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© Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-3984; AD 2017-14-01 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Manufacturer
- Airbus
- Type
- Service Bulletin
- Number
- A340-32-4300
- Latest revision known
- A340-32-4300, Revision 01, dated September 21, 2015
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@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 - INTRODUCE NICKEL UNDER CHROME
PATCH AND NEW BOGIESTOP PAD ON ENHANCED MLG BOGIE BEAM **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR 204421H16719 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 This Service Bulletin is to introduce the application of Nickel under Chrome to improve the protection to the surface of the Bogie Beam under the area of the Stop Pad.
This Service Bulletin is published to advise operators of A340 aircra ft of the issue of MESSIER BUGATTI DOWTY Service Bulletin No. A33/34-32-305, which introduces procedures to:
- install a Nickel under Chrome coating to improve the protective treatments under the Bogie Beam Stop Pad
- install a new Bogie Beam Stop Pad which will have a reduced thickness to allow for the new Nickel under Chrome coating
- introduce new Stop Pad Brackets.
There is no on aircraft work to be completed. This is an administrative Service Bulletin and must be reported to AIRBUS as accomplished for technical data configuration when VSB No. A33/34-32-305 is embodied.
The modification will be embodied at landing gear overhaul.
DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY As a technical pre-requisite to this Service B ulletin, embodiment of MESSIER BUGATTI DOWTY Service Bulletin No. A33/34-32-282 and AIRBUS Service Bulletin No. A340-32-4299 (Mod 204027H16671) is also required at, or before, Main Landing Gear (MLG) overhaul.
Accomplishment of this Service Bulletin will improve the corrosion resistance of the MLG Bogie Beam, and will also remove the requirement for repetitive under Stop Pad inspections mandated by AD2014-0120.
Accomplishment of this Service Bulletin cancels the requirements of Inspection Service Bulletin No.
A340-32-4286.
This Modification Service Bulletin affects the airworthiness limitations of Airworthiness Limitation Section (ALS) Part 1 which shall be introduced within the A/C maintenance program under the operator responsibility. Please download the relevant ALS Variation on Airbus World.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1)
CANCELS INSPECTION SB NO
POTENTIAL AD NO
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 NOTE
(1) : Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION No Material
EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :
06Y 22O 83V 98X ABD AFR AIB ALK ARG BOE CAL CCA CPA DLH FIN G8E GAF HFM IBE IRM LAN MAU MDG MHK PAL PUE
QAF SAA SAS SVW SWR THT THY UAE VIR XAX
CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletins:
Service Bulletin No. A340-32-4299 NOTE : Service Bulletin No. A340-32-4299 (LANDING GEAR - MAIN GEAR - INTRODUCE
INCREASED RECOIL SNUBBING FOR ENHANCE D MAIN LANDING GEAR EXTENSION) which applies Modification No. 204027H16671.
REFERENCES / REPERCUSSIONS TFU
32.11.14.007 OEB None DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY 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 Task 324300-839-895-001: Administrative
TOTAL MANHOURS
0.25
ELAPSED TIME (HOURS)
0.25
APPENDICES None DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
SUMMARY **CONF ALL
LH SHOWN
RH SIMILAR A A
AREA OF MODIFICATION NOTE:
F_SB_324300_7_SAAA_01_00 Figure A-U SAAA - S heet 01 DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 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 - INTRODUCE NICKEL UNDER CHROME
PATCH AND NEW BOGIESTOP PAD ON ENHANCED MLG BOGIE BEAM MODIFICATION No.: 204421H16719 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent.
1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE : This Service Bulletin is applicable to aircraft that are Post Mod.
No. 54500H15561 or Mod. No. 56214H15898 (Service Bulletin No.
A340-32-4256).
(1) Models 340-312 340-313
(2) Effectivity by MSN 0117 0123 0126 0128 0131 0135-0137 0139 0141-0142 0147 0149-0150 0152 0154 0157-0158 0160-0161 0163-0164 0166-0170 0173-0175 0179-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199 0201-0202 0207-0208 0210 0212-0218 0220-0221 0227-0228 0233 0236-0237 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 DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN 0651 0668 0793 0800 0835 0844 0921 0938 0955
(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 06Y 0139 0149 22O 0257 83V 0216 0280 0292 98X 0429 ABD 0210 AFR 0186 0207 0237 0245 0246 0260 0307 0310 0377 0399 AIB 0131 0141 0161 0182 0192 0199 ALK 0367 0374 0381 ARG 0123 0126 0128 0170 0193 0373 BOE 0554 CAL 0402 0406 0411 0415 0433 0541 CCA 0201 0242 0243 0264 CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 DLH 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447 FIN 0168 0174 0835 0844 0921 0938 G8E 0173 0187 0196 GAF 0274 0355 HFM 0117 0190 0202 IBE 0217 0221 0329 0483 IRM 0282 LAN 0359 0363 0442 MAU 0152 0194 0268 0793 0800 MDG 0319 MHK 0164 PAL 0302 0318 0332 0387 0459 0474 PUE 0212 0215 QAF 0528 SAA 0197 0378 0544 0582 0590 0643 0646 0651 SAS 0167 0413 0424 0430 0435 0450 0467 0470 SVW 0955 SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0562 0585 0598 THT 0385 0395 0438 0446 0668 THY 0180 0270 0331 UAE 0163 0166 0185 0236 VIR 0214 XAX 0273 0278 DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
(4) Configuration by MSN MSN
CONFIGURATION 0117 0123 0126 0128 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 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214 0215 0216 0217 0218 0220 0221 0227 0228 0233 0236 0237 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 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 0793 0800 0835 0844 0921 0938 0955 001
(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration.
