# Airbus Service Bulletin A330-27-3223

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## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-27-3223
- Page: https://openairdocs.org/service-documents/airbus/a330-27-3223

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

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

- [AD 2018-21-07](https://openairdocs.org/ad/2018-21-07.md), effective Nov 19, 2018: No revision named

## Text (59 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0498; AD 2018-21-07 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: 27
TITLE: FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY COMPUTER (FCPC)
- INSTALL NEW FCPC M25-2K0 OR P16M25-2K1
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 206412S33844
 206413S33845
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
A new Standard (STD) of Flight Control Primary Computer (FCPC) has been developed to improve
Angle Of Attack (AOA) monitoring.
This Service Bulletin replaces FCPC STDs M23-2K0 and P14M23-2K1 with new FCPC STDs M25-2K0
and P16M25-2K1, respectively, and advises all operators of A330 aircraft of the issue of AIRBUS
OPERATIONS SAS Service Bulletin No. LA2K0-27-026 and AIRBUS OPERATIONS SAS Service
Bulletin No. LA2K1-27-018.
To accomplish this Service Bulletin, you have three possibilities, as FCPC upgrade can be done either:
- By replacement of the FCPCs on aircraft
- By replacement of associated On Board Replaceable Module (OBRM) set (composed of
Part Number (PN) LA2K01500AF0100 and PN LA2K01500AF0200 installed through MOD No.
203036S32366 or PN LA2K1A100DF0100 and PN LA2K1A100DF0200 installed through MOD No.
203034S32365) on aircraft
- By replacement or reprogramming OBRM as per AIRBUS OPERATIONS SAS Service Bulletin No.
LA2K0-27-026 or AIRBUS OPERATIONS SAS Service Bulletin No. LA2K1-27-018 on bench.
NOTE
: We remind operators that, as described in Operator Information Transmission (OIT)
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 1
5
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@A330
SERVICE BULLETIN
SUMMARY
No. 999.0020/16, a replacement campaign of FCPC hardware LA2K0 or LA2K1 (to
hardware LA2K2) is on-going. AIRBUS recommends that operators adhere to this
hardware modification campaign as early as possible.
Accomplishment of this Service Bulletin will improve AOA probe monitoring.
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
 ETOPS AFFECTED
 NO
STRUCTURAL LIFE EXTN
 NO
 VENDOR SB INVOLVED
 YES
NOTE
 (1)
: Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION
**CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEA01
 1
 See SB
 FCPCs
Equipment BFEA03
 1
 See SB
 OBRMs
**CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEA02
 1
 See SB
 FCPCs
Equipment BFEA04
 1
 See SB
 OBRMs
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
38W 56O 83V 96U 98W AAL ACA ACI AEA AFR ALD ALK ARG
AZA AZU BEL BER BGH CPA CRL CSA DGA EIN F2I FWI GFA
GIA GRL HDA HFY HVN JAV KAL MLM MOV OHY PLM QAF QFA
QTR RSY SAI SAS SXD TAE TAM TAP TCX THA THY TSC U6A
UAE VKG WRC XLF
CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the
following Service Bulletin:
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
SUMMARY
Service Bulletin No. A330-27-3207
NOTE
: Service Bulletin No. A330-27-3207 (FLIGHT CONTROLS - FLIGHT CONTROL
PRIMARY COMPUTER (FCPC) - INSTALL NEW FCPC M23-2K0 OR P14M23-2K1)
applies MOD No. 203034S32365 and MOD No. 203036S32366.
REFERENCES / REPERCUSSIONS
TFU
 34.11.00.011
OEB
 None
AOT
 None
SIL
 None
ISI
 00.00.00261
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 Operator Information Transmission (OIT) No. 999.0020/16
NATURE OF THE WORK
AIRCRAFT
 NO
EQUIPMENT
 YES
HARD
 YES
SOFT
 NO
OBRM
 YES
MANPOWER
**CONF 001
Task 273223-831-801-001: OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Task 273223-831-802-001: OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on Aircraft
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Task 273223-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours relat ed to Vendor SB; refer to:
Reprogram the OBRMs in accordance with VSB
LA2K1-27-018 on Bench
AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K1-27-018
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 3
5
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SERVICE BULLETIN
SUMMARY
**CONF 002
Task 273223-831-801-001: OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Task 273223-831-802-001: OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on Aircraft
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Task 273223-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours relat ed to Vendor SB; refer to:
Reprogram the OBRMs in accordance with VSB
LA2K0-27-026 on Bench
AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K0-27-026
APPENDICES
**CONF ALL
None
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 4
5
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@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
Z120
FR20
FR1
B
800VU
915VU
A
MODIFICATION OF THE FCPCB
A
2CE1
MODIFICATION OF THE FCPC
MODIFICATION OF THE FCPC
2CE2
2CE3
G_SB_273223_5_SAAA_01_00
Figure A-FSAAA - Sheet 01
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 5
5
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SERVICE BULLETIN
SUMMARY
This Page Intentionally Left Blank
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 6
5
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### Page 7

@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: 27
TITLE: FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY COMPUTER (FCPC)
- INSTALL NEW FCPC M25-2K0 OR P16M25-2K1
MODIFICATION No.: 206412S33844 206413S33845
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 only to aircraft fitted with the 2K0 or 2K1
FCPC standard.
