@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.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 29

TITLE: HYDRAULIC POWER - BRACKETS AND SUPPORTS- HYDRAULIC

COMPARTMENT - INSTALL PLACARD FOR HYDRAULIC

ACCUMULATOR

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 13540S22823

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Old generation of hydraulic accumulators (pre 1984) have three welds. They can cause damage on the

systems if the accumulators burst.

A modification has been developed to change the design from three welds to one weld and to install

placard to indicate area where hydraulic accumulators of old generation are forbidden.

Installation of accumulators with only one weld (post 1984) will be allowed.

This Service Bulletin requires installing :

- A support bracket and placard adjacent to the blue hydraulic system accumulator.

Accomplishment of this Service Bulletin will avoid inadvertent installation of (pre 1984) accumulator.

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

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 296064A01R00 1 219.00 Support

EFFECTIVITY

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

66U 83V AAL AAW ABD AHK AMU CES CSN DLH F2I FDX G8E

IRA IRM JAL KAC KAL LAA MNB MON MSR MXU NMB OHY QTR

SUD TAR THA TMA UPS UZB

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the following

Service Bulletin :

A300-29-6063

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 296064-831-801-001: Modification

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

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SERVICE BULLETIN

SUMMARY

APPENDICES

None

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-6064

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SERVICE BULLETIN

SUMMARY

**CONF ALL

FR53

SUPPORT AND PLACARD

A

B

Z147 Z148 − 

A

FR47

FR54

B 292070

D_SB_296064_5_SAAA_01_02

TO BE INSTALLED

Figure A-FSAAA - Sheet 01

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-6064

REVISION No.: 00 - Aug 12/10 Page: 4

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@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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 29

TITLE: HYDRAULIC POWER - BRACKETS AND SUPPORTS- HYDRAULIC

COMPARTMENT - INSTALL PLACARD FOR HYDRAULIC

ACCUMULATOR

MODIFICATION No.: 13540S22823

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 modification is applicable by Service Bulletin only.

(1) Models

B4-601 B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/FC4-620

F4-605R F4-622R

(2) Effectivity by MSN

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

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SERVICE BULLETIN

(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

66U 0750 0762

83V 0423 0459 0460 0510 0511 0512 0615 0619

AAL 0461 0463 0466 0469 0470 0474 0506 0507 0508 0509 0513 0514

0515 0516 0517 0606 0610 0612 0626 0639 0643 0645 0675

AAW 0354

ABD 0529 0557

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 0756

DLH 0401 0405

F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351

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 0380 0408 0411 0414 0546 0553 0608 0618 0623 0701 0773

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

MSR 0561 0607

MXU 0767 0788

NMB 0755

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

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SERVICE BULLETIN

OPERATOR MSN

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

(4) Configuration by MSN

MSN CONFIGURATION

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 0460 0461 0462 0463 0464 0465

0466 0469 0470 0474 0477 0479 0505 0506 0507 0508 0509

0510 0511 0512 0513 0514 0515 0516 0517 0518 0521 0525

0529 0530 0532 0536 0540 0543 0546 0553 0554 0555 0556

0557 0558 0559 0560 0561 0563 0566 0569 0572 0575 0577

0579 0581 0582 0584 0601 0602 0603 0604 0605 0606 0607

0608 0609 0610 0611 0612 0613 0614 0615 0616 0617 0618

0619 0621 0623 0625 0626 0627 0628 0629 0630 0631 0632

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 0722 0723 0724 0725 0726 0727 0728

0729 0730 0731 0732 0733 0734 0735 0736 0737 0738 0739

0740 0741 0742 0743 0744 0745 0746 0747 0748 0749 0750

0752 0753 0754 0755 0756 0757 0758 0759 0760 0761 0762

0763 0764 0766 0767 0768 0769 0770 0771 0772 0773 0774

0775 0777 0778 0779 0780 0781 0782 0783 0784 0785 0786

0787 0788 0789 0790 0791 0792 0793 0794 0797 0799 0800

0801 0802 0803 0804 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 0836 0837 0838 0839 0840 0841 0845 0846 0847

0848 0849 0850 0851 0852 0853 0854 0855 0856 0857 0858

0859 0860 0861 0862 0863 0864 0865 0866 0867 0868 0869

0870 0871 0872 0873 0874 0875 0876 0877 0878

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 296064A01R00 1

Consumable CMLA01 1

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-6064

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SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the

following Service Bulletin :

A300-29-6063

C. REASON

(1) History

Old generation of hydraulic accumulators (pre 1984) have three welds. They can cause

damage on the systems if the accumulators burst.

A modification has been developed to change the design from three welds to one weld

and to install placard to indicate area where hydraulic accumulators of old generation are

forbidden.

Installation of accumulators with only one weld (post 1984) will be allowed.

(2) Objective/Action

This Service Bulletin requires installing :

- A support bracket and placard adjacent to the blue hydraulic system accumulator.

(3) Advantages

Accomplishment of this Service Bulletin will avoid inadvertent installation of (pre 1984)

accumulator.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 296064-831-801-001: Modification

(1) Install the Support and Placard of the Blue System Accumulator FIN 292070

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is requested within 6000 Flight Hours (FH) or 30

months after the issue date of the Service Bulletin whichever occurs first.

