@A340

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

ATA SYSTEM: 32

TITLE: LANDING GEAR - MAIN GEAR - IMPROVED 2-PART PAINT SCHEME

FOR BASIC, GROWTH AND ENHANCED MLG BOGIE BEAM

MODIFICATION No.: 58896H16355

This page transmits Revision No.01 of Service Bulletin No.A340-32-4279

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to:

- update configuration effectivity for aircraft that have embodied Service Bulletin No. A340-32-4201

(Install Common Bogie and Dressings for Weight Saving on Growth for Commonality with Basic

Aircraft)

- update configuration effectivity for aircraft that have embodied Service Bulletin No. A340-32-4256

(Install Enhanced Main Landing Gear).

CHANGES

FRONT MATTER

LANDING GEAR - MAIN GEAR -

IMPROVED 2-PART PAINT SCHEME

FOR BASIC, GROWTH AND ENHANCED

MLG BOGIE BEAM

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 1

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

APPENDICES APPENDICES UPDATED R

Fig. A-USAAA

Fig. A-USAAA Sheet 01 SHEET UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 003 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 004 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 005 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

REASON

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

INTERCHANGEABILITY/MIXABILITY UPDATED R

MATERIAL INFORMATION

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

Consumable CMLB00 CONSUMABLE MATERIAL SET UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

R

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 2

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Reidentified part set REIDB02 PART MATERIAL SET UPDATED

NOTE UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

R

Reidentified part set REIDB05 PART MATERIAL SET UPDATED

NOTE UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

R

ACCOMPLISHMENT INSTRUCTIONS

TASK 324279- 831-895-001-

MODIFICATION

TASK SOLUTION UPDATED

CAUTION UPDATED

R

Task associated data - 001 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 002 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 003 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 004 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 005 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Subtask 324279-941-401-001 SUBTASK SOLUTION UPDATED R

Subtask 324279-941-401-001 SUBTASK SOLUTION UPDATED R

Subtask 324279-941-401-001 SUBTASK SOLUTION UPDATED R

Subtask 324279-941-401-006 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

REFERENCES UPDATED

R

Subtask 324279-941-401-002 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

REFERENCES UPDATED

R

Subtask 324279-020-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-831-401-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 324279-420-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-001 SUBTASK SOLUTION UPDATED R

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 324279-020-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-831-401-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 324279-420-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 324279-020-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-831-401-003 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 324279-420-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-003 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 324279-930-401-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

QUANTITY UPDATED

MATERIAL LIST UPDATED

R

Subtask 324279-020-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-831-401-004 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 324279-420-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-004 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 324279-930-401-002 SUBTASK SOLUTION UPDATED

NOTE UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

QUANTITY UPDATED

MATERIAL LIST UPDATED

R

Subtask 324279-020-401-001 SUBTASK SOLUTION ADDED N

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 4

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 324279-831-401-005 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 324279-420-401-001 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-002 SUBTASK SOLUTION ADDED N

Subtask 324279-930-402-005 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 324279-740-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-740-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-740-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-740-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-740-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 324279-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Fig. A-UBAAA FIGURE SOLUTION ADDED N

Fig. A-UBAAA Sheet 01 SHEET ADDED N

APPENDIX 01 : ELAPSED TIME ASSUMPTION

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-UAAAA FIGURE SOLUTION ADDED N

Fig. A-UAAAA Sheet 01 SHEET ADDED N

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 5

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

FILLING 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

No previous revision

REVISION SEQUENCE

ORIGINAL: Jan 18/11

REVISION No. : 01 - Oct 14/11

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 6

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@A340

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: 32

TITLE: LANDING GEAR - MAIN GEAR - IMPROVED 2-PART PAINT SCHEME

FOR BASIC, GROWTH AND ENHANCED MLG BOGIE BEAM

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 58896H16355

MINOR None

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

Fracture of a bogie beam has occurred in-service due to corrosion in the bore. A subsequent

investigation showed thin paint coats and paint degradation.

This Service Bulletin is issued to:

- inform operators of A340 aircraft fitted with basic or strengthened Main Landing Gear (MLG) of the

issue of MESSIER-DOWTY Service Bulletin No. A33/34-32-284

- inform operators of A340 aircraft fitted with enhanced Main Landing Gear (MLG) of the issue of

MESSIER-DOWTY Service Bulletin No. A33/34-32-283.

These vendor bulletins introduce new bogie and dressings that have:

- been inspected prior to the commencement of work

- a new two coat paint procedure applied

- the bogie beam protective treatments checked for correct thickness after application of each

different layer

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 1

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SERVICE BULLETIN

SUMMARY

- a new protective Ardrox AV100D Wax Oil (instead of de-watering oil Ardrox 3140) applied to the

bore of the bogie beam after paint

- a new part number bogie beam axle and spacer sub-assembly (spacer is only fitted on enhanced

bogie beam), bogie beam sub-assembly and bogie beam M/C.

The new part numbers will show that the two coat paint procedure and Ardrox AV100D Wax Oil are

applied and the protective treatments checked for thickness.

Accomplishment of this Service Bulletin will ensure that the MLG bogie beam and dressings have been

inspected and had overall thickness measurements taken and recorded and has improved protection

from corrosion.

NOTE: In-service aircraft which can prove through serial number to have been protective

treated to post modification requirements can be re-part numbered in-service to record

embodiment of MESSIER-DOWTY Service Bulletin No. A33/34-32-283 or MESSIERDOWTY Service Bulletin No. A33/34-32-284 with no further action.

NOTE: If the Serial Number confirms the post modification process then the pre and post

modification inspections are NOT required.

NOTE: Pre mod MLG bogie beam and dressings can be replaced with post mod WITHOUT the

need for modification inspections.

Accomplishment of this Service Bulletin cancels the inspection requirements of Service Bulletin

A340-32-4268 for basic, hybrid and growth standards of bogie beam.