NOTE
: These modifications are applicable by Service Bulletin only.
(1) Models
330-202 330-203 330-223 330-243 330-301 330-321 330-322 330-323
330-341 330-342 330-343
(2) Effectivity by MSN
0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 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 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 0295-0296 0300-0301 0303
0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334
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
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 1
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@A330
SERVICE BULLETIN
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 0525-0527 0529-0530 0532 0535-0536 0539 0548
0550-0551 0565 0567-0568 0581 0584 0597 0627 0635 0657
(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
56O
 0116 0127
83V
 0171
96U
 0396
98W
 0054
AAL
 0315 0323 0333 0337 0342 0370 0375 0380 0388
ACA
 0277 0279 0284 0344 0400 0408 0412 0419
ACI
 0507 0510
AEA
 0461 0505 0526 0551 0597
AFR
 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519
0567 0584 0657
ALD
 0326 0328 0392
ALK
 0303 0306 0311 0313 0456 0627
ARG
 0290 0300 0358 0364
AZA
 0272 0339
AZU
 0462 0494 0527 0529 0532
BEL
 0030 0037 0045 0082 0095 0229 0249 0291 0324
BER
 0288 0322 0403 0432 0444 0454 0469 0476 0493
BGH
 0255
CPA
 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539
0548 0565
CRL
 0285 0320
CSA
 0425
DGA
 0240
EIN
 0269 0330 0397
F2I
 0070 0072 0087 0200
FWI
 0253 0343
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
HFY
 0211 0262
HVN
 0275 0366
JAV
 0409
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 2
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@A330
SERVICE BULLETIN
OPERATOR
 MSN
KAL
 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350
0351 0368 0428 0484 0490 0550
MLM
 0451
MOV
 0535
OHY
 0098 0143 0316 0345 0353 0362 0404 0437
PLM
 0261 0265
QAF
 0487
QFA
 0506 0508 0513 0522
QTR
 0441 0473 0489 0511 0521
RSY
 0096 0120 0283 0295
SAI
 0055 0086
SAS
 0496 0497 0515 0568
SXD
 0530
TAE
 0348
TAM
 0232 0238 0247 0259 0361 0466 0472
TAP
 0181 0195 0223 0305 0308 0312 0317 0365 0372 0477 0486
TCX
 0254 0266 0301 0398
THA
 0050 0060 0062 0112 0122 0209 0231 0346
THY
 0463 0504
TSC
 0111 0132 0177 0248 0250 0251 0271 0314 0369 0407 0427 0455
0480 0518 0536
U6A
 0065 0224
UAE
 0293 0382 0384 0452 0491 0509 0525
VKG
 0309 0349 0356 0357
WRC
 0296
XLF
 0501 0635
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 3
5
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@A330
SERVICE BULLETIN
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 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 0181 0195 0200 0206 0209 0211 0219 0222
0223 0224 0226 0229 0230 0231 0232 0234 0238 0240 0241
0244 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 0295 0296 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 0525 0526 0527 0529
0530 0532 0535 0536 0539 0548 0550 0551 0565 0567 0568
0581 0584 0597 0627 0635 0657
001 002
(5) Configuration definition
**CONF 001
Config. 001 is valid for aircraft fitted with FCPC LA2K1A100DF0000 (MOD No.
203034S32365 is embodied).
**CONF 002
Config. 002 is valid for aircraft fitted with FCPC LA2K01500AF0000 (MOD No.
203036S32366 is embodied).
(6) Material Effectivity
**CONF 001
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEA01
 1
 (1)
Equipment BFEA03
 1
 (2)
Reidentified part set REIDA01
 1
 (3)
NOTE
 (1)
: Equipment BFEA01 is applicable for TASK 273223-831-801 001
OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft .
NOTE
 (2)
: Equipment BFEA03 is applicable for TASK 273223-831-802 001
OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on Aircraft .
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 4
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@A330
SERVICE BULLETIN
NOTE
 (3)
: Reidentified part set REIDA01 is applicable for TASK 273223-831-803
001 OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench .
**CONF 002
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEA02
 1
 (1)
Equipment BFEA04
 1
 (2)
Reidentified part set REIDA02
 1
 (3)
NOTE
 (1)
: Equipment BFEA02 is applicable for TASK 273223-831-801 001
OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft .
NOTE
 (2)
: Equipment BFEA04 is applicable for TASK 273223-831-802 001
OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on Aircraft .
NOTE
 (3)
: Reidentified part set REIDA02 is applicable for TASK 273223-831-803
001 OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench .
**CONF ALL
B. CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of
the following Service Bulletin:
Service Bulletin No. A330-27-3207
NOTE
: Service Bulletin No. A330-27-3207 (FLIGHT CONTROLS - FLIGHT
CONTROL PRIMARY COMPUTER (FCPC) - INSTALL NEW FCPC M23-2K0
OR P14M23-2K1) applies MOD No. 203034S32365 and MOD No.
