# Airbus Service Bulletin A330-32-3275

Copy: No revision named ("SB A330-32-3275"), 22 pages: PDF https://openairdocs.org/files/sha256/49/46/494677a618a8e3b92b302c3893ae2132df320037a47656b8fe3470f34eb1773c; text https://openairdocs.org/service-documents/airbus/a330-32-3275/file/494677a618a8.md. Rights: © 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.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-32-3275
- Page: https://openairdocs.org/service-documents/airbus/a330-32-3275

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2017-14-01](https://openairdocs.org/ad/2017-14-01.md), effective Aug 10, 2017: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-32-3275/proposed.md).

## Text (22 pages)

Rights: © 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. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A330
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 & NEW STOP PAD FOR BASIC & GROWTH MLG BOGIE BEAM
(SB ONLY)
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 205289H16720
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 A330 aircra ft of the issue of MESSIER
BUGATTI DOWTY Service Bulletin No. A33/34-32-306, 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 a new Stop Pad Bracket.
There is no on aircraft work to be completed. This is an administrative Service Bulletin and must
be reported to AIRBUS as accomp lished for technical data confi guration when MESSIER BUGATTI
DOWTY VSB No. A33/34-32-306 is embodied.
The modification will be embodied at landing gear overhaul.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A330
SERVICE BULLETIN
SUMMARY
As a technical prerequisite to this Service Bulle tin, embodiment of MESSIER BUGATTI DOWTY Service
Bulletin Nos. A33/34-32-307 or A33/34-32-308 and AIRBUS Service Bulletin No. A330-32-3276
(Modification No. 205290H16721) is also required at, or before, Main Landing Gear (MLG) overhaul.
NOTE
: The requirements of VSB No. A33/34-32-306 require that when the VSB is embodied at
overhaul VSB No. A33/34-32-284 is also accomplished to introduce the latest standard
paint scheme to the Bogie Beam bore.
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 AD
2014-0120 (Service Bulletin No. A330-32-3248).
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
 YES
POTENTIAL AD
 NO
 A/C OPERATION AFFECTED
 NO
RELIABILITY AFFECTED
 NO
 PAX COMFORT AFFECTED
 NO
COST SAVING
 NO
 ETOPS 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) :
38W 87Z AAR ABD ACA ACI AEA AFR AIB ALK ARG AZA AZU
BEL BER BGH CAL CES CPA CRL CSA CSN DAH DAL DGA DLH
EDW EIN ETD EVA EZX F2I FWI GFA GIA GRL HDA HFY HVN
KAL KLM MAS MLM MON MSR OHY PAL QAF QFA QTR RSY SAI
SAS SXD TAE TAM TAP TCX THA THY TSC UAE USA VKG WRC
XAX XLF
CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the
following Service Bulletins:
Service Bulletin No. A330-32-3276
NOTE
: Service Bulletin No. A330-32-3276 LANDING GEAR - MAIN GEAR - REVISE RECOIL
DAMPING FOR BASIC AND GROWTH MAIN LANDING GEAR EXTENSION (SB
ONLY) which applies Modification No. 205290H16721.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
SUMMARY
REFERENCES / REPERCUSSIONS
TFU
 32.11.14.009
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
OBRM
 NO
MANPOWER
**CONF 001
Task 323275-839-895-001: Administrative
TOTAL MANHOURS
 0.25
ELAPSED TIME (HOURS)
 0.25
**CONF 002
Task 323275-839-895-001: Administrative
TOTAL MANHOURS
 0.25
ELAPSED TIME (HOURS)
 0.25
APPENDICES
**CONF ALL
None
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
LH SHOWN
RH SIMILAR
A
A
AREA OF MODIFICATION
NOTE:
G_SB_323275_7_SAAA_01_00
Figure A-U SAAA - S heet 01
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 4
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A330
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 & NEW STOP PAD FOR BASIC & GROWTH MLG BOGIE BEAM
(SB ONLY)
MODIFICATION No.: 205289H16720
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 modification is applicable by Service Bulletin only.
NOTE