ALS Part 1

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB YES

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

AIRCRAFT JACKING YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

No Material

**CONF 002

No Material

**CONF 003

No Material

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 2

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@A340

SERVICE BULLETIN

SUMMARY

**CONF 004

No Material

**CONF 005

No Material

EFFECTIVITY

**CONF ALL

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

47W 56W AAW AFR ALK ARG B3R CAL CCA CES CPA DGA DLH

FIN GAF GFA HFY IBE KAC KNE LAN M3R MAU MSR NMB OAL

PAL QAF RJA S3R SAA SAS SLM SVW SWR TAP THT THY UAE

VCV VIR XAX

CONCURRENT REQUIREMENTS

None

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 YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 324279-831-895-001: MODIFICATION

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 3

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@A340

SERVICE BULLETIN

SUMMARY

Task 324279-831-895-001: MODIFICATION

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 002

Task 324279-831-895-001: MODIFICATION

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 003

Task 324279-831-895-001: MODIFICATION

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 004

Task 324279-831-895-001: MODIFICATION

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

RE-IDENTIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-284

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 4

7

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@A340

SERVICE BULLETIN

SUMMARY

Task 324279-831-895-001: MODIFICATION

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 005

Task 324279-831-895-001: MODIFICATION

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

RE-IDENTIFY THE BOGIE BEAM AXLE AND SPACER

SUB-ASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-283

MODIFY THE BOGIE BEAM AXLE AND SPACER SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-283

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-283

APPENDICES

**CONF ALL

APPENDIX 01 : ELAPSED TIME ASSUMPTION

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 5

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@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

F_SB_324279_7_SAAA_01_01

AREA OF MODIFICATION

(BOGIE BEAM)

LH MLG SHOWN

RH MLG SIMILAR

Figure A-USAAA - Sheet 01

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 6

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@A340

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 - IMPROVED 2-PART PAINT SCHEME

FOR BASIC, GROWTH AND ENHANCED MLG BOGIE BEAM

MODIFICATION No.: 58896H16355

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

(1) Models

340-211 340-212 340-213 340-311 340-312 340-313

(2) Effectivity by MSN

0002-0006 0008-0009 0011 0013-0015 0018-0029 0031-0035 0038 0041 0043-0044

0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085

0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128-0129 0131

0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 0233

0235-0237 0239 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270

0273-0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325

0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374

0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424

0429-0430 0433-0435 0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528

0538 0541 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646

0651 0668 0793 0800 0835 0844 0921 0938 0955

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 1

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@A340

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

47W 0009

56W 0002 0003 0013 0015

AAW 0151

AFR 0029 0078 0084 0186 0207 0210 0237 0245 0246 0260 0307 0310

0319 0373 0377 0399

ALK 0032 0033 0034 0367 0374 0381

ARG 0048 0063 0074 0080 0085 0093 0094 0123 0126

B3R 0046

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

CES 0129 0131 0141 0161 0182

CPA 0128 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228

DGA 0075 0081

DLH 0020 0024 0027 0028 0035 0052 0053 0056 0135 0158 0213 0233

0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390

0434 0447

FIN 0058 0168 0174 0835 0844 0921 0938

GAF 0274 0355

GFA 0212 0215 0282 0554

HFY 0117 0133 0450

IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0302 0318

0329 0332 0387 0414 0459 0474 0483

KAC 0089 0090 0101 0104

KNE 0004

LAN 0167 0359 0363 0429 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MSR 0156 0159 0178

NMB 0047 0051

OAL 0235 0239 0280 0292

PAL 0173 0176 0187 0196

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0008 0011 0018 0019 0021 0197 0378 0544 0582 0590 0643

0646 0651

SAS 0413 0424 0430 0435 0467 0470

SLM 0049

SVW 0955

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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@A340

SERVICE BULLETIN

OPERATOR MSN

SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561

0562 0585 0598

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446 0668

THY 0023 0025 0057 0115 0180 0216 0257 0270 0331

UAE 0139 0149 0163 0166 0185 0190 0202 0236

VCV 0031

VIR 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0008 0011 0013 0014 0018 0019 0020 0021 0022 0023

0024 0025 0026 0027 0028 0029 0031 0032 0033 0034 0035

0038 0041 0043 0044 0046 0047 0048 0049 0051 0052 0053

0056 0057 0058 0061 0063 0074 0075 0076 0078 0079 0080

0081 0084 0085 0088 0089 0090 0091 0093 0094 0101 0104

0114 0115 0125 0133 0134 0145 0146 0151 0156 0159 0178

002

0003 0004 0005 0006 0009 0015 001

0117 0123 0126 0128 0129 0131 0135 0136 0137 0139 0141

0142 0147 0149 0150 0152 0154 0157 0158 0160 0161 0163

0164 0166 0167 0168 0169 0170 0173 0174 0175 0176 0179

0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197

0199 0201 0202 0207 0208 0210 0212 0213 0214 0215 0216

0218

003 004 005

0204 003 004

0217 0220 0221 0225 0227 0228 0233 0235 0236 0237 0239

0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270

0273 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310

0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352

0354 0355 0359 0363 0367 0373 0374 0377 0378 0379 0381

0385 0387 0390 0395 0399 0402 0406 0411 0413 0414 0415

0424 0429 0430 0433 0434 0435 0438 0442 0446 0447 0450

0459 0467 0470 0474 0483 0528 0538 0541 0544 0545 0546

0554 0556 0559 0561 0562 0582 0585 0590 0598 0643 0646

0651 0668

004 005

0793 0800 0835 0844 0921 0938 0955 005

(5) Configuration definition

**CONF 001

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

are Pre Mod 41366H12716.

**CONF 002

Config. 002 is valid for all the aircraft given in the effectivity of this Service Bulletin that

are Post Mod 41366H12716.

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**CONF 003

Config. 003 is valid for all the aircraft given in the effectivity of this Service Bulletin that

are Post Mod 43029H13154.

NOTE: Aircraft that have embodied Service Bulletin No. A340-32-4201 are to be

considered as Config. 004.

NOTE: Aircraft that have embodied Service Bulletin No. A340-32-4256 are to be

considered as Config. 005.

**CONF 004

Config. 004 is valid for all the aircraft given in the effectivity of this Service Bulletin that

are Post Mod 43029H13154 and Post Mod 45921H13895 (or have embodied Service

Bulletin No. A340-32-4201).

NOTE: Aircraft that have embodied Service Bulletin No. A340-32-4256 are to be

considered as Config. 005.

**CONF 005

Config. 005 is valid for all the aircraft given in the effectivity of this Service Bulletin that

are Post Mod 54500H15561 (or have embodied Service Bulletin No. A340-32-4256).

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Reidentified part set REIDB01 1

Consumable CMLB00 As required

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Reidentified part set REIDB03 1

Consumable CMLB00 As required

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Reidentified part set REIDB04 1

Consumable CMLB00 As required

**CONF 004

MATERIAL QTY PER A/C SEE NOTES

Reidentified part set REIDB04 As required

Reidentified part set REIDB05 As required

Reidentified part set REIDB06 As required

Reidentified part set REIDB07 As required

Consumable CMLB00 As required

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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**CONF 005

MATERIAL QTY PER A/C SEE NOTES

Reidentified part set REIDB02 1

Consumable CMLB00 As required

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Fracture of a bogie beam has occurred in-service due to corrosion in the bore. A

subsequent investigation showed thin paint coats and paint degradation.