203036S32366.
C. REASON
(1) History
A new Standard (STD) of Flight Control Primary Computer (FCPC) has been developed
to improve Angle Of Attack (AOA) monitoring.
(2) Objective/Action
This Service Bulletin replaces FCPC STDs M23-2K0 and P14M23-2K1 with new FCPC
STDs M25-2K0 and P16M25-2K1, respectively, and advises all operators of A330
aircraft of the issue of AIRBUS OPERATIONS SAS Service Bulletin No. LA2K0-27-026
and AIRBUS OPERATIONS SAS Service Bulletin No. LA2K1-27-018.
To accomplish this Service Bulletin, you have three possibilities, as FCPC upgrade can
be done either:
- By replacement of the FCPCs on aircraft
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 5
5
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SERVICE BULLETIN
- By replacement of associated On Board Replaceable Module (OBRM) set
(composed of Part Number (PN) LA2K01500AF0100 and PN LA2K01500AF0200
installed through MOD No. 203036S32366 or PN LA2K1A100DF0100 and PN
LA2K1A100DF0200 installed through MOD No. 203034S32365) on aircraft
- By replacement or reprogramming OBRM as per AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K0-27-026 or AIRBUS OPERATIONS SAS Service Bulletin
No. LA2K1-27-018 on bench.
NOTE
: We remind operators that, as described in Operator Information
Transmission (OIT) No. 999.0020/16, a replacement campaign of FCPC
hardware LA2K0 or LA2K1 (to hardware LA2K2) is on-going. AIRBUS
recommends that operators adhere to this hardware modification
campaign as early as possible.
(3) Advantages
Accomplishment of this Service Bulletin will improve AOA probe monitoring.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
NOTE
: To accomplish this Service Bulletin, you have three options.
To accomplish this Service Bulletin it is necessary to :
**CONF 001
Task 273223-831-801-001: OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft
(1) Replace the FCPCs (2CE1, 2CE2 and 2CE3)
Task 273223-831-802-001: OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on
Aircraft
(1) Replace the OBRMs
Task 273223-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench
(1) Remove the OBRMs
(2) Reprogram the OBRMs in accordance with VSB LA2K1-27-018 on Bench
(3) Install the OBRMs
**CONF 002
Task 273223-831-801-001: OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft
(1) Replace the FCPCs (2CE1, 2CE2 and 2CE3)
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 6
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SERVICE BULLETIN
Task 273223-831-802-001: OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on
Aircraft
(1) Replace the OBRMs
Task 273223-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench
(1) Remove the OBRMs
(2) Reprogram the OBRMs in accordance with VSB LA2K0-27-026 on Bench
(3) Install the OBRMs
**CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin must be done within 12 months from Service
Bulletin issuance date.
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 threshold
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 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.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 7
5
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SERVICE BULLETIN
**CONF 001
Task 273223-831-801-001: OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft
Get Access
 0.50
On Aircraft
Replace the FCPCs (2CE1, 2CE2 and 2CE3)
 1.00
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Task 273223-831-802-001: OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on Aircraft
Get Access
 0.50
On Aircraft
Replace the OBRMs
 0.50
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Task 273223-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench
Get Access
 0.50
On Aircraft
Remove the OBRMs
 0.25
Install the OBRMs
 0.25
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours relat ed to Vendor SB; refer to:
Reprogram the OBRMs in accordance with VSB
LA2K1-27-018 on Bench
AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K1-27-018
**CONF 002
Task 273223-831-801-001: OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft
Get Access
 0.50
On Aircraft
Replace the FCPCs (2CE1, 2CE2 and 2CE3)
 1.00
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 8
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Task 273223-831-802-001: OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on Aircraft
Get Access
 0.50
On Aircraft
Replace the OBRMs
 0.50
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Task 273223-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench
Get Access
 0.50
On Aircraft
Remove the OBRMs
 0.25
Install the OBRMs
 0.25
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours relat ed to Vendor SB; refer to:
Reprogram the OBRMs in accordance with VSB
LA2K0-27-026 on Bench
AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K0-27-026
**CONF ALL
H. WEIGHT AND BALANCE
Not Changed
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Aircraft Maintenance Manual (AMM)
 06-20-00 06-31-53 06-41-53
12-34-24 20-15-00 22-97-00
27-93-34 27-96-00
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Service Bulletin (SB)
 A330-27-3207
Vendor Service Bulletin (VSB)
 AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K1-27-018
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 9
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**CONF 002
Aircraft Maintenance Manual (AMM)
 06-20-00 06-31-53 06-41-53
12-34-24 20-15-00 22-97-00
27-93-34 27-96-00
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Service Bulletin (SB)
 A330-27-3207
Vendor Service Bulletin (VSB)
 AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K0-27-026
**CONF ALL
K. PUBLICATION AFFECTED
Aircraft Wiring List (AWL)
Illustrated Parts Catalog (IPC)
 27-93-08
L. INTERCHANGEABILITY/MIXABILITY
The interchangeability/mixability possibilities are for new or modified parts introduced by the
accomplishment of this Service Bulletin.
