@A330

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: 32

TITLE: LANDING GEAR - MAIN GEAR - REPEAT INSPECTION OF THE

INTERNAL SURFACE OF THE BOGIE BEAM

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

**CONF ALL

A. EFFECTIVITY

NOTE: This inspection is valid for aircraft Pre Modification No. 54500H15561 (Service

Bulletin A330-32-3212) and Pre Modification No. 58896H16335 (Service

Bulletin A330-32-3237).

(1) Models

330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321

330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0069-0073 0077

0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116

0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211

0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256

0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288

0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320

0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353

0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386

0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458

0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487

0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522

0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558

0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588

0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618

0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650

0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688

0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718

0720-0722 0724-0726 0728-0730 0732-0734 0737 0739 0741 0743 0745-0746 0749

0752 0755 0760

(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

AAR 0640 0676 0708

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597 0733 0745 0749

AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657

ALK 0303 0306 0311 0313 0404 0456 0627

AZA 0272 0339

BEL 0030 0037 0045 0082 0095 0229 0249

BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 0739

BMA 0398 0401

BTV 0205 0330

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752

CES 0713 0720 0728 0732

CPA 0012 0017 0071 0102 0113 0118 0121 0155 0244 0386 0389 0393

0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679

CRL 0285 0320

CSC 0462

CSN 0649 0652 0656 0664

DAH 0644 0647 0650 0653 0667

DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674 0690 0718 0722

DGA 0240

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701

EDW 0291

EIN 0269 0397

ETD 0658 0688 0717 0724 0729 0730 0737

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755

FWI 0253

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 2

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

OPERATOR MSN

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HDA 0083 0099 0106 0109 0234 0405 0479 0512 0581 0654 0662 0692

0716 0741

HFY 0096 0211

HVN 0262 0275 0294 0299 0366

I2L 0364

IAC 0353 0362

ISS 0665

IWD 0670

IYE 0625 0632

JAV 0255

JST 0506 0508 0513 0522

KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0425 0428 0484 0490 0550

KKK 0343 0358

KLM 0682 0686 0703

MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

OHY 0072 0087 0098 0143

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712

QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659

0680 0684 0711 0721 0734 0743 0746 0760

RSY 0171

SAS 0496 0497 0515 0568

SWR 0324

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700

TAP 0181 0195 0223 0305 0308 0312 0317

TCX 0254 0266 0301

THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346

THY 0463 0504 0697 0704

TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382

0384 0392 0396 0409 0437 0451 0452 0455 0491 0494 0509 0518

0525 0536

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388

VKG 0309 0349 0356 0357

VLK 0055 0070 0086

VOZ 0365 0372

XAX 0054

XLF 0501 0635

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 3

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064

0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083

0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109

0110 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127

0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171

0172 0177 0181 0183 0184 0188 0189 0191 0195 0198 0200

0203 0205 0206 0209 0211 0219 0222 0223 0224 0226 0229

0230 0231 0232 0234 0238 0240 0241 0244 0247 0248 0249

0250 0251 0253 0254 0255 0256 0258 0259 0261 0262 0265

0266 0267 0269 0271 0272 0275 0276 0277 0279 0281 0283

0284 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296

0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313

0314 0315 0316 0317 0320 0322 0323 0324 0326 0328 0330

0333 0334 0337 0338 0339 0340 0342 0343 0344 0345 0346

0348 0349 0350 0351 0353 0356 0357 0358 0361 0362 0364

0365 0366 0368 0369 0370 0372 0375 0380 0382 0384 0386

0388 0389 0392 0393 0396 0397 0398 0400 0401 0403 0404

0405 0407 0408 0409 0412 0418 0419 0420 0421 0422 0423

0425 0427 0428 0432 0437 0439 0441 0443 0444 0448 0451

0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469

0472 0473 0476 0477 0479 0480 0481 0484 0486 0487 0489

0490 0491 0493 0494 0496 0497 0498 0500 0501 0502 0503

0504 0505 0506 0507 0508 0509 0510 0511 0512 0513 0515

0516 0518 0519 0521 0522 0524 0525 0526 0527 0529 0530

0532 0533 0535 0536 0539 0542 0548 0549 0550 0551 0552

0553 0555 0558 0564 0565 0567 0568 0570 0571 0573 0574

0576 0578 0579 0581 0584 0587 0588 0591 0593 0595 0597

0600 0602 0603 0605 0607 0609 0610 0612 0614 0616 0618

0620 0621 0623 0625 0627 0629 0631 0632 0633 0634 0635

0636 0637 0638 0640 0641 0642 0644 0645 0647 0648 0649

0650 0652 0653 0654 0655 0656 0657 0658 0659 0661 0662

0663 0664 0665 0666 0667 0669 0670 0671 0673 0674 0675

0676 0678 0679 0680 0682 0683 0684 0686 0687 0688 0690

0691 0692 0693 0695 0696 0697 0699 0700 0701 0703 0704

0705 0707 0708 0709 0711 0712 0713 0714 0716 0717 0718

0720 0721 0722 0724 0725 0726 0728 0729 0730 0732 0733

0734 0737 0739 0741 0743 0745 0746 0749 0752 0755 0760

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

None

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 4

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

An operator of an A330 in-service aircraft reported that the bogie beam on the right hand

MLG ruptured while taxiing during a slow turning manoeuvre.