(2) Objective/Action

This Service Bulletin is issued to:

- inform operators of A340 aircraft fitted with basic or strengthened Main Landing

Gear (MLG) of the issue of MESSIER-DOWTY Service Bulletin No. A33/34-32-284

- inform operators of A340 aircraft fitted with enhanced Main Landing Gear (MLG) of

the issue of MESSIER-DOWTY Service Bulletin No. A33/34-32-283.

These vendor bulletins introduce new bogie and dressings that have:

- been inspected prior to the commencement of work

- a new two coat paint procedure applied

- the bogie beam protective treatments checked for correct thickness after application

of each different layer

- a new protective Ardrox AV100D Wax Oil (instead of de-watering oil Ardrox 3140)

applied to the bore of the bogie beam after paint

- a new part number bogie beam axle and spacer sub-assembly (spacer is only fitted

on enhanced bogie beam), bogie beam sub-assembly and bogie beam M/C.

The new part numbers will show that the two coat paint procedure and Ardrox

AV100D Wax Oil are applied and the protective treatments checked for thickness.

(3) Advantages

Accomplishment of this Service Bulletin will ensure that the MLG bogie beam and

dressings have been inspected and had overall thickness measurements taken and

recorded and has improved protection from corrosion.

NOTE: In-service aircraft which can prove through serial number to have

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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been protective treated to post modification requirements can be repart numbered in-service to record embodiment of MESSIER-DOWTY

Service Bulletin No. A33/34-32-283 or MESSIER-DOWTY Service

Bulletin No. A33/34-32-284 with no further action.

NOTE: If the Serial Number confirms the post modification process then the pre

and post modification inspections are NOT required.

NOTE: Pre mod MLG bogie beam and dressings can be replaced with post mod

WITHOUT the need for modification inspections.

Accomplishment of this Service Bulletin cancels the inspection requirements of Service

Bulletin A340-32-4268 for basic, hybrid and growth standards of bogie beam.

(4) Operational/Maintenance Consequences

ALS Part 1

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 324279-831-895-001: MODIFICATION

(1) REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR MODIFICATION

(2) MODIFY THE BOGIE BEAM AND AXLE SUB-ASSEMBLY, BOGIE BEAM SUBASSEMBLY AND BOGIE BEAM M/C

(3) INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER MODIFICATION

(4) MARKING - STRIKE NUMBERS

**CONF 002

Task 324279-831-895-001: MODIFICATION

(1) REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR MODIFICATION

(2) MODIFY THE BOGIE BEAM AND AXLE SUB-ASSEMBLY, BOGIE BEAM SUBASSEMBLY AND BOGIE BEAM M/C

(3) INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER MODIFICATION

(4) MARKING - STRIKE NUMBERS

**CONF 003

Task 324279-831-895-001: MODIFICATION

(1) REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR MODIFICATION

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(2) MODIFY THE BOGIE BEAM AND AXLE SUB-ASSEMBLY, BOGIE BEAM SUBASSEMBLY AND BOGIE BEAM M/C

(3) INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER MODIFICATION

(4) MARKING - STRIKE NUMBERS

**CONF 004

Task 324279-831-895-001: MODIFICATION

(1) RE-IDENTIFY THE BOGIE BEAM AND AXLE SUB-ASSEMBLY, BOGIE BEAM SUBASSEMBLY AND BOGIE BEAM M/C

(2) REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR MODIFICATION

(3) MODIFY THE BOGIE BEAM AND AXLE SUB-ASSEMBLY, BOGIE BEAM SUBASSEMBLY AND BOGIE BEAM M/C

(4) INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER MODIFICATION

(5) MARKING - STRIKE NUMBERS

**CONF 005

Task 324279-831-895-001: MODIFICATION

(1) RE-IDENTIFY THE BOGIE BEAM AXLE AND SPACER SUB-ASSEMBLY, BOGIE

BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

(2) REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR MODIFICATION

(3) MODIFY THE BOGIE BEAM AXLE AND SPACER SUB-ASSEMBLY, BOGIE BEAM

SUB-ASSEMBLY AND BOGIE BEAM M/C

(4) INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER MODIFICATION

(5) MARKING - STRIKE NUMBERS

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

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). The accomplishment timescale, which has not yet been defined, will be

given in the AD.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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F. APPROVAL

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

Organization 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.

**CONF 001

Task 324279-831-895-001: MODIFICATION

Get Access 1.00

On Aircraft

REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

6.00

INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER

MODIFICATION

6.00

Tests 2.00

Close-Up 1.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

NOTE: The manhours indicated for the Removal/Installation of the MLG Bogie Beam

Assembly and the Tests are only applicable if the MLG Bogie Beam Assembly

requires modification.

**CONF 002

Task 324279-831-895-001: MODIFICATION

Get Access 1.00

On Aircraft

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Task 324279-831-895-001: MODIFICATION

REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

6.00

INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER

MODIFICATION

6.00

Tests 2.00

Close-Up 1.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

NOTE: The manhours indicated for the Removal/Installation of the MLG Bogie Beam

Assembly and the Tests are only applicable if the MLG Bogie Beam Assembly

requires modification.

**CONF 003

Task 324279-831-895-001: MODIFICATION

Get Access 1.00

On Aircraft

REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

6.00

INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER

MODIFICATION

6.00

Tests 2.00

Close-Up 1.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

NOTE: The manhours indicated for the Removal/Installation of the MLG Bogie Beam

Assembly and the Tests are only applicable if the MLG Bogie Beam Assembly

requires modification.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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**CONF 004

Task 324279-831-895-001: MODIFICATION

Get Access 1.00

On Aircraft

REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

6.00

INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER

MODIFICATION

6.00

Tests 2.00

Close-Up 1.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

RE-IDENTIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-284

MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND

BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-284

NOTE: The manhours indicated for the Removal/Installation of the MLG Bogie Beam

Assembly and the Tests are only applicable if the MLG Bogie Beam Assembly

requires modification.

**CONF 005

Task 324279-831-895-001: MODIFICATION

Get Access 1.00

On Aircraft

REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

6.00

INSTALL THE MLG BOGIE BEAM ASSEMBLY AFTER

MODIFICATION

6.00

Tests 2.00

Close-Up 1.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

RE-IDENTIFY THE BOGIE BEAM AXLE AND

SPACER SUB-ASSEMBLY, BOGIE BEAM SUBASSEMBLY AND BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-283

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Task 324279-831-895-001: MODIFICATION

MODIFY THE BOGIE BEAM AXLE AND SPACER

SUB-ASSEMBLY, BOGIE BEAM SUB-ASSEMBLY

AND BOGIE BEAM M/C

Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-283

MARKING - STRIKE NUMBERS Messier-Dowty Service Bulletin No.