**CONF 001
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
FCPC
 LA2K1A100DF0000
 LA2K1A100DG0000
 03
 NO
 (1) (2)
OBRM1
 LA2K1A100DF0100
 LA2K1A100DG0100
 03
 NO
OBRM2
 LA2K1A100DF0200
 LA2K1A100DG0200
 03
 NO
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.
NOTE
 (1)
: Not interchangeable, but one-way interchangeable with conditions.
When the old PN is removed, it may be replaced:
- With the old PN
- With the new PN only if the complete set of old PN is replaced with a set
of new PN.
When the new PN is removed, it must be replaced with the new PN.
NOTE
 (2)
: On A330-300 with mechanical rudder (not having MOD No. 49144S16279
installed), the new PN LA2K1A100DG0000 is fully intermixable with FCPC
P15M24 PN LA2K2B100DH0000 (installed by MOD No. 206414S33846) and
FCPC M25 PN LA2K01500AG0000 (installed by MOD No. 206412S33844).
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 10
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On A330-200 with mechanical rudder (not having MOD No. 49144S16279
installed), the new PN LA2K1A100DG0000 is fully intermixable with FCPC
P15M24 PN LA2K2B100DH0000 (installed by MOD No. 206414S33846).
**CONF 002
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
FCPC
 LA2K01500AF0000
 LA2K01500AG0000
 03
 NO
 (1) (2)
OBRM1
 LA2K01500AF0100
 LA2K01500AG0100
 03
 NO
OBRM2
 LA2K01500AF0200
 LA2K01500AG0200
 03
 NO
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.
NOTE
 (1)
: Not interchangeable, but one-way interchangeable with conditions.
When the old PN is removed, it may be replaced:
- With the old PN
- With the new PN only if the complete set of old PN is replaced with a set
of new PN.
When the new PN is removed, it must be replaced with the new PN.
NOTE
 (2)
: On A330-300 with mechanical rudder (not having MOD No. 49144S16279
installed), the new PN LA2K01500AG0000 is fully intermixable with FCPC
P16M25 PN LA2K1A100DG0000 (installed by MOD No. 206413S33845)
and FCPC P15M24 PN LA2K2B100DH0000 (installed by MOD No.
206414S33846).
**CONF ALL
M. SPARES
FCPC LA2K01500AF0000
FCPC LA2K1A100DF0000
The parts listed here must not be installed anymore on aircraft which have accomplished this
Service Bulletin or which have the equivalent production modification embodied.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 11
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This Page Intentionally Left Blank
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 12
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SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Vendor parts are to be procured from:
Equipment BFEA01
Equipment BFEA02
Equipment BFEA03
Equipment BFEA04
AIRBUS OPERATIONS SAS
AVIONICS AND SIMULATION PRODUCTS
EYY - M8621 - 316, route de Bayonne
31060 TOULOUSE Cedex 09 - FRANCE
FAX: 33 (0)5 61 18 04 94
E-mail: systems.support@airbus.com
(2) Price and Availability
Equipment BFEA01
Procurement terms for the equipment must be negotiated with the equipment supplier.
Equipment BFEA02
Procurement terms for the equipment must be negotiated with the equipment supplier.
Equipment BFEA03
Procurement terms for the equipment must be negotiated with the equipment supplier.
Equipment BFEA04
Procurement terms for the equipment must be negotiated with the equipment supplier.
Reidentified part set REIDA01
Refer to the AIRBUS OPERATIONS SAS Service Bulletin No. LA2K1-27-018 for the
equipment modification sales terms.
Reidentified part set REIDA02
Refer to the AIRBUS OPERATIONS SAS Service Bulletin No. LA2K0-27-026 for the
equipment modification sales terms.
B. INDUSTRY SUPPORT INFORMATION
From Equipment BFEA01 to Equipment BFEA04, industry support terms for the equipment
must be negotiated with the equipment supplier.
For Reidentified part set REIDA01, modification of removed equipment should be negotiated
directly with AIRBUS OPERATIONS SAS as per instructions given in Service Bulletin No.
LA2K1-27-018.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 13
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SERVICE BULLETIN
Refer to the AIRBUS OPERATIONS SAS Service Bulletin No. LA2K1-27-018 for the industry
support terms of the Vendor Service Bulletin parts and labor.
For Reidentified part set REIDA02, modification of removed equipment should be negotiated
directly with AIRBUS OPERATIONS SAS as per instructions given in Service Bulletin No.
LA2K0-27-026.
Refer to the AIRBUS OPERATIONS SAS Service Bulletin No. LA2K0-27-026 for the industry
support terms of the Vendor Service Bulletin parts and labor.