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-6064

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SERVICE BULLETIN

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the

issue of an Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals

and/or date) given above but reference should be made to the AD for confirmation of the

mandated accomplishment timescale.

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.

Task 296064-831-801-001: Modification

Get Access 1.00

On Aircraft

Install the Support and Placard of the Blue System

Accumulator FIN 292070

1.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 20-21-12 20-28-11 24-00-00

31-12-11 32-12-11

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-51-20 20-55-00

Service Bulletin (SB) A300-29-6063

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-24-00 51-40-20

51-40-30 51-40-40

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SERVICE BULLETIN

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 29-11-56

Illustrated Parts Catalog (IPC) 11-34-29

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-6064

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 296064A01R00 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 :

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet : http :

//spares.airbus.com

For ordering modification kits by fax : +49 40

50 76 25 90

For ordering of single spares by fax : +49 40

50 76 40 13

(2) Price and Availability

Kit 296064A01R00

Cost 219.00 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.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will provide a 10% reduction to the applicable sales prices given in the paragraph

’Price and Availability’ for orders placed before Dec 31/16.

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

C. LIST OF COMPONENTS

Kit 296064A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 A2913202500000 1 SUPPORT

2 ASNA2050DCJ3215 2 RIVET

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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

Interfay Sealant 09-005E As required

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

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 296064-831-801-001 - Modification

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

Zone

147

Access

Door 734

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

A. GENERAL

(1) Subtask 296064-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

(a) Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

(2) Subtask 296064-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Interfay Sealant 09-005E As required

Solvent General Purpose 11-026 As required

References

Aircraft Maintenance Manual (AMM) 20-21-12, Page Block 001

20-28-11, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-51-20

Structural Repair Manual (SRM) 51-23-10

51-24-00

51-40-20

51-40-30

51-40-40

(a) For the specifications of the materials numbers (Mat.No) (Refer to Consumable

Material List (CML)).

(b) For the removal and installation of fasteners (Refer to SRM 51-40-20).

(c) For alternative and substitute fasteners (Refer to SRM 51-40-30).

(d) For fastener hole diameters and drill data (Refer to SRM 51-40-40).

(e) To torque tighten the standard threaded fasteners (Refer to AMM 20-21-12, Page

Block 001).

(f) Use a non-metallic spatule to remove the sealant and clean the areas with :

Solvent General

Purpose

11-026 As required

(g) Apply :

Interfay Sealant 09-005E As required

to interfaces of structure and new parts, (Refer to SRM 51-24-00).

(h) Renew the protective finish, (Refer to SRM 51-23-10).

(i) Do the electrical bonding (Refer to ESPM 20-51-20 and AMM 20-28-11, Page Block

001).

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B. PREPARATION

(1) Subtask 296064-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301

32-12-11, Page Block 301

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

Block 301).

(b) Put access platform(s) in position.

(c) Open the LH main landing gear door 734 (Refer to AMM 32-12-11, Page Block

301).

C. PROCEDURE

(1) Subtask 296064-420-001-001 - Install the Support and Placard of the Blue System

Accumulator FIN 292070

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 734

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 296064A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A2913202500000 1 SUPPORT

2 ASNA2050DCJ3215 2 RIVET

References

Fig. A-FBAAA

Install the Support and Placard of the

Blue System Accumulator FIN 292070

Sheet 01

Sheet 02

(a) Put the support and placard Item 1 in position as shown in Fig. A-FBAAA Sheet 01

and Fig. A-FBAAA Sheet 02.

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SERVICE BULLETIN

(b) Drill two holes on the structure to a diameter between 3.25 mm (0.128 in.) and 3.35

mm (0.132 in.) to match the holes of the support Item 1 as shown in Fig. A-FBAAA

Sheet 02.

(c) Install :

1 Support A2913202500000 Item 1

2 Rivet ASNA2050DCJ3215 Item 2

D. TEST

None

E. CLOSE-UP

(1) Subtask 296064-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-12-11, Page Block 301

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

equipment

(b) Close the LH main landing gear door 734 (Refer to AMM 31-12-11, Page Block

301).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating conditions.

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**CONF ALL

FR53

99 mm

(3.898 in)

C

1

B

A

Z147 Z148 − 

A

FR47

FR54

B 292070

D_SB_296064_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Install the Support and Placard of the Blue System Accumulator FIN 292070

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-6064

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**CONF ALL

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

3.25 mm

(0.128 in)

3.35 mm

(0.132 in) 2 ASNA2050DCJ3215 RIVET

1

VIEW LOOKING FORWARD

D_SB_296064_5_BAAA_02_01

N

HEAD ON VISIBLE FACE

N

C

Figure A-FBAAA - Sheet 02

Install the Support and Placard of the Blue System Accumulator FIN 292070

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-6064

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REPORTING SHEET

TITLE: HYDRAULIC POWER - BRACKETS AND SUPPORTS- HYDRAULIC

COMPARTMENT - INSTALL PLACARD FOR HYDRAULIC

ACCUMULATOR

MODIFICATION No.: 13540S22823

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 12/10 SERVICE BULLETIN No.: A300-29-6064

REVISION No.: 00 - Aug 12/10 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 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 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 12/10 SERVICE BULLETIN No.: A300-29-6064

REVISION No.: 00 - Aug 12/10 Page: 1

5

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