Investigations have revealed that the rupture was due to compromized paint protection

leading to excessive corrosion on the internal surface of the bogie beam. Further

investigations indicate that a corrosion pit reached a depth sufficient to promote stress

corrosion cracking and a subsequent fast static rupture. No evidence of fatigue was

apparent.

Initial inspections of 15 aircraft on the bogie beams belonging to 5 operators have found

8 further bogie beams with compromized paint surfaces and corrosion in this area. A

further 2 bogie beams were suffering from paint damage. So far no bogie beams have

been scrapped but some repairs outside the published limits have been necessary.

(2) Objective/Action

This Service Bulletin is published to advise operators of A330 aircraft of the issue of

MESSIER DOWTY Service Bulletin No. A33/34-32-272.

This Service Bulletin details instructions to perform a repeat inspection on the internal

surface of the bogie beam assemblies to ensure that there is no corrosion. The

inspection requires the removal of the bogie beam assembly and a detailed inspection of

the internal surfaces using a boroscope.

(3) Advantages

This Service Bulletin will give an early detection of corrosion and prevent possible

rupture of the bogie beam due to corrosion.

The inspection requirement is cancelled by the accomplishment of Service Bulletin No.

A330-32-3237. MESSIER-DOWTY Service Bulletin No. A33/34-32-284.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 323225-832-895-001: INSPECTION

(1) Remove the Bogie Beam Assembly from both the LH and RH Wings

(2) Do the inspection on the Bogie Beam Assembly LH and RH Wings

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 5

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(3) Install the Bogie Beam Assembly to the LH and RH Wings

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified 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 mandated accomplishment timescale.

MLG Bogie Beam Condition Inspection Threshold Inspection Interval

MLG bogie beams which have not

embodied AIRBUS modification

54500H15561 in production nor

AIRBUS Service Bulletin No.

A330-32-3212 in service, and which

had accumulated on 03 June 2008

(the effective date of EASA AD

2008-0093) less than or equal to 4.5

years since their first flight on an

aeroplane or since their first flight

after their last overhaul, as

applicable.

At the first convenient

maintenance opportunity

which occurs after the 4.5

years threshold, but no later

than 6 years since the LH or

RH MLG bogie beam first

flight on an aeroplane or since

first flight after its last

overhaul, as applicable

MLG bogie beams which have not

embodied AIRBUS modification

54500H15561 in production nor

AIRBUS Service Bulletin

A330-32-3212 in service, and which

had accumulated on 03 June 2008

more than 4.5 years since their first

flight on an aeroplane or since their

first flight after their last overhaul, as

applicable.

At the next convenient

maintenance opportunity, or

within 18 months after 04

January 2008 (the effective

date of EASA AD

2007-0314R1), whichever

occurs first and without

exceeding the next bogie

beam overhaul.

No later than 6 years, but no

earlier than 4 years since its

first flight after the MLG bogie

beam overhaul which occurs

after the last inspection

F. APPROVAL

The technical content of this document is approved under the authority of 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.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 6

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

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 323225-832-895-001: INSPECTION

Get Access 1.00

On Aircraft

Remove the Bogie Beam Assembly from both the LH

and RH Wings

10.00

Install the Bogie Beam Assembly to the LH and RH

Wings

10.00

Tests 2.50

Close-Up 1.00

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 12.00

Additional manhours related to Vendor SB; refer to:

Do the inspection on the Bogie Beam Assembly LH

and RH Wings

MESSIER DOWTY Service Bulletin

No. A33/34-32-272

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

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

32-11-14

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

Vendor Service Bulletin (VSB) MESSIER DOWTY Service Bulletin

No. A33/34-32-272

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 7

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 8

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Inspection and repair of removed equipment should be negotiated directly with

MESSIER DOWTY as per instructions given in Service Bulletin No. A33/34-32-272.

(2) Price and Availability

No AIRBUS kit will be provided.

Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272 for the equipment sales

terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272 for the industry support

terms.

C. LIST OF COMPONENTS

Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this Service Bulletin it will be necessary to use the consumable materials

included in AMM Task 32-11-14-410-801 and MESSIER DOWTY Service Bulletin No.

A33/34-32-272.

(2) Components

To accomplish this Service Bulletin it will be necessary to use the expendable parts

included in AMM Task 32-11-14-410-801 and MESSIER DOWTY Service Bulletin No.