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 BLANGNAC CEDEX
France
E-mail: monitored.retrofit@airbus.com
C. LIST OF COMPONENTS
No Kit
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
None
(2) Components
None
(3) Equipment
Equipment BFEA01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K1A100DG0000
 3
 FCPC
 LA2K1A100DF0000
 03
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 14
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Equipment BFEA02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K01500AG0000
 3
 FCPC
 LA2K01500AF0000
 03
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
Equipment BFEA03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K1A100DG0100
 3
 OBRM1
 LA2K1A100DF0100
 03
LA2K1A100DG0200
 3
 OBRM2
 LA2K1A100DF0200
 03
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
Equipment BFEA04
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K01500AG0100
 3
 OBRM1
 LA2K01500AF0100
 03
LA2K01500AG0200
 3
 OBRM2
 LA2K01500AF0200
 03
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
Reidentified part set REIDA01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K1A100DG0100
 OBRM1
 LA2K1A100DF0100
LA2K1A100DG0200
 OBRM2
 LA2K1A100DF0200
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K1-27-018.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 15
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Reidentified part set REIDA02
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K01500AG0100
 OBRM1
 LA2K01500AF0100
LA2K01500AG0200
 OBRM2
 LA2K01500AF0200
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K0-27-026.
F. TOOLING
(1) Tooling - Price and Availability
None
(2) Tools
NOTE
: To accomplish TASK 273223-831-803 001 OPTION 3 - Upgrade by
Reprogramming of FCPCs OBRMs in accordance with VSB on Bench of
this Service Bulletin, it is necessary to use the tools defined in AIRBUS
OPERATIONS SAS Service Bulletin No. LA2K1-27-018.
NOTE
: To accomplish TASK 273223-831-803 001 OPTION 3 - Upgrade by
Reprogramming of FCPCs OBRMs in accordance with VSB on Bench of
this Service Bulletin, it is necessary to use the tools defined in AIRBUS
OPERATIONS SAS Service Bulletin No. LA2K0-27-026.
(3) Special Tools
None
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 16
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3. ACCOMPLISHMENT INSTRUCTIONS
Task 273223-831-801-001 - OPTION 1 - Upgrade by Replacement of FCPCs on Aircraft
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.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has a procedure accepted by the local authority
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. Other paragraphs are recommended and may be deviated
from, done as part of other actions or done with accepted methods different from
those given in the Service Bulletin, as long as the RC paragraphs can be done and
the aircraft can be put back into a serviceable condition.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact AIRBUS for further
instructions and approval.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 17
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NOTE
: Discarded parts must be managed at the operator’s discretion.
Task Associated Data
**CONF 001
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
**CONF 002
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 273223-910-001-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 18
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(2) Subtask 273223-839-001-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF 002
(1) Subtask 273223-910-001-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.
(2) Subtask 273223-839-001-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
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 273223-941-001-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 19
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locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
**CONF 002
(1) Subtask 273223-941-001-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 20
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- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 273223-960-001-001 - Replace the FCPCs (2CE1, 2CE2 and 2CE3)
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 1.00
Minimum number of person
 1
Subtask elapsed time
 1.00
Skills
 ELECTRICAL
Material necessary to do the job
Equipment BFEA01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K1A100DG0000
 3
 FCPC
NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
(a) Remove the FCPCs (2CE1, 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-000-801
FIN 2CE1
1 FCPC LA2K1A100DF0000 Discard
and
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 21
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FIN 2CE2
1 FCPC LA2K1A100DF0000 Discard
and
FIN 2CE3
1 FCPC LA2K1A100DF0000 Discard
(b) Install the FCPCs (2CE1, 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-400-801
FIN 2CE1
1 FCPC LA2K1A100DG0000
and
FIN 2CE2
1 FCPC LA2K1A100DG0000
and
FIN 2CE3
1 FCPC LA2K1A100DG0000
**CONF 002
(1) Subtask 273223-960-001-002 - Replace the FCPCs (2CE1, 2CE2 and 2CE3)
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 1.00
Minimum number of person
 1
Subtask elapsed time
 1.00
Skills
 ELECTRICAL
Material necessary to do the job
Equipment BFEA02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K01500AG0000
 3
 FCPC
NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 22
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References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
(a) Remove the FCPCs (2CE1, 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-000-801
FIN 2CE1
1 FCPC LA2K01500AF0000 Discard
and
FIN 2CE2
1 FCPC LA2K01500AF0000 Discard
and
FIN 2CE3
1 FCPC LA2K01500AF0000 Discard
(b) Install the FCPCs (2CE1, 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-400-801
FIN 2CE1
1 FCPC LA2K01500AG0000
and
FIN 2CE2
1 FCPC LA2K01500AG0000
and
FIN 2CE3
1 FCPC LA2K01500AG0000
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 273223-700-001-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 23
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(a) Remove the safety clips and/or tags and close/unlock the circuit breakers as
specified after the installation of the FCPCs (2CE1, 2CE2 and 2CE3), refer to AMM
Task 27-93-34-400-801.
(b) Do the test procedure as specified after the installation of the FCPCs (2CE1, 2CE2
and 2CE3), refer to AMM Task 27-93-34-400-801.
**CONF 002
(1) Subtask 273223-700-001-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Remove the safety clips and/or tags and close/unlock the circuit breakers as
specified after the installation of the FCPCs (2CE1, 2CE2 and 2CE3), refer to AMM
Task 27-93-34-400-801.
(b) Do the test procedure as specified after the installation of the FCPCs (2CE1, 2CE2
and 2CE3), refer to AMM Task 27-93-34-400-801.
