
SUD 0666 0775
T AR 0505 0558 0563
THA 0368 0398 0464 0518 0566 0569 0577 0628 0629 0635 0681 0705
0782 0784 0785 0786 0787
TMA 0872
UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816
0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828
0829 0830 0831 0832 0833 0834 0835 0839 0840 0841 0845 0846
0847 0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864
0865 0866 0867 0868 0869
UZB 0717 0722
(c) Effectivity by MSN and Kit/Configuration
The Kits and configurations applicable to these MSNs are given at the end of this list
0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0354 0358 0361 0365
0368 0380 0388 0398 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0470
0474 0477 0479 0505-0518 0521 0525 0529-0530 0532 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 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 0721-0750 0752-0764 0766-0775
0777-0794 0797 0799-0841 0845-0878
KIT No. QTY PER A/C CONFIGURA TION
None 01
NOTE : Config. 01 is valid for all the aircraft given in the effectivity of this
Service Bulletin.
(3) Spares
None
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A300-600A300-600
SERVICE BULLETIN
B. C ONCURRENT REQUIREMENTS
None
C. R EASON
(1) History
During full scale fatigue testing, a crack was discovered in the bottom skin adjacent to the
aft pylon attachment fitting at approximately 58,650 simulated flights.
There is a possibility of a similar crack appearing in service which would require extensive
repairs.
(2) Objective/Action
Mandatory Detailed Visual Inspections (DVI) of the wing bottom skin are required in the
area of the cut-out for the pylon rear attachment fitting.
(3) Advantages
Early detection of cracks in this area may prevent the necessity for expensive and time
consuming repairs.
(4) Operational/Maintenance Consequences
None
D. D ESCRIPTION
T o accomplish this Service Bulletin it is necessary to :
(1) Config. 01
(a) Get access to the engine pylon in the area of the center spar.
(b) Remove the pylon fairing panels 473BL, 474BR, 483BL and 484BR.
(c) Do a Detailed Visual inspection of the wing bottom skin at the cut out for the pylon
rear attachment fitting.
(d) Do any necessary repairs.
(e) Remove any tools and clean the work area.
(f) Install the pylon fairing panels 473BL, 474BR, 483BL and 484BR.
E. C OMPLIANCE
(1) Classification
Mandatory
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A300-600A300-600
SERVICE BULLETIN
(2) Accomplishment Timescale
(a) Accomplishment of this Service Bulletin has been rendered mandatory by the issue
of an Airworthiness Directive (AD) published by the European Aviation Safety
Agency (EASA). The AD must be used as the reference document for the mandatory
accomplishment timescale.
(b) Detailed Visual inspections are required within the number of Flight Cycles (FC) /
Flight Hours (FH) that follow:
T able 1. Normal Range Operation - Freighter Aircraft
Normal Range Operation - A300F4-600R
Threshold Inspection Interval Inspection Grace PeriodInspection
Method FC FH FC FH FC FH
DVI 24,000 51,800 9,000 19,400 2,000 4,300
T able 2. Short Range Operation - Freighter Aircraft
Short Range Operation (Average Flight Time less than 1.5 Hours) - A300F4-600R
Threshold Inspection Interval Inspection Grace PeriodInspection
Method FC FH FC FH FC FH
DVI 25,900 38,800 9,700 14,500 2,100 3,200
T able 3. Normal Range Operation - Passenger Aircraft
Normal Range Operation - A300B4-600(R), A300C4-600(R)
Threshold Inspection Interval Inspection Grace PeriodInspection
Method FC FH FC FH FC FH
DVI 19,100 41,200 7,100 15,300 1,500 3,200
T able 4. Short Range Operation - Passenger Aircraft
Short Range Operation (Average Flight Time less than 1.5 Hours) - A300B4-600(R), A300C4-600(R)
Threshold Inspection Interval Inspection Grace PeriodInspection
Method FC FH FC FH FC FH
DVI 20,600 30,900 7,600 11,500 1,600 2,400
Grace periods are to be applied for aircraft approaching or which have exceeded the
Inspection threshold/interval.
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A300-600A300-600
SERVICE BULLETIN
F. A PPROVAL
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. M ANPOWER
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.
Config. 01
Get Access 2.0
Skin Inspection 2.0
Close Up 2.0
TOTAL MANHOURS 6.0
ELAPSED TIME (HOURS) 3.0
H. W EIGHT AND BALANCE
Not changed
I. E LECTRICAL LOAD DATA
Not changed
J. R EFERENCES
Aircraft Maintenance Manual (AMM) : 24-00-00 54-50-00
Elec. Std. Practices Manual (ESPM) : 20-55-00
Structural Repair Manual (SRM) : 51-10-13
Repair Instruction : R57140141
K. P UBLICATIONS AFFECTED
None
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L. I NTERCHANGEABILITY/MIXABILITY
None
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A300-600A300-600
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2. M ATERIAL INFORMATION
A. M ATERIAL - PRICE AND AVAILABILITY
None
B. I NDUSTRY SUPPORT INFORMATION
AIRBUS will not provide industry support for accomplishment of this Service Bulletin.
C. L IST OF COMPONENTS
None
D. L IST OF MATERIALS - OPERATOR SUPPLIED
None