A33/34-32-283

NOTE: The manhours indicated for the Removal/Installation of the MLG Bogie Beam

Assembly and the Tests are only applicable if the MLG Bogie Beam Assembly

requires modification.

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 07-11-00 32-00-00 32-11-00

32-11-14 32-49-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Vendor Service Bulletin (VSB) Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 002

Aircraft Maintenance Manual (AMM) 07-11-00 32-00-00 32-11-00

32-11-14 32-49-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Vendor Service Bulletin (VSB) Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 003

Aircraft Maintenance Manual (AMM) 07-11-00 32-00-00 32-11-00

32-11-14 32-49-00

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ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Vendor Service Bulletin (VSB) Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 004

Aircraft Maintenance Manual (AMM) 07-11-00 32-00-00 32-11-00

32-11-14 32-49-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Vendor Service Bulletin (VSB) Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-284

**CONF 005

Aircraft Maintenance Manual (AMM) 07-11-00 32-00-00 32-11-00

32-11-14 32-49-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Vendor Service Bulletin (VSB) Messier-Dowty Service Bulletin No.

A33/34-32-278

Messier-Dowty Service Bulletin No.

A33/34-32-283

**CONF ALL

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 32-11-05 32-11-14 32-11-15

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Bogie Beam & Axle

Sub-Assy

201272240 201272246 01 YES

Bogie Beam Sub-Assy 201272230 201272243 01 YES

Bogie Beam M/C 201272300 201272305 01 YES

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Bogie Beam & Axle

Sub-Assy

201272239 201272247 01 YES

Bogie Beam Sub-Assy 201272228 201272244 01 YES

Bogie Beam M/C 201272302 201272306 01 YES

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Bogie Beam & Axle

Sub-Assy

201485206 201485208 01 YES

Bogie Beam Sub-Assy 201485205 201485207 01 YES

Bogie Beam M/C 201485300 201485301 01 YES

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Bogie Beam & Axle

Sub-Assy

201485206 201485208 01 YES

Bogie Beam Sub-Assy 201485205 201485207 01 YES

Bogie Beam M/C 201485300 201485301 01 YES

Bogie Beam & Axle

Sub-Assy

201272236 201272248 01 YES

Bogie Beam Sub-Assy 201272235 201272245 01 YES

Bogie Beam M/C 201272304 201272307 01 YES

Bogie Beam & Axle

Sub-Assy

201272238 201272247 01 YES

Bogie Beam Sub-Assy 201272226 201272244 01 YES

Bogie Beam M/C 201272302 201272306 01 YES

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NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 005

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Bogie Beam M/C 50-2117002-00 50-2117002-01 01 YES

Bogie Beam Sub-Assy 30-2117002-00 30-2117002-01 01 YES

Bogie Beam, Axle &

Spacer Sub-Assy

30-2117004-00 30-2117004-01 01 YES

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF ALL

M. SPARES

None

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with MESSIER-DOWTY

as per instructions given in Service Bulletin No. A33/34-32-283 or A33/34-32-284.

(2) Price and Availability

For the equipment modification sales terms refer to MESSIER-DOWTY Service Bulletin

No. A33/34-32-283 or A33/34-32-284.

B. INDUSTRY SUPPORT INFORMATION

For the industry support terms refer to MESSIER -DOWTY Service Bulletin No.

A33/34-32-283 or A33/34-32-284.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

Ardrox AV100D Wax Oil (Temporary

Protective Compound)

15-008 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

For the re-identification of parts refer to MESSIER-DOWTY Service Bulletin No.

A33/34-32-283 or MESSIER-DOWTY Service Bulletin No. A33/34-32-284.

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Reidentified part set REIDB01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272243 Bogie 201272230 (1)

201272246 Bogie 201272240 (2)

201272305 Bogie 201272300 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Reidentified part set REIDB02

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

30-2117002-01 Bogie 30-2117002-00 (1)

30-2117004-01 Bogie 30-2117004-00 (2)

50-2117002-01 Bogie 50-2117002-00 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam, Axle & Spacer Sub-Assy

NOTE (3): Bogie Beam M/C

Reidentified part set REIDB03

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272244 Bogie 201272228 (1)

201272247 Bogie 201272239 (2)

201272306 Bogie 201272302 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Reidentified part set REIDB04

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201485207 Bogie 201485205 (1)

201485208 Bogie 201485206 (2)

201485301 Bogie 201485300 (3)

NOTE (1): Bogie Beam Sub-Assy

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SERVICE BULLETIN

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Reidentified part set REIDB05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272245 Bogie 201272235 (1)

201272248 Bogie 201272236 (2)

201272307 Bogie 201272304 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Reidentified part set REIDB06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272244 Bogie 201272226 (1)

201272247 Bogie 201272238 (2)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

Reidentified part set REIDB07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272306 Bogie 201272302 (1)

NOTE (1): Bogie Beam M/C

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

For the standard tools refer to MESSIER-DOWTY Service Bulletin No. A33/34-32-283 or

A33/34-32-284.

NOTE: A spray lance (1.50 metres minimum length) MUST be used to ensure

that the paint can be applied evenly to the bogie beam bore.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 17

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SERVICE BULLETIN

(3) Special Tools

For the special tools refer to MESSIER-DOWTY Service Bulletin No. A33/34-32-283 or

A33/34-32-284.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 18

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 324279-831-895-001 - 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.

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

Task Associated Data

**CONF 001

Zone

731 741

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

Messier-Dowty Service Bulletin No. A33/34-32-278

Messier-Dowty Service Bulletin No. A33/34-32-284

**CONF 002

Zone

731 741

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

Messier-Dowty Service Bulletin No. A33/34-32-278

Messier-Dowty Service Bulletin No. A33/34-32-284

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 19

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SERVICE BULLETIN

**CONF 003

Zone

731 741

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

Messier-Dowty Service Bulletin No. A33/34-32-278

Messier-Dowty Service Bulletin No. A33/34-32-284

**CONF 004

Zone

731 741

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

Messier-Dowty Service Bulletin No. A33/34-32-284

Messier-Dowty Service Bulletin No. A33/34-32-278

**CONF 005

Zone

731 741

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 10.00

Additional manhours related to Vendor SB; refer to:

Messier-Dowty Service Bulletin No. A33/34-32-283

Messier-Dowty Service Bulletin No. A33/34-32-278

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 324279-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills UTILITY

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

Service Bulletin.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 20

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@A340

SERVICE BULLETIN

**CONF 002

(1) Subtask 324279-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills UTILITY

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

Service Bulletin.

**CONF 003

(1) Subtask 324279-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills UTILITY

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

Service Bulletin.

**CONF 004

(1) Subtask 324279-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills UTILITY

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

Service Bulletin.

