# @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 7

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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 7

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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 7

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# @A340 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 7

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# @A340 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 7

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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 7

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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 7

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# @A340 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 7

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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 7

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# @A340 SERVICE BULLETIN SUMMARY Task 324279-831-895-001: MODIFICATIONMODIFY 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: MODIFICATIONMODIFY 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. A33/34-32-283MODIFY 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 7

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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 7

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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 7

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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 REVISION No.: 01 - Oct 14/11 Page: 2 7

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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.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 3 7

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# @A340 SERVICE BULLETIN
**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 REVISION No.: 01 - Oct 14/11 Page: 4 7

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# @A340 SERVICE BULLETIN
**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 REVISION No.: 01 - Oct 14/11 Page: 5 7

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# @A340 SERVICE BULLETINbeen 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

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 6 7

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# @A340 SERVICE BULLETIN(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 REVISION No.: 01 - Oct 14/11 Page: 7 7

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# @A340 SERVICE BULLETIN
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

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 8 7

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# @A340 SERVICE BULLETIN

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 REVISION No.: 01 - Oct 14/11 Page: 9 7

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# @A340 SERVICE BULLETIN
**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. A33/34-32-284MODIFY 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 ANDSPACER SUB-ASSEMBLY, BOGIE BEAM SUBASSEMBLY AND BOGIE BEAM M/C Messier-Dowty Service Bulletin No. A33/34-32-283

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 10 7

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# @A340 SERVICE BULLETIN

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
DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 11 7

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# @A340 SERVICE BULLETIN
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.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 12 7

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# @A340 SERVICE BULLETIN
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
DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 13 7

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# @A340 SERVICE BULLETIN
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

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 14 7

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# @A340 SERVICE BULLETIN
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.

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 15 7

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# @A340 SERVICE BULLETIN 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 DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 16 7

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# @A340 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 7

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# @A340 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 7

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# @A340 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 7

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# @A340 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 7

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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 7

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# @A340 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 7

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# @A340 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 7

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# @A340 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 7

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# @A340 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 7

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# @A340 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 7

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# @A340 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 7

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# @A340 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 7

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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 7

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# @A340 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 7

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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 7

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# @A340 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 7

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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 7

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# @A340 SERVICE BULLETIN
**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 7

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# @A340 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 REVISION No.: 01 - Oct 14/11 Page: 35 7

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# @A340 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 7

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# @A340 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 REVISION No.: 01 - Oct 14/11 Page: 37 7

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# @A340 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 DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 38 7

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# @A340 SERVICE BULLETIN

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 REVISION No.: 01 - Oct 14/11 Page: 39 7

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# @A340 SERVICE BULLETIN

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 REVISION No.: 01 - Oct 14/11 Page: 40 7

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# @A340 SERVICE BULLETIN (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 7

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# @A340 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 7

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# @A340 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 REVISION No.: 01 - Oct 14/11 Page: 43 7

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# @A340 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
DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 44 7

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# @A340 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 REVISION No.: 01 - Oct 14/11 Page: 45 7

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# @A340 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 ).

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 46 7

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# @A340 SERVICE BULLETIN (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 DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 47 7

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# @A340 SERVICE BULLETIN (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 7

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# @A340 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 REVISION No.: 01 - Oct 14/11 Page: 49 7

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# @A340 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 18/11 SERVICE BULLETIN No.: A340-32-4279 REVISION No.: 01 - Oct 14/11 Page: 50 7

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# @A340 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 REVISION No.: 01 - Oct 14/11 Page: 1 7

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# @A340 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

10 0 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

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# @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

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# @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

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