: This Service Bulletin is applicable to aircraft that have Basic MLG and Growth
MLG only.
(1) Models
330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321
330-322 330-323 330-341 330-342 330-343
(2) Effectivity by MSN
0012 0017 0030 0037 0042 0045 0050 0054-0055 0060 0062 0064-0065 0070-0072
0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116 0118
0120-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172
0177 0181 0195 0198 0200 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234
0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269
0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303
0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A330
SERVICE BULLETIN
0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370
0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401
0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441
0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473
0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513
0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539
0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576
0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607
0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638
0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676
0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705
0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0734 0737
0739 0741 0743 0745-0746 0749 0752 0755 0760
(3) Effectivity by Operator
The Operator/MSN relationship is provided for information only and is correct at the time
of issue in accordance with the information available to AIRBUS. Any future changes
resulting from transfer of an aircraft from one operator to another will not be reflected in
this list unless the Service Bulletin is revised for another reason.
OPERATOR
 MSN
38W
 0401
87Z
 0535
AAR
 0640 0676 0708
ABD
 0343
ACA
 0277 0279 0284 0344 0400 0408 0412 0419
ACI
 0507 0510
AEA
 0461 0505 0526 0551 0597 0670 0733 0745 0749
AFR
 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519
0567 0584 0657
AIB
 0042 0437
ALK
 0303 0306 0311 0313 0404 0456 0627
ARG
 0290 0300 0358 0364
AZA
 0272 0339
AZU
 0365 0372 0462 0494 0527 0529 0532
BEL
 0030 0037 0045 0082 0095 0229 0249 0324
BER
 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 0739
BGH
 0255
CAL
 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752
CES
 0713 0720 0728 0732
CPA
 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539
0548 0565 0679
CRL
 0285 0320
CSA
 0425
CSN
 0649 0652 0656 0664
DAH
 0644 0647 0650 0653 0667
DAL
 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620
0621 0631 0633 0663 0674 0690 0718 0722
DGA
 0240
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@A330
SERVICE BULLETIN
OPERATOR
 MSN
DLH
 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701
EDW
 0291
EIN
 0269 0330 0397
ETD
 0658 0688 0717 0724 0729 0730 0737
EVA
 0555 0573 0587 0634 0655 0661 0678 0693 0755
EZX
 0261
F2I
 0200
FWI
 0253
GFA
 0276 0281 0286 0287 0334 0340
GIA
 0138 0140 0144 0148 0153 0165
GRL
 0230
HDA
 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405
0479 0512 0581 0669 0673
HFY
 0096 0127 0211 0262
HVN
 0275 0294 0299 0366
KAL
 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350
0351 0368 0428 0484 0490 0550
KLM
 0682 0686 0703
MAS
 0116
MLM
 0451
MON
 0265
MSR
 0600 0610 0666 0683 0696 0709 0726
OHY
 0072 0087 0098 0143 0345 0353 0362 0625 0632
PAL
 0198
QAF
 0487 0605
QFA
 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695
0705 0712
QTR
 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659
0680 0711 0721 0734 0743 0746 0760
RSY
 0120 0171
SAI
 0055 0070 0086
SAS
 0496 0497 0515 0568
SXD
 0530 0684
TAE
 0348
TAM
 0232 0238 0247 0259 0361 0466 0472 0700
TAP
 0181 0195 0223 0305 0308 0312 0317 0477 0486
TCX
 0254 0266 0301 0398
THA
 0050 0060 0062 0064 0065 0112 0122 0209 0224 0231 0346
THY
 0463 0504 0697 0704
TSC
 0111 0132 0177 0250 0271 0369 0407 0427 0480
UAE
 0248 0251 0283 0293 0295 0314 0316 0326 0328 0382 0384 0392
0396 0409 0452 0455 0491 0509 0518 0525 0536
