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@A340
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 32 TITLE: LANDING GEAR - MAIN GEAR - INSPECTION - PARTS WITH 300M
MATERIAL PROPERTIES OUTSIDE OF SPECIFICATION
REQUIREMENTS MODIFICATION No.: None This page transmits Revision No.02 of Service Bulletin No.A340-32-4310
ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft inspected by any previous issue.
REASON Revision No. 02 issued to amend Appendix 04 - Life Limit Sheet 01 by updating the Applicability A340-2xx column and adding a NOTE for Main Fitting PNs 201488324, 201488335, 201488325 and 201488336.
CHANGES The main changes of this revision are:
- Update figure A-UAEAA
- Update the Service Bulletin effectivity.
SUMMARY
EFFECTIVITY
OPERATOR LIST UPDATED R
PLANNING INFORMATION
EFFECTIVITY
EFFECTIVITY RELATED INFORMATION
UPDATED R Configuration definition CONF 001
CONFIGURATION DEFINITION UPDATED R Appendix 04 - Life Limit Fig. A-UAEAA DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Fig. A-UAEAA Sheet 01
SHEET UPDATED R Fig. A-UAEAA Sheet 02
SHEET UPDATED R Fig. A-UAEAA Sheet 03
SHEET UPDATED R Fig. A-UAEAA Sheet 04
SHEET UPDATED R Appendix 05 - Definitions and Formulas Fig. A-UAHAA Fig. A-UAHAA Sheet 01
SHEET UPDATED R
FILING 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 Revision No. 01 issued to:
Aubert and Duval material source designated S4 to be deleted Amend Appendix 02 so that PN 201488325 is a RH main fitting and PN 201488335 is a LH main fitting.
REVISION SEQUENCE ORIGINAL: Aug 08/16 REVISION No. : 01 - Jan 31/17 REVISION No. : 02 - Jun 16/17 DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 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 - INSPECTION - PARTS WITH 300M
MATERIAL PROPERTIES OUTSIDE OF SPECIFICATION
REQUIREMENTS **CONF ALL
MODIFICATIONS None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES In 2006, Messier-Dowty identified a deficiency in the fatigue performance of 300M high strength steel used in forgings. The root cause for fatigue deficiency was process issues during the material preparation.
After thorough investigations, AIRBUS identified that the following material sources were impacted:
- Electralloy (Source 1)
- RSM (Source 2)
- Latrobe (Source 3).
Parts that have been identified as being manufactured from the suspect material properties issue are Main Fittings, Bogie Beams and Sliding Pistons installed on Main Landing Gear (MLG), Nose Landing Gear (NLG) and Center Landing Gear (CLG) of A330 and A340 aircraft. If the identified fatigue life of these suspect components is affected and were exceeded, subsequent failure could lead to a potentially unsafe condition of the aircraft.
Affected 300M Part Numbers (PNs) from Source 1 thru 3 were previously listed in the ALS Part 1, however, these PNs will now be managed through dedicated Airworthiness Directive/Service Bulletin in order to simplify the ALS Part 1.
This Inspection Service Bulletin is issued to:
- list affected part and Serial Numbers (SNs) DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY
- specify the reduced lives for the Main Fittings Bogie Beams and Sliding Pistons affected by the 300M material properties quality issue.
Accomplishment of this Inspection Service Bulletin will help in the detection of fatigue life of the Main Fittings, Bogie Beams and Sliding Pistons affected by the 300M material properties quality.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1)
CANCELS INSPECTION SB NO
POTENTIAL AD YES
A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
LROPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO NOTE
(1) : Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION No Material
EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :
01V 06Y 09M 14S 15R 17M 31V 39N 41N 65W 74W 83V 98W ABD AFR AIB ALD ARG AXY BOE CAL CPA DGA DLH EDW F2I
FIN GAF HFM HFY IBE IRC IRM KAC KMF M3R MAU MDG MRJ PAL PUE QQE ROI S3R SAA SAS SFB SLM SWR SYR
TAP THT
THY VCV
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None ISI None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None OTHER None
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT YES HARD NO SOFT NO DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY OBRM NO
MANPOWER **CONF 001 Task 324310-832-895-001: Inspection
TOTAL MANHOURS
4.00
ELAPSED TIME (HOURS)
2.50 **CONF 002 Task 324310-832-895-001: Inspection
TOTAL MANHOURS
4.00
ELAPSED TIME (HOURS)
2.50
APPENDICES **CONF ALL Appendix 01 - Bogie Beams Appendix 02 - Main Fittings Appendix 03 - Sliding Pistons Appendix 04 - Life Limit Appendix 05 - Definitions and Formulas Appendix 06 - Manpower Gantt Chart DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY **CONF ALL
LH SHOWN
RH SIMILAR Z730 (Z740) F_SB_324310_7_SAAA_01_00 Figure A-U SAAA - S heet 01 DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 32 TITLE: LANDING GEAR - MAIN GEAR - INSPECTION - PARTS WITH 300M
MATERIAL PROPERTIES OUTSIDE OF SPECIFICATION
REQUIREMENTS MODIFICATION No.: None This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent.