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 273223-942-001-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up as specified in the installation of the FCPCs (2CE1, 2CE2 and
2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
**CONF 002
(1) Subtask 273223-942-001-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 24
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References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up as specified in the installation of the FCPCs (2CE1, 2CE2 and
2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 25
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DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
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Task 273223-831-802-001 - OPTION 2 - Upgrade by Replacement of FCPCs OBRMs on
Aircraft
**CONF ALL
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.
CAUTION
: REFER TO AMM 20-15-00, Page Block 201 FOR ELECTROSTATIC
DISCHARGE PRECAUTIONS.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has a procedure accepted by the local authority
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. Other paragraphs are recommended and may be deviated
from, done as part of other actions or done with accepted methods different from
those given in the Service Bulletin, as long as the RC paragraphs can be done and
the aircraft can be put back into a serviceable condition.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 27
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necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact AIRBUS for further
instructions and approval.
NOTE
: Discarded parts must be managed at the operator’s discretion.
Task Associated Data
**CONF 001
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
**CONF 002
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 273223-910-002-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 28
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(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.
(2) Subtask 273223-839-002-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF 002
(1) Subtask 273223-910-002-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.
(2) Subtask 273223-839-002-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
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 273223-941-002-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 29
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NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
NOTE
: The circuit breakers will be managed in another SUBTASK
273223-960-002 001 Replace the OBRMs to allow the Built-In
Test Equipment (BITE) test of the Electrical Flight Control System
(EFCS).
**CONF 002
(1) Subtask 273223-941-002-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 30
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- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
NOTE
: The circuit breakers will be managed in another SUBTASK
273223-960-002 002 Replace the OBRMs to allow the Built-In
Test Equipment (BITE) test of the Electrical Flight Control System
(EFCS).
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 273223-960-002-001 - Replace the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 ELECTRICAL
Material necessary to do the job
Equipment BFEA03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K1A100DG0100
 3
 OBRM1
LA2K1A100DG0200
 3
 OBRM2
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 31
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NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-96-00-740-807
(a) Before replacement of the OBRMs:
1
 On the FLT CTL section of the overhead panel 241VU (212VU), make sure
that the PRIMary Computer (PRIM) 1, (PRIM 2), (PRIM 3) pushbutton
switch(es) is (are) pushed (the OFF and FAULT legends of this (these)
pushbutton switch(es) are off).
2
 Do the BITE test of the EFCS (Line Replaceable Unit (LRU) IDENT), refer to
AMM Task 27-96-00-740-807 and make sure that the old PN of the FCPCs
are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Open, safety/lock and tag the circuit breakers as specified in the removal of
the FCPCs (2CE1, 2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
(b) Remove the OBRMs from the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K1A100DF0100 Discard
and
3 OBRM2 LA2K1A100DF0200 Discard
NOTE
: Some OBRMs are located behind a flap on the equipment, open it if
necessary.
NOTE
: To remove the OBRM, unlock the two locks located at the lower
and upper extremities of the OBRM.
(c) Install the OBRMs on the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K1A100DG0100
and
3 OBRM2 LA2K1A100DG0200
NOTE
: Re-identification of the FCPCs from PN LA2K1A100DF0000 to PN
LA2K1A100DG0000 is automatically performed by replacement of
the OBRMs, nevertheless, the responsible quality inspector can put
his own sticker and his own control seal on the front face to confirm
the replacement of the OBRMs.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 32
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**CONF 002
(1) Subtask 273223-960-002-002 - Replace the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 ELECTRICAL
Material necessary to do the job
Equipment BFEA04
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K01500AG0100
 3
 OBRM1
LA2K01500AG0200
 3
 OBRM2
NOTE
: The above list of components is not an AIRBUS kit, the required parts
shall be ordered as necessary through the given channel.
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-96-00-740-807
(a) Before replacement of the OBRMs:
1
 On the FLT CTL section of the overhead panel 241VU (212VU), make sure
that the PRIM 1, (PRIM 2), (PRIM 3) pushbutton switch(es) is (are) pushed
(the OFF and FAULT legends of this (these) pushbutton switch(es) are off).
2
 Do the BITE test of the EFCS (Line Replaceable Unit (LRU) IDENT), refer to
AMM Task 27-96-00-740-807 and make sure that the old PN of the FCPCs
are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Open, safety/lock and tag the circuit breakers as specified in the removal of
the FCPCs (2CE1, 2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
(b) Remove the OBRMs from the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K01500AF0100 Discard
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 33
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and
3 OBRM2 LA2K01500AF0200 Discard
NOTE
: Some OBRMs are located behind a flap on the equipment, open it if
necessary.
NOTE
: To remove the OBRM, unlock the two locks located at the lower
and upper extremities of the OBRM.
(c) Install the OBRMs on the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K01500AG0100
and
3 OBRM2 LA2K01500AG0200
NOTE
: Re-identification of the FCPCs from PN LA2K1A100DF0000 to PN
LA2K1A100DG0000 is automatically performed by replacement of
the OBRMs, nevertheless, the responsible quality inspector can put
his own sticker and his own control seal on the front face to confirm
the replacement of the OBRMs.