**CONF 005

(1) Subtask 324279-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills UTILITY

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 324279-941-401-001 - JOB SET-UP

Work Zones and Access Panels

Zone Access/Work location

731

741

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 21

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SERVICE BULLETIN

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-00-210-807

(a) Do the Job Set-up procedure as specified in task ’Detailed Inspection of MLG Bogie

Beam’ (Refer to AMM Task 32-11-00-210-807).

(b) If the Bogie Beam M/C part number is not listed in Section 1. L.

(INTERCHANGEABILITY/MIXABILITY), contact AIRBUS department SEEL3 for

instruction.

**CONF 002

(1) Subtask 324279-941-401-001 - JOB SET-UP

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-00-210-807

(a) Do the Job Set-up procedure as specified in task ’Detailed Inspection of MLG Bogie

Beam’ (Refer to AMM Task 32-11-00-210-807).

(b) If the Bogie Beam M/C part number is not listed in Section 1. L.

(INTERCHANGEABILITY/MIXABILITY), contact AIRBUS department SEEL3 for

instruction.

**CONF 003

(1) Subtask 324279-941-401-001 - JOB SET-UP

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-00-210-807

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 22

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SERVICE BULLETIN

(a) Do the Job Set-up procedure as specified in task ’Detailed Inspection of MLG Bogie

Beam’ (Refer to AMM Task 32-11-00-210-807).

(b) If the Bogie Beam M/C part number is not listed in Section 1. L.

(INTERCHANGEABILITY/MIXABILITY), contact AIRBUS department SEEL3 for

instruction.

**CONF 004

(1) Subtask 324279-941-401-006 - JOB SET-UP

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-00-210-807

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-284

Fig. A-UBAAA

BOGIE BEAM M/C - SERIAL NUMBER

LOCATION

Sheet 01

(a) Do the Job Set-up procedure as specified in task ’Detailed Inspection of MLG Bogie

Beam’ (Refer to AMM Task 32-11-00-210-807).

(b) If the Bogie Beam M/C Part Number is 201272304, do a visual check for the serial

number (Refer to Appendix A of Messier-Dowty Service Bulletin No. A33/34-32-284

and Fig. A-UBAAA Sheet 01):

1 If the serial number of the Bogie Beam M/C is not clear, use a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

to clean the area.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 23

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SERVICE BULLETIN

2 If the Bogie Beam M/C serial number is listed in Appendix A, do SUBTASK

324279-930-401 001 RE-IDENTIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C .

3 If the Bogie Beam M/C serial number is not listed in Appendix A,

do SUBTASK 324279-020-401 001 REMOVE THE MLG BOGIE BEAM

ASSEMBLY FOR MODIFICATION .

(c) If the Bogie Beam M/C Part Number is not 201272304, do SUBTASK

324279-020-401 001 REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION .

(d) If the Bogie Beam M/C part number is not listed in Section 1. L.

(INTERCHANGEABILITY/MIXABILITY), contact AIRBUS department SEEL3 for

instruction.

**CONF 005

(1) Subtask 324279-941-401-002 - JOB SET-UP

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-00-210-807

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-283

Fig. A-UBAAA

BOGIE BEAM M/C - SERIAL NUMBER

LOCATION

Sheet 01

(a) Do the Job Set-up procedure as specified in task ’Detailed Inspection of MLG Bogie

Beam’ (Refer to AMM Task 32-11-00-210-807).

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 24

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SERVICE BULLETIN

(b) If the Bogie Beam M/C Part Number is 50-2117002-00, do a visual check for

the serial number Refer to Appendix A of Messier-Dowty Service Bulletin No.

A33/34-32-283 and Fig. A-UBAAA Sheet 01):

1 If the serial number of the Bogie Beam M/C is not clear, use a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

to clean the area.

2 If the Bogie Beam M/C serial number is listed in Appendix A, do SUBTASK

324279-930-401 002 RE-IDENTIFY THE BOGIE BEAM AXLE AND SPACER

SUB-ASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C .

3 If the Bogie Beam M/C serial number is not listed in Appendix A,

do SUBTASK 324279-020-401 001 REMOVE THE MLG BOGIE BEAM

ASSEMBLY FOR MODIFICATION .

(c) If the Bogie Beam M/C part number is not listed in Section 1. L.

(INTERCHANGEABILITY/MIXABILITY), contact AIRBUS department SEEL3 for

instruction.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 324279-020-401-001 - REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-000-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 25

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SERVICE BULLETIN

(a) Remove the MLG bogie beam assembly (Refer to AMM Task 32-11-14-000-801).

(2) Subtask 324279-831-401-001 - MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

Work Zones and Access Panels

Zone Access/Work location

731

741

Material necessary to do the job

Reidentified part set REIDB01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272243 Bogie 201272230 (1)

201272246 Bogie 201272240 (2)

201272305 Bogie 201272300 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Ardrox AV100D Wax Oil

(Temporary Protective

Compound)

15-008 As required

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-278

Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Do a visual inspection of the internal bore of the bogie beam and record the results

of the inspection (Refer to Messier-Dowty Service Bulletin No. A33/34-32-278).

(b) Modify the bogie beam and axle sub-assembly, bogie beam sub-assembly and

bogie beam M/C (Refer to Messier-Dowty Service Bulletin No. A33/34-32-284):

Modify and re-identify

2 Bogie Beam & Axle

Sub-Assy

201272240

to

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 26

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SERVICE BULLETIN

2 Bogie Beam & Axle

Sub-Assy

201272246

Modify and re-identify

2 Bogie Beam Sub-Assy 201272230

to

2 Bogie Beam Sub-Assy 201272243

Modify and re-identify

2 Bogie Beam M/C 201272300

to

2 Bogie Beam M/C 201272305

(c) Apply

Ardrox AV100D

Wax Oil (Temporary

Protective

Compound)

15-008 As required

to the bore of the bogie beam (Refer to Messier-Dowty Service Bulletin No.

A33/34-32-284).

(3) Subtask 324279-420-401-001 - INSTALL THE MLG BOGIE BEAM ASSEMBLY

AFTER MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Install the MLG bogie beam assembly (Refer to AMM Task 32-11-14-400-801).

(b) Go to SUBTASK 324279-930-402 001 MARKING - STRIKE NUMBERS .

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 27

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SERVICE BULLETIN

(4) Subtask 324279-930-402-001 - MARKING - STRIKE NUMBERS

Work Zones and Access Panels

Zone Access/Work location

731

741

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Cancel the strike number 25 on the MLG bogie and dressings nameplate (Refer to

Messier-Dowty Service Bulletin No. A33/34-32-284).

**CONF 002

(1) Subtask 324279-020-401-001 - REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-000-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Remove the MLG bogie beam assembly (Refer to AMM Task 32-11-14-000-801).