1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY
(1) Models 340-211 340-212 340-213 340-311 340-312 340-313
(2) Effectivity by MSN 0001-0002 0004 0009 0014 0020 0022-0023 0025-0026 0029 0031 0038 0041 0043-0044 0046-0047 0049 0051 0056-0058 0061 0063 0074-0076 0078-0081 0084 0089-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128 0134-0135 0139 0145-0146 0149-0152 0154 0156-0160 0163-0164 0166-0170 0174-0175 0178-0180 0185-0186 0190 0192-0194 0197 0199 0201-0202 0204 0207-0208 0210 0212-0215 0217-0218 0221 0227 0233 0236-0237 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332 0335 0347 0352 0354-0355 0367 0373-0374 0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0430 0433-0435 0438 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: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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 01V 0146 06Y 0139 0149 09M 0483 14S 0058 15R 0151 17M 0955 31V 0093 39N 0168 0174 41N 0009 65W 0029 74W 0047 0051 83V 0280 0292 98W 0014 0022 ABD 0210 AFR 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377 AIB 0001 0192 0243 0264 ALD 0156 0159 0178 ARG 0063 0074 0080 0123 0126 0128 0170 0193 0373 AXY 0374 BOE 0554 CAL 0402 0406 0411 0415 0433 0541 CPA 0157 0160 0208 0218 0227 DGA 0075 0081 DLH 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447 EDW 0562 F2I 0038 0043 0094 0114 0214 FIN 0835 0844 0921 0938 GAF 0274 0355 HFM 0117 0163 0166 0185 0236 0367 HFY 0190 0202 IBE 0125 0134 0145 0217 0221 0329 IRC 0002 IRM 0020 0056 0164 0282 KAC 0089 0090 0101 0104 KMF 0278 M3R 0061 MAU 0076 0152 0194 0268 0793 0800 MDG 0319 MRJ 0257 DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
OPERATOR MSN PAL 0302 0318 0332 0387 0459 0474 PUE 0212 0215 0399 QQE 0026 0528 ROI 0199 0201 S3R 0004 0204 SAA 0197 0378 0544 0582 0590 0643 0646 0651 SAS 0167 0413 0424 0430 0435 0450 0467 0470 SFB 0046 SLM 0049 0242 SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0585 0598 SYR 0381 TAP 0041 0044 0079 0091 THT 0385 0395 0438 0446 0668 THY 0023 0025 0057 0115 0180 0270 0331 VCV 0031
(4) Configuration by MSN MSN
CONFIGURATION 0001 0002 0004 0009 0014 0020 0022 0023 0025 0026 0029 0031 0038 0041 0043 0044 0046 0047 0049 0051 0056 0057 0058 0061 0063 0074 0075 0076 0078 0079 0080 0081 0084 0089 0090 0091 0093 0094 0101 0104 0114 0115 0117 0123 0125 0126 0128 0134 0135 0139 0145 0146 0149 0150 0151 0152 0154 0156 0157 0158 0159 0160 0163 0164 0166 0167 0168 0169 0170 0174 0175 0178 0179 0180 0185 0186 0190 0192 0193 0194 0197 0199 0201 0202 0204 0207 0208 0210 0212 0213 0214 0215 0217 0218 0221 0227 0233 0236 0237 0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352 0354 0355 0367 0373 0374 0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0430 0433 0434 0435 0438 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 001 0793 0800 0835 0844 0921 0938 0955 002
(5) Configuration definition **CONF 001 Config. 001 is valid for aircraft with Basic and Growth MLG.
