A300-600 A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY 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/OPERATIONAL CONSEQUENCES

. AD reference has been removed and yes added to Evaluation Table.

- EFFECTIVITY

. Effectivity has been updated.

PLANNING INFORMATION :

- EFFECTIVITY

. 1.A. Effectivity updated.

- REASON

- Objective/Action

. 1.C.(2) Minor correction.

- COMPLIANCE

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 1 of 3

Printed in France © AIRBUS 2008 All rights reserved
A300-600 A300-600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- Accomplishment Timescale

. 1.E.(2)(a) AD reference revised.

. 1.E.(2)(b) Tables 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 Tables 1 thru 4 added.

- REPAIR

. 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 Transmittal 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.

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 2

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SERVICE BULLETIN

REVISION TRANSMITTAL 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

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 3

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 4

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is

not approved for modification of the aircraft

MANDATORY MANDATORY MANDATORY 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.

EVALUATION TABLE

COMPLIANCE Mandatory CANCELS INSPECTION SB No

AD Yes A/C OPERATION AFFECTED No

RELIABILITY AFFECTED Yes PAX COMFORT AFFECTED No

COST SAVING No ETOPS AFFECTED No

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED No

KIT PRICE (USD) No AIRBUS kit

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 1 of 3

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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 TAR 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 : Yes

EQUIPMENT : No

HARD : No

SOFT : No

OBRM : No

MANPOWER

Config. 01

TOTAL MANHOURS 6.0

ELAPSED TIME (HOURS) 3.0

MATERIAL INFORMATION

AIRCRAFT DATA

None

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 2

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SERVICE BULLETIN

SUMMARY

APPENDICES

None

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 3

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 4

Printed in France © AIRBUS 2008 All rights reserved
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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY 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 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

A. EFFECTIVITY

(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

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 1 of 13

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A300-600 A300-600

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.

OPERATOR 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

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 2

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SERVICE BULLETIN

OPERATOR MSN

MSR 0561 0607

MXU 0767 0788

OHY 0584 0603 0744 0747 0749 0764

QTR 0554 0560 0614

SUD 0666 0775

TAR 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 CONFIGURATION

None 01

NOTE : Config. 01 is valid for all the aircraft given in the effectivity of this

Service Bulletin.

(3) Spares

None

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 3

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SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

None

C. REASON

(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. DESCRIPTION

To 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. COMPLIANCE

(1) Classification

Mandatory

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 4

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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:

Table 1. Normal Range Operation - Freighter Aircraft

Normal Range Operation - A300F4-600R

Inspection Threshold Inspection Interval Inspection Grace Period

Method FC FH FC FH FC FH

DVI 24,000 51,800 9,000 19,400 2,000 4,300

Table 2. Short Range Operation - Freighter Aircraft

Short Range Operation (Average Flight Time less than 1.5 Hours) - A300F4-600R

Inspection Threshold Inspection Interval Inspection Grace Period

Method FC FH FC FH FC FH

DVI 25,900 38,800 9,700 14,500 2,100 3,200

Table 3. Normal Range Operation - Passenger Aircraft

Normal Range Operation - A300B4-600(R), A300C4-600(R)

Inspection Threshold Inspection Interval Inspection Grace Period

Method FC FH FC FH FC FH

DVI 19,100 41,200 7,100 15,300 1,500 3,200

Table 4. Short Range Operation - Passenger Aircraft

Short Range Operation (Average Flight Time less than 1.5 Hours) - A300B4-600(R), A300C4-600(R)

Inspection Threshold Inspection Interval Inspection Grace Period

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.

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 5

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SERVICE BULLETIN

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.

Config. 01

Get Access 2.0

Skin Inspection 2.0

Close Up 2.0

TOTAL MANHOURS 6.0

ELAPSED TIME (HOURS) 3.0

H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

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. PUBLICATIONS AFFECTED

None

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

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L. INTERCHANGEABILITY/MIXABILITY

None

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

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This Page Intentionally Left Blank

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

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2. MATERIAL INFORMATION

A. MATERIAL - PRICE AND AVAILABILITY

None

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

None

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY THE OPERATOR

None

F. TOOLING - PRICE AND AVAILABILITY

None

G. SPECIAL TOOLS

None

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING : LANDING GEAR - MAKE SURE THAT THE GROUND SAFETIES ARE IN

POSITION.

WARNING : FLIGHT CONTROLS - MAKE SURE THAT THE GROUND SAFETIES AND

NOTICES ARE IN POSITION.

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, 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. INSPECTION

(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)

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

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(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 Tables 1 thru 4 as

necessary.

C. REPAIR

(1) Config. 01

(a) Repair instructions will be made available upon application to AIRBUS.

D. TEST

None

E. CLOSE 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. DOCUMENTATION

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

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

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SERVICE BULLETIN

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. : A300-57-6028

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DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

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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 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 embodiement:

.............................................................................................................................................................................

.............................................................................................................................................................................

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 : Advance data................................................................................... YES/NO

Or : Intermediate/Temporary 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: SEDCC1 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 : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 1 of 1

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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 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: SEMB Service Bulletins Management

FAX: (+33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE : May 31/91 SERVICE BULLETIN No. : A300-57-6028

REVISION No. : 07 - Jun 06/11 Page : 1 of 1

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