A33/34-32-272.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 9

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(2) Tools

To accomplish this Service Bulletin it will be necessary to use the tools listed in AMM

Task 32-11-14-010-801 and AMM Task 32-11-14-410-801.

Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272.

(3) Special Tools

Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 10

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 323225-832-895-001 - INSPECTION

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.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

Zone

731 741

Manpower

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 12.00

Additional manhours related to Vendor SB; refer to:

MESSIER DOWTY Service Bulletin No. A33/34-32-272

A. GENERAL

(1) Subtask 323225-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803

Task 20-21-12-911-801

Task 20-28-00-912-802

(a) Put blanking caps on all the related disconnected electrical-connectors.

(b) Put blanking caps on all the related disconnected hydraulic-connectors.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 11

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(c) Tightening Torques for Pipe Unions (Refer to AMM Task 20-21-12-911-801).

(d) Electrical Bonding of Components with Conductive Screws and Bolts (Refer to

AMM Task 20-28-00-912-802).

(e) For the removal and installation of wire locking (Refer to AMM Task

20-11-11-911-803).

(2) Subtask 323225-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 323225-941-401-001 - Job Set-Up

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-010-801

(a) Do the "Job Set-up" procedures as specified in AMM Task "Removal of the MLG

Bogie Beam Assembly for Access, Complete with Wheels and Brakes" (Refer to

AMM Task 32-11-14-010-801).

C. PROCEDURE

(1) Subtask 323225-020-401-001 - Remove the Bogie Beam Assembly from both the

LH and RH Wings

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills AIRFRAME

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 12

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-010-801

(a) Remove the LH and RH Bogie Beam Assembly for Access, Complete with Wheels

and Brakes (Refer to AMM Task 32-11-14-010-801).

(2) Subtask 323225-832-405-001 - Do the inspection on the Bogie Beam Assembly LH

and RH Wings

Work Zones and Access Panels

Zone Access/Work location

731

741

References

Vendor Service Bulletin (VSB) MESSIER DOWTY A33/34-32-272

Fig. A-UFAAA

Inspection Flowchart

Sheet 01

NOTE: The latest revision of MESSIER DOWTY Service Bulletin No.

A33/34-32-272 must be used.

Refer to Fig. A-UFAAA Sheet 01.

(a) Do the inspection on the bogie beam assembly LH and RH (Refer to MESSIER

DOWTY Service Bulletin No. A33/34-32-272).

(b) Report all findings, including nil findings, to AIRBUS SEEL3 department within 90

days.

Refer to Appendix. 1 - Inspection Report of Bogie Beam Assembly , Inspection

Report.

(3) Subtask 323225-420-401-001 - Install the Bogie Beam Assembly to the LH and RH

Wings

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-410-801

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 13

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(a) Install the LH and RH Bogie Beam assembly After Access, Complete with Wheels

and Brakes (Refer to AMM Task 32-11-14-410-801).

D. TEST

(1) Subtask 323225-700-401-001 - Test

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-410-801

(a) Do the test procedures as specified in AMM Task "Installation of the MLG Bogie

Beam Assembly after Access, Complete with Wheels and Brakes" (Refer to AMM

Task 32-11-14-410-801).

E. CLOSE-UP

(1) Subtask 323225-832-408-001 - Close-Up

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-410-801

(a) Make sure that the work area is clean and clear of tools and other items of

equipment.

(b) Do the "Close up" procedures as specified in AMM Task "Installation of the MLG

Bogie Beam Assembly after Access, Complete with Wheels and Brakes" (Refer to

AMM Task 32-11-14-410-801).

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 14

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

YES

QUESTION

ACTION

FINDING

DO A DETAILED INSPECTION

OR RH BOGIE BEAM INTERNAL

DIAMETER FOR CORROSION OR

IN PARAGRAPH 1E(2) OF THE LH

BEAM INTERNAL SURFACE

PROTECTION INTACT?

IS THE BOGIE

CONFIRM THE EXTENT OF THE

CADMIUM/BASE METAL DAMAGE)

BEFORE NEXT FLIGHT

DAMAGE (LEVEL OF PAINT/

IS THE

REPAIRABLE?

BOGIE BEAM

PROCEED WITH REPAIR

BEFORE NEXT FLIGHT, AND

RECORD THE DAMAGE.

RECORD THE REPAIRS MADE

FINDINGS AND RETURN

INTO SERVICE

RECORD THE NIL

SCRAP THE BOGIE BEAM

RECORD THE FINDINGS.

WITHIN 90 DAYS, INFORM AIRBUS

AND MESSIER−DOWTY LTD. OF 

INSPECTION RESULTS

BEEN EMBODIED ON THE

AIRCRAFT OR A33/34−32−284

HAS SB32−3237

BEEN APPLIED ON THE

NO FURTHER ACTION

BOGIE BEAM) ?