USA
 0315 0323 0333 0337 0342 0370 0375 0380 0388
VKG
 0309 0349 0356 0357
WRC
 0296
XAX
 0054 0654 0662 0692 0716 0741
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A330
SERVICE BULLETIN
OPERATOR
 MSN
XLF
 0501 0635
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0042 0045 0050 0054 0055 0060 0062
0064 0065 0070 0071 0072 0082 0083 0086 0087 0095 0096
0098 0099 0102 0106 0109 0111 0112 0113 0116 0118 0120
0121 0122 0127 0132 0138 0140 0143 0144 0148 0153 0155
0162 0165 0171 0172 0177 0198 0200 0206 0209 0219 0224
0231 0234 0241 0244
001
0181 0195 0211 0222 0223 0226 0229 0230 0232 0238 0240
0247 0248 0249 0250 0251 0253 0254 0255 0256 0258 0259
0261 0262 0265 0266 0267 0269 0271 0272 0275 0276 0277
0279 0281 0283 0284 0285 0286 0287 0288 0290 0291 0293
0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309
0311 0312 0313 0314 0315 0316 0317 0320 0322 0323 0324
0326 0328 0330 0333 0334 0337 0338 0339 0340 0342 0343
0344 0345 0346 0348 0349 0350 0351 0353 0356 0357 0358
0361 0362 0364 0365 0366 0368 0369 0370 0372 0375 0380
0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400
0401 0403 0404 0405 0407 0408 0409 0412 0418 0419 0420
0421 0422 0423 0425 0427 0428 0432 0437 0439 0441 0443
0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463
0465 0466 0469 0472 0473 0476 0477 0479 0480 0481 0484
0486 0487 0489 0490 0491 0493 0494 0496 0497 0498 0500
0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511
0512 0513 0515 0516 0518 0519 0521 0522 0524 0525 0526
0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549
0550 0551 0552 0553 0555 0558 0564 0565 0567 0568 0570
0571 0573 0574 0576 0578 0579 0581 0584 0587 0588 0591
0593 0595 0597 0600 0602 0603 0605 0607 0609 0610 0612
0614 0616 0618 0620 0621 0623 0625 0627 0629 0631 0632
0633 0634 0635 0636 0637 0638 0640 0641 0642 0644 0645
0647 0648 0649 0650 0652 0653 0654 0655 0656 0657 0658
0659 0661 0662 0663 0664 0665 0666 0667 0669 0670 0671
0673 0674 0675 0676 0678 0679 0680 0682 0683 0684 0686
0687 0688 0690 0691 0692 0693 0695 0696 0697 0699 0700
0701 0703 0704 0705 0707 0708 0709 0711 0712 0713 0714
0716 0717 0718 0720 0721 0722 0724 0725 0726 0728 0729
0730 0732 0733 0734 0737 0739 0741 0743 0745 0746 0749
0752 0755 0760
002
(5) Configuration definition
**CONF 001
Config. 001 is valid for the aircraft given in the effectivity of this Service Bulletin that
have not embodied Modification No. 43029H13154.
**CONF 002
Config. 002 is valid for the aircraft given in the effectivity of this Service Bulletin that
have embodied Modification No. 43029H13154.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 4
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A330
SERVICE BULLETIN
(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. A330-32-3276
NOTE
: Service Bulletin No. A330-32-3276 LANDING GEAR - MAIN GEAR - REVISE
RECOIL DAMPING FOR BASIC AND GROWTH MAIN LANDING GEAR
EXTENSION (SB ONLY) which applies Modification No. 205290H16721.
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 A330 aircraft of the issue
of MESSIER BUGATTI DOWTY Service Bulle tin No. A33/34-32-306, 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 a new Stop Pad Bracket.
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
MESSIER BUGATTI DOWTY VSB No. A33/34-32-306 is embodied.
The modification will be embodied at landing gear overhaul.
As a technical prerequisite to this Servic e Bulletin, embodim ent of MESSIER BUGATTI
DOWTY Service Bulletin Nos. A33/34-32-307 or A33/34-32-308 and AIRBUS Service
Bulletin No. A330-32-3276 (Modification No. 205290H16721) is also required at, or
before, Main Landing Gear (MLG) overhaul.
NOTE
: The requirements of VSB No. A33/34-32-306 require that when the VSB
is embodied at overhaul VSB No. A33/34-32-284 is also accomplished to
introduce the latest standard paint scheme to the Bogie Beam bore.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 5
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A330
SERVICE BULLETIN