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 273223-700-002-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 22-97-00-740-801
Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-802
Task 27-96-00-740-807
(a) Job set-up
1
 Remove the safety clips and/or tags and close/unlock the circuit breakers as
specified in the installation of the FCPCs (2CE1, 2CE2 and 2CE3), refer to
AMM Task 27-93-34-400-801.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 34
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(b) Procedure:
1
 After power-up, on the FLT CTL section of the overhead panel 241VU
(212VU), make sure that the PRIM 1, (PRIM 2), (PRIM 3) pushbutton
switch(es) is (are) pushed (the OFF and FAULT legends of this (these)
pushbutton switch(es) are off).
If a FAULT is present, do a reset with the concerned pushbutton switch.
If FAULT persists, replace the concerned computer, refer to AMM Task
27-93-34-000-801 and AMM Task 27-93-34-400-801.
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the new PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Do the BITE test of the EFCS (SYSTEM TEST), refer to AMM Task
27-96-00-740-802.
4
 If the airline operates the aircraft in CAT III conditions, do the LAND CAT III
capability test, refer to AMM Task 22-97-00-740-801.
**CONF 002
(1) Subtask 273223-700-002-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 22-97-00-740-801
Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-802
Task 27-96-00-740-807
(a) Job set-up
1
 Remove the safety clips and/or tags and close/unlock the circuit breakers as
specified in the installation of the FCPCs (2CE1, 2CE2 and 2CE3), refer to
AMM Task 27-93-34-400-801.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 35
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(b) Procedure:
1
 After power-up, on the FLT CTL section of the overhead panel 241VU
(212VU), make sure that the PRIM 1, (PRIM 2), (PRIM 3) pushbutton
switch(es) is (are) pushed (the OFF and FAULT legends of this (these)
pushbutton switch(es) are off).
If a FAULT is present, do a reset with the concerned pushbutton switch.
If FAULT persists, replace the concerned computer, refer to AMM Task
27-93-34-000-801 and AMM Task 27-93-34-400-801.
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the new PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Do the BITE test of the EFCS (SYSTEM TEST), refer to AMM Task
27-96-00-740-802.
4
 If the airline operates the aircraft in CAT III conditions, do the LAND CAT III
capability test, refer to AMM Task 22-97-00-740-801.
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 273223-942-002-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up procedure as specified in the installation of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
**CONF 002
(1) Subtask 273223-942-002-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 36
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References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up procedure as specified in the installation of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 37
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This Page Intentionally Left Blank
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 38
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Task 273223-831-803-001 - OPTION 3 - Upgrade by Reprogramming of FCPCs OBRMs in
accordance with VSB on Bench
**CONF ALL
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.
CAUTION
: REFER TO AMM 20-15-00, Page Block 201 FOR ELECTROSTATIC
DISCHARGE PRECAUTIONS.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has a procedure accepted by the local authority
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. Other paragraphs are recommended and may be deviated
from, done as part of other actions or done with accepted methods different from
those given in the Service Bulletin, as long as the RC paragraphs can be done and
the aircraft can be put back into a serviceable condition.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 39
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necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact AIRBUS for further
instructions and approval.
Task Associated Data
**CONF 001
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours related to Vendor SB; refer to:
AIRBUS OPERATIONS SAS Service Bulletin No. LA2K1-27-018
**CONF 002
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours related to Vendor SB; refer to:
AIRBUS OPERATIONS SAS Service Bulletin No. LA2K0-27-026
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 273223-910-003-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 40
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References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) Tag all the parts you must remove and retain to make the subsequent installation
easier.
(d) Put all the retained hardware in identified plastic bags and attach the bags to the
related unit.
(2) Subtask 273223-839-003-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF 002
(1) Subtask 273223-910-003-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) Tag all the parts you must remove and retain to make the subsequent installation
easier.
(d) Put all the retained hardware in identified plastic bags and attach the bags to the
related unit.
(2) Subtask 273223-839-003-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 41
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**CONF ALL
B. PREPARATION
**CONF 001
(1) Subtask 273223-941-003-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
NOTE
: The circuit breakers will be managed in another SUBTASK
273223-020-001 001 Remove the OBRMs to allow the BITE of the
EFCS.
**CONF 002
(1) Subtask 273223-941-003-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 42
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SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
NOTE
: The circuit breakers will be managed in another SUBTASK
273223-020-001 002 Remove the OBRMs to allow the BITE of the
EFCS.
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 273223-020-001-001 - Remove the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 43
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Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 ELECTRICAL
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-96-00-740-807
(a) Before reprogramming of the OBRMs:
1
 On the FLT CTL section of the overhead panel 241VU (212VU), make sure
that the PRIM 1, (PRIM 2), (PRIM 3) pushbutton switch(es) is (are) pushed
(the OFF and FAULT legends of this (these) pushbutton switch(es) are off).
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the old PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Open, safety/lock and tag the circuit breakers as specified in the removal of
the FCPCs (2CE1, 2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
(b) Remove the OBRMs from the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K1A100DF0100 Retain
and
3 OBRM2 LA2K1A100DF0200 Retain
NOTE
: Retained for modification.
