@A310

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 accumulator with only one weld (post 1984) will be allowed.

This Service Bulletin requires installing :

- A support bracket and placard adjacent to the green hydraulic system accumulators

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 292100A01R00 1 197.00 Support

EFFECTIVITY

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

19U 52X 58X 82Z 83V 99Y ACQ AFG AIB AIC BAF BBC BLE

CFC CSA DAH DEC DGA F2I FDX G8E GAF HFY I2L IRA IRM

IYE JAB JAV K1P KAC KTC KYV KZU MGL MWA PIA QAF R1T

RJA ROT RZO SBI SGX SUD THY TSC UZB WHT WTJ

CONCURRENT REQUIREMENTS

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

Service Bulletin :

A310-29-2099

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 292100-831-801-001: Modification

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

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SERVICE BULLETIN

SUMMARY

APPENDICES

None

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SERVICE BULLETIN

SUMMARY

**CONF ALL

FR47

FR54

SUPPORT AND PLACARD

Z147

A

B

C

SUPPORT AND

PLACARD TO

FR52

FR52

FWD

B

C

291070

A

B_SB_292100_5_SAAA_01_02

TO BE INSTALLED

BE INSTALLED

Figure A-FSAAA - Sheet 01

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@A310

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

310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324

310-325

(2) Effectivity by MSN

0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260

0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318

0320 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357

0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0386 0389-0390 0392

0394 0397 0399-0400 0406-0407 0410 0413 0416 0418-0419 0421-0422 0425

0427-0429 0431 0434 0436-0437 0439 0441 0444-0449 0452 0454 0456-0458 0467

0472-0473 0475-0476 0478 0480-0492 0494-0500 0502-0503 0519-0520 0522-0524

0526-0527 0531 0534 0537-0539 0541-0542 0544-0545 0547 0549-0552 0562

0564-0565 0567-0568 0571 0573-0574 0576 0585-0588 0590-0595 0597 0599-0600

0620 0622 0624 0636 0638 0640 0642 0644 0646-0654 0656 0658 0660-0661 0663

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SERVICE BULLETIN

0665 0667 0669 0671-0672 0674 0676 0678 0680 0682 0684 0686-0687 0689 0691

0693 0697 0700 0702 0704 0706

(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

19U 0399

52X 0410

58X 0431

82Z 0550 0551

83V 0427

99Y 0489

ACQ 0538 0544

AFG 0496 0497

AIB 0686

AIC 0392 0406 0407 0413 0428 0429 0654 0665 0669 0680

BAF 0367 0372

BBC 0594 0642 0700

BLE 0650 0674

CFC 0425 0441 0444 0446 0482

CSA 0672

DAH 0291 0293

DEC 0684 0693 0697

DGA 0418 0421 0422

F2I 0309 0487

FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251

0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303

0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346

0353 0355 0356 0359 0360 0362 0364 0369 0378 0394 0397 0400

0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539

0542 0549 0552 0593 0638

G8E 0475

GAF 0434 0484 0498 0499 0503 0522 0523

HFY 0495 0565

I2L 0640

IRA 0338 0370 0375 0379 0389 0390 0436 0671

IRM 0488 0537 0564 0586 0595

IYE 0568 0702 0704

JAB 0320 0419

JAV 0357 0481

K1P 0648

KAC 0647 0649 0663

KTC 0524 0567 0620

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@A310

SERVICE BULLETIN

OPERATOR MSN

KYV 0386

KZU 0592 0622 0646

MGL 0526

MWA 0652

PIA 0473 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689

0691

QAF 0667

R1T 0591

RJA 0416 0445 0490 0491 0531

ROT 0636 0644

RZO 0571 0624 0651 0661

SBI 0486 0520

SGX 0519 0562

SUD 0437

THY 0476 0478 0480 0502

TSC 0447 0472 0483 0485 0527 0541 0545 0547 0588 0597 0599 0600

0658

UZB 0574 0576 0706

WHT 0448 0573

WTJ 0494

(4) Configuration by MSN

MSN CONFIGURATION

0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248

0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288

0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331

0333 0335 0338 0339 0342 0343 0345 0346 0353 0355 0356

0357 0359 0360 0362 0364 0367 0369 0370 0372 0375 0378

0379 0386 0389 0390 0392 0394 0397 0399 0400 0406 0407

0410 0413 0416 0418 0419 0421 0422 0425 0427 0428 0429

0431 0434 0436 0437 0439 0441 0444 0445 0446 0447 0448

0449 0452 0454 0456 0457 0458 0467 0472 0473 0475 0476

0478 0480 0481 0482 0483 0484 0485 0486 0487 0488 0489

0490 0491 0492 0494 0495 0496 0497 0498 0499 0500 0502

0503 0519 0520 0522 0523 0524 0526 0527 0531 0534 0537

0538 0539 0541 0542 0544 0545 0547 0549 0550 0551 0552

0562 0564 0565 0567 0568 0571 0573 0574 0576 0585 0586

0587 0588 0590 0591 0592 0593 0594 0595 0597 0599 0600

0620 0622 0624 0636 0638 0640 0642 0644 0646 0647 0648

0649 0650 0651 0652 0653 0654 0656 0658 0660 0661 0663

0665 0667 0669 0671 0672 0674 0676 0678 0680 0682 0684