**CONF 002 Config. 002 is valid for aircraft with Enhanced MLG.
(6) Material Effectivity No Material Set DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN B. CONCURRENT REQUIREMENTS None C. REASON
(1) History In 2006, Messier-Dowty identified a deficiency in the fatigue performance of 300M high strength steel used in forgings. The root cause for fatigue deficiency was process issues during the material preparation.
After thorough investigations, AIRBUS identified that the following material sources were impacted:
- Electralloy (Source 1)
- RSM (Source 2)
- Latrobe (Source 3).
Parts that have been identified as being manufactured from the suspect material properties issue are Main Fittings, Bogie Beams and Sliding Pistons installed on Main Landing Gear (MLG), Nose Landing Gear (NLG) and Center Landing Gear (CLG) of A330 and A340 aircraft. If the identified fatigue life of these suspect components is affected and were exceeded, subsequent failure could lead to a potentially unsafe condition of the aircraft.
Affected 300M Part Numbers (PNs) from Source 1 thru 3 were previously listed in the ALS Part 1, however, these PNs will now be managed through dedicated Airworthiness Directive/Service Bulletin in order to simplify the ALS Part 1.
(2) Objective/Action This Inspection Service Bulletin is issued to:
- list affected part and Serial Numbers (SNs)
- specify the reduced lives for the Main Fittings Bogie Beams and Sliding Pistons affected by the 300M material properties quality issue.
(3) Advantages Accomplishment of this Inspection Service Bulletin will help in the detection of fatigue life of the Main Fittings, Bogie Beams and Sliding Pistons affected by the 300M material properties quality.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN **CONF 001 Task 324310-832-895-001: Inspection
(1) Identify the PN and SN on the Basic and Growth Left Hand (LH) MLG Common Standard Bogie Beam
(2) Identify the PN and SN on the Basic and Growth Right Hand (RH) MLG Common Standard Bogie Beam
(3) Identify the PN and SN on the Basic LH MLG Hybrid Standard and Growth Main Fitting
(4) Identify the PN and SN on the Basic RH MLG Hybrid Standard and Growth Main Fitting
(5) Identify the PN and SN on the Growth LH MLG Standard Sliding Pistons
(6) Identify the PN and SN on the Growth RH MLG Standard Sliding Pistons **CONF 002 Task 324310-832-895-001: Inspection
(1) Identify the PN and SN on the Enhanced LH MLG Bogie Beam
(2) Identify the PNs and SN on the Enhanced RH MLG Bogie Beam
(3) Identify the PN and SN on the Enhanced LH MLG Main Fitting
(4) Identify the PN and SN on the Enhanced RH MLG Main Fitting
(5) Identify the PN and SN on the Enhanced LH MLG Standard Sliding Pistons
(6) Identify the PN and SN on the Enhanced RH MLG Standard Sliding Pistons **CONF ALL E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued to confirm this classification. The accomplishment timescale, which has not yet been defined, will be given in the AD.
DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 5 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approv al 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 324310-832-895-001: Inspection Get Access
0.50 On Aircraft Identify the PN and SN on the Basic and Growth Left Hand (LH) MLG Common Standard Bogie Beam
0.50 Identify the PN and SN on the Basic and Growth Right Hand (RH) MLG Common Standard Bogie Beam
0.50 Identify the PN and SN on the Basic LH MLG Hybrid Standard and Growth Main Fitting
0.50 Identify the PN and SN on the Basic RH MLG Hybrid Standard and Growth Main Fitting
0.50 Identify the PN and SN on the Growth LH MLG Standard Sliding Pistons
0.50 Identify the PN and SN on the Growth RH MLG Standard Sliding Pistons
0.50 Close-Up
0.50
TOTAL MANHOURS
4.00
ELAPSED TIME (HOURS)
2.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-UAGAA given in Appendix 06 - Manpower Gantt Chart .
**CONF 002 Task 324310-832-895-001: Inspection Get Access
0.50 On Aircraft Identify the PN and SN on the Enhanced LH MLG Bogie Beam
0.50 DATE: Aug 08/16 SERVICE BULLETIN No.: A340-32-4310 REVISION No.: 02 - Jun 16/17 Page: 6 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.