(6) Material Effectivity No Material Set B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletins:
Service Bulletin No. A340-32-4299 NOTE : Service Bulletin No. A340-32-4299 (LANDING GEAR - MAIN GEAR
- INTRODUCE INCR EASED RECOIL SNUBBING FOR ENHANCED MAIN LANDING GEAR EXTENSION) which applies Modification No.
204027H16671.
C. REASON
(1) History This Service Bulletin is to introduce the application of Nickel under Chrome to improve the protection to the surface of the Bogie Beam under the area of the Stop Pad.
(2) Objective/Action This Service Bulletin is published to advise operators of A340 aircraft of the issue of MESSIER BUGATTI DOWTY Service Bulle tin No. A33/34-32-305, which introduces procedures to:
DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
- install a Nickel under Chrome coating to improve the protective treatments under the Bogie Beam Stop Pad
- install a new Bogie Beam Stop Pad which will have a reduced thickness to allow for the new Nickel under Chrome coating
- introduce new Stop Pad Brackets.
There is no on aircraft work to be completed. This is an administrative Service Bulletin and must be reported to AIRBUS as accomplished for technical data configuration when VSB No. A33/34-32-305 is embodied.
The modification will be embodied at landing gear overhaul.
As a technical pre-requisite to this Servic e Bulletin, embodim ent of MESSIER BUGATTI DOWTY Service Bulletin No. A33/34-32-282 and AIRBUS Service Bulletin No.
A340-32-4299 (Mod 204027H16671) is also required at, or before, Main Landing Gear (MLG) overhaul.
(3) Advantages Accomplishment of this Service Bulletin will improve the corrosion resistance of the MLG Bogie Beam, and will also remove the requirement for repetitive under Stop Pad inspections mandated by AD2014-0120.
Accomplishment of this Service Bulletin cancels the requirements of Inspection Service Bulletin No. A340-32-4286.
(4) Operational/Maintenance Consequences This Modification Service Bulletin affects the airworthiness limitations of Airworthiness Limitation Section (ALS) Part 1 which shall be introduced within the A/C maintenance program under the operator responsibility. Please download the relevant ALS Variation on Airbus World.
D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
Task 324300-839-895-001: Administrative
(1) Update the Aircraft Records E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
(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.
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.
Task 324300-839-895-001: Administrative On Aircraft Update the Aircraft Records
0.25
TOTAL MANHOURS
0.25
ELAPSED TIME (HOURS)
0.25 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES None K. PUBLICATION AFFECTED Aircraft Maintenance Manual (AMM) 32-11-00 32-11-14 Illustrated Parts Catalog (IPC) 32-11-14 L. INTERCHANGEABILITY/MIXABILITY
DESCRIPTION (OLD P/N)
OLD P/N
DESCRIPTION (NEW P/N)
NEW P/N INT
MIXABILITY DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 5 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN Bogie Beam and Dressing 10-211501-XXX
(1) Bogie Beam and Dressing 10-211501-XXX
(1) 01 Yes (2) NOTE : For definitions of interchangeability codes in column INT, refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.
NOTE : (1): XXX Denotes the last three digits of any Bogie and Dressings P/N beginning with 10-211501. Old PN does not have Strike No. 4 cancelled. New PN has Strike No. 4 cancelled.
NOTE : (2): It is acceptable to have mixed fitment of pre mod and post mod bogie beams on LH and RH MLG without detriment to landing gear performance;
however Operators should be made aware of the fact that an aircraft will only comply with Airworthiness Directive 2014-0120, and inspections may be terminated once both MLG have been modified to this (H16719) standard.
M. SPARES None DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 6 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY No Material Set B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin.
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit management department.
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX France T e l:( 3 3 )56 71 90 62 2 E-mail : monitored.retrofit@airbus.com F a x:( 3 3 )56 19 32 74 5 C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 7 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340
SERVICE BULLETIN This Page Intentionally Left Blank DATE: Apr 20/15 SERVICE BULLETIN No.: A340-32-4300 REVISION No.: 00 - Apr 20/15 Page: 8 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.