0686 0687 0689 0691 0693 0697 0700 0702 0704 0706

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.

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SERVICE BULLETIN

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 292100A01R00 1

Consumable CMLA01 1

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the

following Service Bulletin :

A310-29-2099

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 accumulator 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 green hydraulic system accumulators

(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 292100-831-801-001: Modification

(1) Install the Support and Placard of the Green System Accumulator FIN 291070

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

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SERVICE BULLETIN

(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.

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 292100-831-801-001: Modification

Get Access 1.00

On Aircraft

Install the Support and Placard of the Green System

Accumulator FIN 291070

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) A310-29-2099

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SERVICE BULLETIN

Standards Manual (SM)

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

51-40-30 51-40-40

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 29-11-56

Illustrated Parts Catalog (IPC) 53-15-03

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 292100A01R00 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 292100A01R

Cost 197.00 USD

Availability 90 calendar days from receipt of order

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 292100A01R00

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

NOTES

1 A2913203300000 1 SUPPORT

2 NAS1801-08-7 2 BOLT

3 NAS1149FN832P 2 WASHER

4 MS21042L08 2 NUT

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.

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SERVICE BULLETIN

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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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 292100-831-801-001 - 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 292100-839-001-001 - 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 292100-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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SERVICE BULLETIN

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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SERVICE BULLETIN

B. PREPARATION

(1) Subtask 292100-941-001-001 - 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 292100-420-001-001 - Install the Support and Placard of the Green System

Accumulator FIN 291070

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 292100A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A2913203300000 1 SUPPORT

2 NAS1801-08-7 2 BOLT

3 NAS1149FN832P 2 WASHER

4 MS21042L08 2 NUT

References

Fig. A-FBAAA

Install the Support and Placard of the

Green System Accumulator FIN 291070

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 4.3 mm (0.169 in.) and 4.4

mm (0.173 in.) to match the holes of the support Item 1 as shown in Fig. A-FBAAA

Sheet 02.

(c) Install :

1 Support A2913203300000 Item 1

2 Bolt NAS1801-08-7 Item 2

2 Washer NAS1149FN832P Item 3

2 Nut MS21042L08 Item 4

D. TEST

None

E. CLOSE-UP

(1) Subtask 292100-942-001-001 - 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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SERVICE BULLETIN

**CONF ALL

FR47

FR54

A

Z147

A

B

C

D

FR52

FR52

FWD

B

C

1

291070

B_SB_292100_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Install the Support and Placard of the Green System Accumulator FIN 291070

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100

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SERVICE BULLETIN

**CONF ALL

5 mm

(0.197 in)

FR52

1

FWD

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

4.30 mm

(0.169 in)

4.40 mm

(0.173 in)

NAS1801−08−7 BOLT

NAS1149FN832P WASHER

MS21042L08 NUT

2

3

4

B_SB_292100_5_BAAA_02_01

N

HEAD ON VISIBLE FACE

NOTE:

01 DO THE ELECTRICAL BONDING

ON BOTH SIDES (AS 2 POINTS).

01

N

D

Figure A-FBAAA - Sheet 02

Install the Support and Placard of the Green System Accumulator FIN 291070

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100

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SERVICE BULLETIN

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.: A310-29-2100

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

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

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.: A310-29-2100

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

5

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