E. P ARTS TO BE RE-IDENTIFIED BY THE OPERATOR
None
F. T OOLING - PRICE AND AVAILABILITY
None
G. S PECIAL TOOLS
None
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A300-600A300-600
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3. A CCOMPLISHMENT INSTRUCTIONS
A. G ENERAL
WARNING : MAKE SURE THA T YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
WARNING : LANDING GEAR - MAKE SURE THA T THE GROUND SAFETIES ARE IN
POSITION.
WARNING : FLIGHT CONTROLS - MAKE SURE THA T THE GROUND SAFETIES AND
NOTICES ARE IN POSITION.
CAUTION : ALWAYS OBEY THE PRECAUTIONS THA T FOLLOW TO KEEP ELECTRICAL
WIRING IN A SA TISFACTORY CONDITION (ELECTRICALL Y AND MECHANICALL Y
SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REP AIRS OR
MODIFICA TIONS, ALWA YS 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
- REGULARL Y REMOVE ALL SHAVINGS, UNWANTED MA TERIAL AND OTHER
CONT AMINA TION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONT AMINA TION AND
DAMAGE TO THE ELECTRICAL WIRING INST ALLA TION.
IN CASE OF CONT AMINA TION, REFER TO ESPM 20-55-00, CLEANING.
(1) Preparation
(a) Config. 01
1 Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00,
Page block 301).
2 Put access platforms in position.
3 Remove the pylon fairing panels 473BL, 474BR, 483BL and 484BR (Refer
to AMM 54-50-00, Page block 401).
(2) Standard Practices
None
B. I NSPECTION
(1) Config. 01
(a) Do a Detailed Visual inspection of the wing bottom skin in the area of the cut out for
the pylon rear attachment fitting (Refer to Figure 1)
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A300-600A300-600
SERVICE BULLETIN
(b) If there are crack findings report to AIRBUS for an approved repair before the
next flight (Refer to SRM 51-10-13).
(c) Repeat inspections are to be done at intervals defined in T ables 1 thru 4 as
necessary.
C. R EPAIR
(1) Config. 01
(a) Repair instructions will be made available upon application to AIRBUS.
D. T EST
None
E. C LOSE UP
(1) Config. 01
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Install the pylon fairing panels 473BL, 474BR, 483BL and 484BR (Refer to AMM
54-50-00, Page block 401).
(c) Report all findings including nil findings to SEE8. (Refer to SRM 51-10-13).
F. D OCUMENTATION
Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.
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© A300-600
SERVICE BULLETIN
+  +  + _ ++
76 79 82 84 86f 88 99t  795798107105195107
SPAR  53 57 6465 6973-7780,83+587 89 9796  196, 98,100, 17 + 176
+ +
REAR PYLON FITTING
RIB 7  RIB 8
DB7 57 6028 AA AA A
Figure 1, Sheet 1
Config. 01: Plan View on Bottom Skin (Bolt Numbering In Accordance With R571 40141 Sheet 15)
DATE: May 31/91  SERVICE BULLETIN No. : А300-57-6028
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REPORTING SHEET
TITLE : WINGS - INSPECTION OF THE BOTTOM SKIN ADJACENT TO THE PYLON REAR ATTACHMENT
FITTING
MODIFICATION No. : None
Please complete the appropriate item (A or B):
A - SB W ILL BE embodied .................................................................. YES/NO (if NO please comment)
If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiement:
.............................................................................................................................................................................
.............................................................................................................................................................................
B - SB H AS 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 : Advance data................................................................................... YES/NO
Or : Intermediate/T emporary 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 DIRECTORA TE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn: SEDCC1 T echnical 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.
DA TE : May 31/91 SERVICE BULLETIN No. : A300-57-6028
REVISION No. : 07 - Jun 06/11 Page : 1 of 1
Printed in France © AIRBUS 2008 All rights reserved

### Page 24

A300-600A300-600
SERVICE BULLETIN
REPORTING QUALITY
TITLE : WINGS - INSPECTION OF THE BOTTOM SKIN ADJACENT TO THE PYLON REAR ATTACHMENT
FITTING
MODIFICATION No. : None
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 futher 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 4 3 2 1
-Quality rating of the Accomplishment Instructions 4 3 2 1
-Quality rating of the Illustrations 4 3 2 1
-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 X Mod/Inspection
X Manpower Operator Supplied X T est
X References X Re-identification X Close-up
X Publication X T ooling X Illustrations
Comments :
Operator : Date:
Name/Title :
Please return this form to:
AIRBUS
CUSTOMER SERVICES DIRECTORA TE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn: SEMB Service Bulletins Management
FAX: (+33) 5 61 93 42 51
Or via your Resident Customer Support Office.
DA TE : May 31/91 SERVICE BULLETIN No. : A300-57-6028
REVISION No. : 07 - Jun 06/11 Page : 1 of 1
Printed in France © AIRBUS 2008 All rights reserved

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