(2) Subtask 324279-831-401-002 - MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

Work Zones and Access Panels

Zone Access/Work location

731

741

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 28

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@A340

SERVICE BULLETIN

Material necessary to do the job

Reidentified part set REIDB03

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272244 Bogie 201272228 (1)

201272247 Bogie 201272239 (2)

201272306 Bogie 201272302 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Ardrox AV100D Wax Oil

(Temporary Protective

Compound)

15-008 As required

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-278

Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Do a visual inspection of the internal bore of the bogie beam and record the results

of the inspection (Refer to Messier-Dowty Service Bulletin No. A33/34-32-278).

(b) Modify the bogie beam and axle sub-assembly, bogie beam sub-assembly and

bogie beam M/C (Refer to Messier-Dowty Service Bulletin No. A33/34-32-284):

Modify and re-identify

2 Bogie Beam & Axle

Sub-Assy

201272239

to

2 Bogie Beam & Axle

Sub-Assy

201272247

Modify and re-identify

2 Bogie Beam Sub-Assy 201272228

to

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 29

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SERVICE BULLETIN

2 Bogie Beam Sub-Assy 201272244

Modify and re-identify

2 Bogie Beam M/C 201272302

to

2 Bogie Beam M/C 201272306

(c) Apply

Ardrox AV100D

Wax Oil (Temporary

Protective

Compound)

15-008 As required

to the bore of the bogie beam (Refer to Messier-Dowty Service Bulletin No.

A33/34-32-284).

(3) Subtask 324279-420-401-001 - INSTALL THE MLG BOGIE BEAM ASSEMBLY

AFTER MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Install the MLG bogie beam assembly (Refer to AMM Task 32-11-14-400-801).

(b) Go to SUBTASK 324279-930-402 001 MARKING - STRIKE NUMBERS .

(4) Subtask 324279-930-402-001 - MARKING - STRIKE NUMBERS

Work Zones and Access Panels

Zone Access/Work location

731

741

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 30

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@A340

SERVICE BULLETIN

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Cancel the strike number 25 on the MLG bogie and dressings nameplate (Refer to

Messier-Dowty Service Bulletin No. A33/34-32-284).

**CONF 003

(1) Subtask 324279-020-401-001 - REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-000-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Remove the MLG bogie beam assembly (Refer to AMM Task 32-11-14-000-801).

(2) Subtask 324279-831-401-003 - MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

Work Zones and Access Panels

Zone Access/Work location

731

741

Material necessary to do the job

Reidentified part set REIDB04

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201485207 Bogie 201485205 (1)

201485208 Bogie 201485206 (2)

201485301 Bogie 201485300 (3)

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 31

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SERVICE BULLETIN

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Ardrox AV100D Wax Oil

(Temporary Protective

Compound)

15-008 As required

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-278

Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Do a visual inspection of the internal bore of the bogie beam and record the results

of the inspection (Refer to Messier-Dowty Service Bulletin No. A33/34-32-278).

(b) Modify the bogie beam and axle sub-assembly, bogie beam sub-assembly and

bogie beam M/C (Refer to Messier-Dowty Service Bulletin No. A33/34-32-284):

Modify and re-identify

2 Bogie Beam & Axle

Sub-Assy

201485206

to

2 Bogie Beam & Axle

Sub-Assy

201485208

Modify and re-identify

2 Bogie Beam Sub-Assy 201485205

to

2 Bogie Beam Sub-Assy 201485207

Modify and re-identify

2 Bogie Beam M/C 201485300

to

2 Bogie Beam M/C 201485301

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 32

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@A340

SERVICE BULLETIN

(c) Apply

Ardrox AV100D

Wax Oil (Temporary

Protective

Compound)

15-008 As required

to the bore of the bogie beam (Refer to Messier-Dowty Service Bulletin No.

A33/34-32-284).

(3) Subtask 324279-420-401-001 - INSTALL THE MLG BOGIE BEAM ASSEMBLY

AFTER MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Install the MLG bogie beam assembly (Refer to AMM Task 32-11-14-400-801).

(b) Go to SUBTASK 324279-930-402 001 MARKING - STRIKE NUMBERS .

(4) Subtask 324279-930-402-001 - MARKING - STRIKE NUMBERS

Work Zones and Access Panels

Zone Access/Work location

731

741

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Cancel the strike number 25 on the MLG bogie and dressings nameplate (Refer to

Messier-Dowty Service Bulletin No. A33/34-32-284).

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 33

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**CONF 004

(1) Subtask 324279-930-401-001 - RE-IDENTIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

Work Zones and Access Panels

Zone Access/Work location

731

741

Material necessary to do the job

Reidentified part set REIDB05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272245 Bogie 201272235 (1)

201272248 Bogie 201272236 (2)

201272307 Bogie 201272304 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Re-identify the bogie beam and axle sub-assy, bogie beam sub-assy and

bogie beam M/C, that follow (Refer to Messier-Dowty Service Bulletin No.

A33/34-32-284):

Re-identify

2 Bogie Beam & Axle

Sub-Assy

201272236

to

2 Bogie Beam & Axle

Sub-Assy

201272248

Re-identify

2 Bogie Beam Sub-Assy 201272235

to

2 Bogie Beam Sub-Assy 201272245

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 34

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SERVICE BULLETIN

Re-identify

2 Bogie Beam M/C 201272304

to

2 Bogie Beam M/C 201272307

(b) Go to SUBTASK 324279-930-402 001 MARKING - STRIKE NUMBERS .

(2) Subtask 324279-020-401-001 - REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-000-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Remove the MLG bogie beam assembly (Refer to AMM Task 32-11-14-000-801).

(3) Subtask 324279-831-401-004 - MODIFY THE BOGIE BEAM AND AXLE SUBASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

Work Zones and Access Panels

Zone Access/Work location

731

741

Material necessary to do the job

Reidentified part set REIDB04

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201485207 Bogie 201485205 (1)

201485208 Bogie 201485206 (2)

201485301 Bogie 201485300 (3)

NOTE (1): Bogie Beam Sub-Assy

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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SERVICE BULLETIN

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Reidentified part set REIDB05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272245 Bogie 201272235 (1)

201272248 Bogie 201272236 (2)

201272307 Bogie 201272304 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

NOTE (3): Bogie Beam M/C

Reidentified part set REIDB06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272244 Bogie 201272226 (1)

201272247 Bogie 201272238 (2)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam & Axle Sub-Assy

Reidentified part set REIDB07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

201272306 Bogie 201272302 (1)

NOTE (1): Bogie Beam M/C

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Ardrox AV100D Wax Oil

(Temporary Protective

Compound)

15-008 As required

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-278

Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Do a visual inspection of the internal bore of the bogie beam and record the results

of the inspection (Refer to Messier-Dowty Service Bulletin No. A33/34-32-278).