(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 AD 2014-0120 (Service Bulletin No. A330-32-3248).
(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 :
**CONF 001
Task 323275-839-895-001: Administrative
(1) Update the Aircraft Records
**CONF 002
Task 323275-839-895-001: Administrative
(1) Update the Aircraft Records
**CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
This Service Bulletin must be embodied before the MLG exceeds 2500 landings or 24
months, whichever occurs first, since its first flight on an aeroplane or since its first flight
after the last overhaul.
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. It is anticipated that the AD will confirm the thresholds
given but reference should be made to the AD for confirmation of the mandated
accomplishment timescale.
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organisation Approv al No. EASA. 21J.031.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 6
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A330
SERVICE BULLETIN
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 323275-839-895-001: Administrative
On Aircraft
Update the Aircraft Records
 0.25
TOTAL MANHOURS
 0.25
ELAPSED TIME (HOURS)
 0.25
**CONF 002
Task 323275-839-895-001: Administrative
On Aircraft
Update the Aircraft Records
 0.25
TOTAL MANHOURS
 0.25
ELAPSED TIME (HOURS)
 0.25
**CONF ALL
H. WEIGHT AND BALANCE
Not Changed
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Maintenance Planning Document (MPD)
 321100-01-1
Vendor Service B ulletin (VSB)
 MESSIER BUGATTI DOWTY
A33/34-32-306
**CONF 002
Maintenance Planning Document (MPD)
 321100-01-1
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 7
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A330
SERVICE BULLETIN
Vendor Service B ulletin (VSB)
 MESSIER BUGATTI DOWTY
A33/34-32-306
**CONF ALL
K. PUBLICATION AFFECTED
Airworthiness Limitation Section (ALS)
 Part 1
Illustrated Parts Catalog (IPC)
 32-11-14
L. INTERCHANGEABILITY/MIXABILITY
**CONF 001
DESCRIPTION
(OLD P/N)
OLD P/N
 DESCRIPTION
(NEW P/N)
NEW P/N
 INT
 MIXABILITY
Bogie Beam
and Dressing
201274001-
XXX (1)
Bogie Beam
and Dressing
201274001-
XXX (1)
01
 YES
Bogie Beam
and Dressing
201274002-
XXX (1)
Bogie Beam
and Dressing
201274002-
XXX (1)
01
 YES
Bogie Beam
and Dressing
201274003-
XXX (1)
Bogie Beam
and Dressing
201274003-
XXX (1)
01
 YES
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 PN
beginning with 201274. Old PN does not have Strike No. 26 cancelled. New
PN has Strike No. 26 cancelled.
NOTE
: 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 AD 2014-0120
inspection will still be applicable to aircraft with mixed fitment configuration,
and inspections may be terminated once both MLG have been modified to this
(205289H16720) standard.
**CONF 002
DESCRIPTION
(OLD P/N)
OLD P/N
 DESCRIPTION
(NEW P/N)
NEW P/N
 INT
 MIXABILITY
Bogie Beam
and Dressing
201486001-
XXX (1)
Bogie Beam
and Dressing
201486001-
XXX (1)
01
 YES
Bogie Beam
and Dressing
201486002-
XXX (1)
Bogie Beam
and Dressing
201486002-
XXX (1)
01
 YES
Bogie Beam
and Dressing
201486003-
XXX (1)
Bogie Beam
and Dressing
201486003-
XXX (1)
01
 YES
Bogie Beam
and Dressing
201486004-
XXX (1)
Bogie Beam
and Dressing
201486004-
XXX (1)
01
 YES
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 8
7
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@A330
SERVICE BULLETIN
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: (1): XXX Denotes the last three digits of any Bogie and Dressings PN
beginning with 201486. Old PN does not have Strike No. 26 cancelled. New
PN has Strike No. 26 cancelled.
NOTE
: 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 AD 2014-0120
inspection will still be applicable to aircraft with mixed fitment configuration,
and inspections may be terminated once both MLG have been modified to this
(205289H16720) standard.
**CONF ALL
M. SPARES
None
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 9
7
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### Page 14