YES

YES

NO

NO

NO

BETWEEN 4 AND 6 YEARS

REPEAT THE INSPECTION

AFTER OVERHAUL,

WITHIN THE TIMESCALE DEFINED

PAINT DAMAGE

NOTE: THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION

GIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO

SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMES

GIVEN IN THIS SERVICE BULLETIN. G_SB_323225_7_FAAA_01_03

Figure A-UFAAA - Sheet 01

Inspection Flowchart

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 15

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 16

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Appendix. 1 - Inspection Report of Bogie Beam Assembly

**CONF ALL

(1) Appendix. 1 - Inspection Report of Bogie Beam Assembly

INSPECTION REPORT OF BOGIE BEAM ASSEMBLY LH WING

SERVICE BULLETIN NO.

A330-32-3225

DATE OF

INSPECTION:

OPERATOR:

AIRCRAFT MSN: SERIAL NUMBER

FLIGHT HOURS FLIGHT CYCLES

BOGIE BEAM PAINT DAMAGE

FOUND

YES NO

OVER WHAT

AREA

LOCATION (AXIALLY AND

CIRCUMFERENTIALLY)

USE THE ILLUSTRATIONS SUPPLIED IN

MESSIER DOWTY SERVICE BULLETIN NO.

A33/34-32-272 TO INDICATE THE AREA AND

THE LOCATION AND RETURN TO AIRBUS

WITH THIS REPORT.

BOGIE BEAM CORROSION

DAMAGE FOUND

YES NO

OVER WHAT

AREA

LOCATION (AXIALLY AND

CIRCUMFERENTIALLY)

USE THE ILLUSTRATIONS SUPPLIED IN

MESSIER DOWTY SERVICE BULLETIN NO.

A33/34-32-272 TO INDICATE THE AREA AND

THE LOCATION AND RETURN TO AIRBUS

WITH THIS REPORT.

DEPTH OF THE CORROSION:

SURFACE ONLY, REFER TO

MESSIER DOWTY SERVICE

BULLETIN NO. A33/34-32-272.

WITHIN REPAIRABLE LIMITS, REFER TO MESSIER DOWTY

SERVICE BULLETIN NO. A33/34-32-272.

OUTSIDE THE ABOVE REPAIR LIMITS, CONTACT AIRBUS

CUSTOMER SERVICES FOR FURTHER ADVICE / NTO

APPLICATION.

AREA AND MAXIMUM BLEND NECESSARY TO

CLEAR THE CORROSION

NOTE: Include photographs of the area before repair and return to AIRBUS. Report all

findings including nil findings to AIRBUS Customer Services.

INSPECTION REPORT OF BOGIE BEAM ASSEMBLY RH WING

SERVICE BULLETIN NO.

A330-32-3225

DATE OF

INSPECTION:

OPERATOR:

AIRCRAFT MSN: SERIAL NUMBER

FLIGHT HOURS FLIGHT CYCLES

BOGIE BEAM PAINT DAMAGE

FOUND

YES NO

OVER WHAT

AREA

LOCATION (AXIALLY AND

CIRCUMFERENTIALLY)

USE THE ILLUSTRATIONS SUPPLIED IN

MESSIER DOWTY SERVICE BULLETIN NO.

A33/34-32-272 TO INDICATE THE AREA AND

THE LOCATION AND RETURN TO AIRBUS

WITH THIS REPORT.

BOGIE BEAM CORROSION

DAMAGE FOUND

YES NO

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Appendix. 1 - Inspection Report of Bogie Beam Assembly

OVER WHAT

AREA

LOCATION (AXIALLY AND

CIRCUMFERENTIALLY)

USE THE ILLUSTRATIONS SUPPLIED IN

MESSIER DOWTY SERVICE BULLETIN NO.

A33/34-32-272 TO INDICATE THE AREA AND

THE LOCATION AND RETURN TO AIRBUS

WITH THIS REPORT.

DEPTH OF THE CORROSION:

SURFACE ONLY, REFER TO

MESSIER DOWTY SERVICE

BULLETIN NO. A33/34-32-272.

WITHIN REPAIRABLE LIMITS, REFER TO MESSIER DOWTY

SERVICE BULLETIN NO. A33/34-32-272.

OUTSIDE THE ABOVE REPAIR LIMITS, CONTACT AIRBUS

CUSTOMER SERVICES FOR FURTHER ADVICE / NTO

APPLICATION.

AREA AND MAXIMUM BLEND NECESSARY TO

CLEAR THE CORROSION

NOTE: Include photographs of the area before repair and return to AIRBUS. Report all

findings including nil findings to AIRBUS Customer Services.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225

REVISION No.: 02 - Oct 26/12 Page: 2

7

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