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 36

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SERVICE BULLETIN

(b) Modify the bogie beam and axle sub-assembly, bogie beam sub-assembly and

bogie beam M/C (Refer to Messier-Dowty Service Bulletin No. A33/34-32-284):

Modify and re-identify

2 Bogie Beam & Axle

Sub-Assy

201485206

to

2 Bogie Beam & Axle

Sub-Assy

201485208

OR

Modify and re-identify

2 Bogie Beam & Axle

Sub-Assy

201272236

to

2 Bogie Beam & Axle

Sub-Assy

201272248

OR

Modify and re-identify

2 Bogie Beam & Axle

Sub-Assy

201272238

to

2 Bogie Beam & Axle

Sub-Assy

201272247

Modify and re-identify

2 Bogie Beam Sub-Assy 201485205

to

2 Bogie Beam Sub-Assy 201485207

OR

Modify and re-identify

2 Bogie Beam Sub-Assy 201272235

to

2 Bogie Beam Sub-Assy 201272245

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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SERVICE BULLETIN

OR

Modify and re-identify

2 Bogie Beam Sub-Assy 201272226

to

2 Bogie Beam Sub-Assy 201272244

Modify and re-identify

2 Bogie Beam M/C 201485300

to

2 Bogie Beam M/C 201485301

OR

Modify and re-identify

2 Bogie Beam M/C 201272304

to

2 Bogie Beam M/C 201272307

OR

Modify and re-identify

2 Bogie Beam M/C 201272302

to

2 Bogie Beam M/C 201272306

(c) Apply

Ardrox AV100D

Wax Oil (Temporary

Protective

Compound)

15-008 As required

to the bore of the bogie beam (Refer to Messier-Dowty Service Bulletin No.

A33/34-32-284).

(4) Subtask 324279-420-401-001 - INSTALL THE MLG BOGIE BEAM ASSEMBLY

AFTER MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

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741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Install the MLG bogie beam assembly (Refer to AMM Task 32-11-14-400-801).

(b) Go to SUBTASK 324279-930-402 001 MARKING - STRIKE NUMBERS .

(5) Subtask 324279-930-402-001 - MARKING - STRIKE NUMBERS

Work Zones and Access Panels

Zone Access/Work location

731

741

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-284

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Cancel the strike number 25 on the MLG bogie and dressings nameplate (Refer to

Messier-Dowty Service Bulletin No. A33/34-32-284).

**CONF 005

(1) Subtask 324279-930-401-002 - RE-IDENTIFY THE BOGIE BEAM AXLE AND

SPACER SUB-ASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

Work Zones and Access Panels

Zone Access/Work location

731

741

Material necessary to do the job

Reidentified part set REIDB02

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

30-2117002-01 Bogie 30-2117002-00 (1)

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

30-2117004-01 Bogie 30-2117004-00 (2)

50-2117002-01 Bogie 50-2117002-00 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam, Axle & Spacer Sub-Assy

NOTE (3): Bogie Beam M/C

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-283

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Re-identify the bogie beam axle and spacer sub-assy, bogie beam sub-assy

and bogie beam M/C that follow (Refer to Messier-Dowty Service Bulletin No.

A33/34-32-283):

Re-identify

2 Bogie Beam, Axle &

Spacer Sub-Assy

30-2117004-00

to

2 Bogie Beam, Axle &

Spacer Sub-Assy

30-2117004-01

Re-identify

2 Bogie Beam Sub-Assy 30-2117002-00

to

2 Bogie Beam Sub-Assy 30-2117002-01

Re-identify

2 Bogie Beam M/C 50-2117002-00

to

2 Bogie Beam M/C 50-2117002-01

(b) Go to SUBTASK 324279-930-402 002 MARKING - STRIKE NUMBERS .

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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(2) Subtask 324279-020-401-001 - REMOVE THE MLG BOGIE BEAM ASSEMBLY FOR

MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-000-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Remove the MLG bogie beam assembly (Refer to AMM Task 32-11-14-000-801).

(3) Subtask 324279-831-401-005 - MODIFY THE BOGIE BEAM AXLE AND SPACER

SUB-ASSEMBLY, BOGIE BEAM SUB-ASSEMBLY AND BOGIE BEAM M/C

Work Zones and Access Panels

Zone Access/Work location

731

741

Material necessary to do the job

Reidentified part set REIDB02

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

30-2117002-01 Bogie 30-2117002-00 (1)

30-2117004-01 Bogie 30-2117004-00 (2)

50-2117002-01 Bogie 50-2117002-00 (3)

NOTE (1): Bogie Beam Sub-Assy

NOTE (2): Bogie Beam, Axle & Spacer Sub-Assy

NOTE (3): Bogie Beam M/C

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 41

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SERVICE BULLETIN

Consumable CMLB00

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Ardrox AV100D Wax Oil

(Temporary Protective

Compound)

15-008 As required

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-278

Messier-Dowty A33/34-32-283

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Do a visual inspection of the internal bore of the bogie beam and record the results

of the inspection (Refer to Messier-Dowty Service Bulletin No. A33/34-32-278).

(b) Modify the bogie beam axle and spacer sub-assembly, bogie assembly and bogie

beam M/C (Refer to Messier-Dowty Service Bulletin No. A33/34-32-283):

Modify and re-identify

2 Bogie Beam, Axle &

Spacer Sub-Assy

30-2117004-00

to

2 Bogie Beam, Axle &

Spacer Sub-Assy

30-2117004-01

Modify and re-identify

2 Bogie Beam Sub-Assy 30-2117002-00

to

2 Bogie Beam Sub-Assy 30-2117002-01

Modify and re-identify

2 Bogie Beam M/C 50-2117002-00

to

2 Bogie Beam M/C 50-2117002-01

(c) Apply

Ardrox AV100D

Wax Oil (Temporary

Protective

Compound)

15-008 As required

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 42

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SERVICE BULLETIN

to the bore of the bogie beam (Refer to Messier-Dowty Service Bulletin No.

A33/34-32-283).

(4) Subtask 324279-420-401-001 - INSTALL THE MLG BOGIE BEAM ASSEMBLY

AFTER MODIFICATION

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Install the MLG bogie beam assembly (Refer to AMM Task 32-11-14-400-801).

(b) Go to SUBTASK 324279-930-402 002 MARKING - STRIKE NUMBERS .

(5) Subtask 324279-930-402-002 - MARKING - STRIKE NUMBERS

Work Zones and Access Panels

Zone Access/Work location

731

741

References

Vendor Service Bulletin (VSB) Messier-Dowty A33/34-32-283

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG.