@A330
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 10
7
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### Page 15

@A330
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: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 11
7
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### Page 16

@A330
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 12
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 17

@A330
SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 323275-839-895-001 - Administrative
Task Associated Data
**CONF 001
Manpower
TOTAL MANHOURS
 0.25
ELAPSED TIME (HOURS)
 0.25
**CONF 002
Manpower
TOTAL MANHOURS
 0.25
ELAPSED TIME (HOURS)
 0.25
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 323275-839-401-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have accomplished this Service Bulletin.
**CONF 002
(1) Subtask 323275-839-401-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have accomplished this Service Bulletin.
**CONF ALL
B. PREPARATION
**CONF 001
(1) Subtask 323275-941-401-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 13
7
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### Page 18

@A330
SERVICE BULLETIN
References
Maintenance Planning Document (MPD)
 321100-01-1
(a) This Service Bulletin being accomplished in the frame of MLG overhaul,
Preparation steps are already covered by MPD 321100-01-1. No additional
preparation is necessary for SB accomplishment.
**CONF 002
(1) Subtask 323275-941-401-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Maintenance Planning Document (MPD)
 321100-01-1
(a) This Service Bulletin being accomplished in the frame of MLG overhaul,
Preparation steps are already covered by MPD 321100-01-1. No additional
preparation is necessary for SB accomplishment.
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 323275-839-402-001 - Update the Aircraft Records
Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 NON SPECIFIC
References
Vendor Service B ulletin (VSB)
 MESSIER BUGATTI DOWTY
A33/34-32-306
(a) Update your aircraft records to show accomplishment of this Service Bulletin in
accordance wit h MESSIER BUGATTI DOWTY Service Bulletin No. A33/34-32-306.
(b) Complete the Service Bulletin Reporting Sheet and return to AIRBUS.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 14
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 19

@A330
SERVICE BULLETIN
**CONF 002
(1) Subtask 323275-839-402-001 - Update the Aircraft Records
Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 NON SPECIFIC
References
Vendor Service B ulletin (VSB)
 MESSIER BUGATTI DOWTY
A33/34-32-306
(a) Update your aircraft records to show accomplishment of this Service Bulletin in
accordance wit h MESSIER BUGATTI DOWTY Service Bulletin No. A33/34-32-306.
(b) Complete the Service Bulletin Reporting Sheet and return to AIRBUS.
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 323275-700-401-001 - Test
Manpower Resources
Skills
 NON SPECIFIC
References
Maintenance Planning Document (MPD)
 321100-01-1
(a) This Service Bulletin being accomplished in the frame of MLG overhaul, Test steps
are already covered by MPD 321100-01-1. No additional Tests are necessary for
SB accomplishment.
**CONF 002
(1) Subtask 323275-700-401-001 - Test
Manpower Resources
Skills
 NON SPECIFIC
References
Maintenance Planning Document (MPD)
 321100-01-1
(a) This Service Bulletin being accomplished in the frame of MLG overhaul, Test steps
are already covered by MPD 321100-01-1. No additional Tests are necessary for
SB accomplishment.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 15
7
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### Page 20

@A330
SERVICE BULLETIN
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 323275-942-401-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Maintenance Planning Document (MPD)
 321100-01-1
(a) This Service Bulletin being accomplished in the frame of MLG overhaul, Close-up
steps are already covered by MPD 321100-01-1. No additional work is necessary
for SB accomplishment.
**CONF 002
(1) Subtask 323275-942-401-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Maintenance Planning Document (MPD)
 321100-01-1
(a) This Service Bulletin being accomplished in the frame of MLG overhaul, Close-up
steps are already covered by MPD 321100-01-1. No additional work is necessary
for SB accomplishment.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 16
7
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### Page 21

@A330
SERVICE BULLETIN
REPORTING SHEET
TITLE: LANDING GEAR-MAIN GEAR- INTRODUCE NICKEL UNDER CHROME
PATCH & NEW STOP PAD FOR BASIC & GROWTH MLG BOGIE BEAM
(SB ONLY)
MODIFICATION No.: 205289H16720
Please complete the appropriate item (A or B):
A - SB WILL BE
 embodied YES/NO (if NO please comment)
If YES, aircraft concer ned (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
F A X :( + 3 3 )56 19 32 80 6
e-mail: sb.reporting@airbus.com
or via your Resident Customer Support Office.
Alternatively, SB lists via letters or fax are also accepted.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 22

@A330
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
F A X:( 3 3 )56 19 34 25 1
Or via your Resident Customer Support Office.
DATE: Dec 23/15 SERVICE BULLETIN No.: A330-32-3275
REVISION No.: 00 - Dec 23/15 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

---
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