(a) Cancel the strike number 2 on the MLG bogie and dressings nameplate (Refer to

Messier-Dowty Service Bulletin No. A33/34-32-283).

**CONF ALL

D. TEST

NOTE: The tests that follow are only applicable if the MLG bogie beam assembly was

removed for modification.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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SERVICE BULLETIN

**CONF 001

(1) Subtask 324279-740-401-001 - BITE

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

Task 32-49-00-740-801

(a) Do the BITE test of the Normal Extension and Retraction System and the BITE test

of the Braking/Steering Control Unit (BSCU) as given in AMM Task ’Installation of

the MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

(b) If installed, do a BITE test of the TPIS (Refer to AMM Task 32-49-00-740-801).

(2) Subtask 324279-720-401-001 - FUNCTIONAL

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

(a) Do the functional and operational tests as given in AMM Task ’Installation of the

MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

**CONF 002

(1) Subtask 324279-740-401-001 - BITE

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

Task 32-49-00-740-801

(a) Do the BITE test of the Normal Extension and Retraction System and the BITE test

of the Braking/Steering Control Unit (BSCU) as given in AMM Task ’Installation of

the MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

(b) If installed, do a BITE test of the TPIS (Refer to AMM Task 32-49-00-740-801).

(2) Subtask 324279-720-401-001 - FUNCTIONAL

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

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SERVICE BULLETIN

(a) Do the functional and operational tests as given in AMM Task ’Installation of the

MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

**CONF 003

(1) Subtask 324279-740-401-001 - BITE

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

Task 32-49-00-740-801

(a) Do the BITE test of the Normal Extension and Retraction System and the BITE test

of the Braking/Steering Control Unit (BSCU) as given in AMM Task ’Installation of

the MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

(b) If installed, do a BITE test of the TPIS (Refer to AMM Task 32-49-00-740-801).

(2) Subtask 324279-720-401-001 - FUNCTIONAL

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

(a) Do the functional and operational tests as given in AMM Task ’Installation of the

MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

**CONF 004

(1) Subtask 324279-740-401-001 - BITE

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

Task 32-49-00-740-801

(a) Do the BITE test of the Normal Extension and Retraction System and the BITE test

of the Braking/Steering Control Unit (BSCU) as given in AMM Task ’Installation of

the MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

(b) If installed, do a BITE test of the TPIS (Refer to AMM Task 32-49-00-740-801).

(2) Subtask 324279-720-401-001 - FUNCTIONAL

Manpower Resources

Skills AIRFRAME

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

(a) Do the functional and operational tests as given in AMM Task ’Installation of the

MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

**CONF 005

(1) Subtask 324279-740-401-001 - BITE

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

Task 32-49-00-740-801

(a) Do the BITE test of the Normal Extension and Retraction System and the BITE test

of the Braking/Steering Control Unit (BSCU) as given in AMM Task ’Installation of

the MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

(b) If installed, do a BITE test of the TPIS (Refer to AMM Task 32-49-00-740-801).

(2) Subtask 324279-720-401-001 - FUNCTIONAL

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-400-801

(a) Do the functional and operational tests as given in AMM Task ’Installation of the

MLG Bogie Beam Assembly’ (Refer to AMM Task 32-11-14-400-801).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 324279-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-801

Task 32-00-00-860-805

(a) If necessary, lower the aircraft off the jacks (Refer to AMM Task

07-11-00-586-801).

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(b) Do the ground configuration after flight configuration (Refer to AMM Task

32-00-00-860-805).

(c) Remove all the fixtures, tools, test and support equipment.

**CONF 002

(1) Subtask 324279-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-801

Task 32-00-00-860-805

(a) If necessary, lower the aircraft off the jacks (Refer to AMM Task

07-11-00-586-801).

(b) Do the ground configuration after flight configuration (Refer to AMM Task

32-00-00-860-805).

(c) Remove all the fixtures, tools, test and support equipment.

**CONF 003

(1) Subtask 324279-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-801

Task 32-00-00-860-805

(a) If necessary, lower the aircraft off the jacks (Refer to AMM Task

07-11-00-586-801).

(b) Do the ground configuration after flight configuration (Refer to AMM Task

32-00-00-860-805).

(c) Remove all the fixtures, tools, test and support equipment.

**CONF 004

(1) Subtask 324279-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-801

Task 32-00-00-860-805

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(a) If necessary, lower the aircraft off the jacks (Refer to AMM Task

07-11-00-586-801).

(b) Do the ground configuration after flight configuration (Refer to AMM Task

32-00-00-860-805).

(c) Remove all the fixtures, tools, test and support equipment.

**CONF 005

(1) Subtask 324279-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-801

Task 32-00-00-860-805

(a) If necessary, lower the aircraft off the jacks (Refer to AMM Task

07-11-00-586-801).

(b) Do the ground configuration after flight configuration (Refer to AMM Task

32-00-00-860-805).

(c) Remove all the fixtures, tools, test and support equipment.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 48

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SERVICE BULLETIN

**CONF 004 thru 005

LH MLG SHOWN

RH MLG SIMILAR

A

INSPECTION AREA

NOTE:

A

F_SB_324279_7_BAAA_01_00

Figure A-UBAAA - Sheet 01

BOGIE BEAM M/C - SERIAL NUMBER LOCATION

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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This Page Intentionally Left Blank

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 50

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SERVICE BULLETIN

APPENDIX 01 : ELAPSED TIME ASSUMPTION

**CONF ALL

For detail concerning the elapsed time assumptions, refer to the Gantt chart shown below:

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

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SERVICE BULLETIN

APPENDIX 01 : ELAPSED TIME ASSUMPTION

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−32−4279

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

16.00

10.00

STEPS

1.00 1.00

0 10

REMOVE THE MLG BOGIE 6.00 3.00

INSTALL THE MLG BOGIE 6.00 3.00

TEST 2.00 2.00

CLOSE−UP 1.00 1.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

01

02

NOTES:

PER

1

2

2

1

1

:

:

SB ELAPSED TIME

(HOURS)

2 4 6 8 12

BEAM ASSEMBLY FOR

BEAM ASSEMBLY AFTER

MODIFICATION

MODIFICATION

F_SB_324279_7_AAAA_01_00

Figure A-UAAAA - Sheet 01

ELAPSED TIME ASSUMPTION

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 2

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REPORTING SHEET

TITLE: LANDING GEAR - MAIN GEAR - IMPROVED 2-PART PAINT SCHEME

FOR BASIC, GROWTH AND ENHANCED MLG BOGIE BEAM

MODIFICATION No.: 58896H16355

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: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- 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: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279

REVISION No.: 01 - Oct 14/11 Page: 1

7

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