NOTE
: Some OBRMs are located behind a flap on the equipment, open it if
necessary.
NOTE
: To remove the OBRM, unlock the two locks located at the lower
and upper extremities of the OBRM.
(2) Subtask 273223-831-001-001 - Reprogram the OBRMs in accordance with VSB
LA2K1-27-018 on Bench
Material necessary to do the job
Reidentified part set REIDA01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K1A100DG0100
 OBRM1
 LA2K1A100DF0100
LA2K1A100DG0200
 OBRM2
 LA2K1A100DF0200
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 44
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SERVICE BULLETIN
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K1-27-018.
References
Vendor Service Bulletin (VSB)
 AIRBUS OPERATIONS SAS LA2K1-27-018
(a) Reprogram and re-identify the OBRMs in accordance with AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K1-27-018.
(b) After the re-identification:
3 OBRM1 LA2K1A100DF0100
becomes
3 OBRM1 LA2K1A100DG0100
and
3 OBRM2 LA2K1A100DF0200
becomes
3 OBRM2 LA2K1A100DG0200
(3) Subtask 273223-420-001-001 - Install the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 ELECTRICAL
Material necessary to do the job
Reidentified part set REIDA01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K1A100DG0100
 OBRM1
LA2K1A100DG0200
 OBRM2
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K1-27-018.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 45
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(a) Install the OBRMs on the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K1A100DG0100
and
3 OBRM2 LA2K1A100DG0200
NOTE
: Re-identification of the FCPCs (2CE1, 2CE2 and 2CE3) from
PN LA2K1A100DF0000 to PN LA2K1A100DG0000 is automatically
performed by replacement of the OBRMs, nevertheless, the
responsible quality inspector can put his own sticker and his own
control seal on the front face to confirm the replacement of the
OBRMs.
**CONF 002
(1) Subtask 273223-020-001-002 - Remove the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 ELECTRICAL
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-96-00-740-807
(a) Before reprogramming of the OBRMs:
1
 On the FLT CTL section of the overhead panel 241VU (212VU), make sure
that the PRIM 1, (PRIM 2), (PRIM 3) pushbutton switch(es) is (are) pushed
(the OFF and FAULT legends of this (these) pushbutton switch(es) are off).
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the old PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Open, safety/lock and tag the circuit breakers as specified in the removal of
the FCPCs (2CE1, 2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 46
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(b) Remove the OBRMs from the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K01500AF0100 Retain
and
3 OBRM2 LA2K01500AF0200 Retain
NOTE
: Retained for modification.
NOTE
: Some OBRMs are located behind a flap on the equipment, open it if
necessary.
NOTE
: To remove the OBRM, unlock the two locks located at the lower
and upper extremities of the OBRM.
(2) Subtask 273223-831-001-002 - Reprogram the OBRMs in accordance with VSB
LA2K0-27-026 on Bench
Material necessary to do the job
Reidentified part set REIDA02
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K01500AG0100
 OBRM1
 LA2K01500AF0100
LA2K01500AG0200
 OBRM2
 LA2K01500AF0200
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K0-27-026.
References
Vendor Service Bulletin (VSB)
 AIRBUS OPERATIONS SAS LA2K0-27-026
(a) Reprogram and re-identify the OBRMs in accordance with AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K0-27-026.
(b) After the re-identification:
3 OBRM1 LA2K01500AF0100
becomes
3 OBRM1 LA2K01500AG0100
and
3 OBRM2 LA2K01500AF0200
becomes
3 OBRM2 LA2K01500AG0200
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 47
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(3) Subtask 273223-420-001-002 - Install the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 ELECTRICAL
Material necessary to do the job
Reidentified part set REIDA02
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K01500AG0100
 OBRM1
LA2K01500AG0200
 OBRM2
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K0-27-026.
(a) Install the OBRMs on the FCPCs (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K01500AG0100
and
3 OBRM2 LA2K01500AG0200
NOTE
: Re-identification of the FCPCs (2CE1, 2CE2 and 2CE3) from
PN LA2K01500AF0000 to PN LA2K01500AG0000 is automatically
performed by replacement of the OBRMs, nevertheless, the
responsible quality inspector can put his own sticker and his own
control seal on the front face to confirm the replacement of the
OBRMs.
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 273223-700-003-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 48
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SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 Task 22-97-00-740-801
Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-802
Task 27-96-00-740-807
(a) Job set-up:
1
 Remove the safety clips and/or tags and close/unlock the circuit breakers as
specified in the installation of the FCPCs (2CE1, 2CE2 and 2CE3), refer to
AMM Task 27-93-34-400-801.
(b) Procedure:
1
 After power-up, on the FLT CTL section of the overhead panel 241VU
(212VU), make sure that the PRIM 1, (PRIM 2), (PRIM 3) pushbutton
switch(es) is (are) pushed (the OFF and FAULT legends of this (these)
pushbutton switch(es) are off).
If a FAULT is present, do a reset with the concerned pushbutton switch.
If FAULT persists, replace the concerned computer, refer to AMM Task
27-93-34-000-801 and AMM Task 27-93-34-400-801.
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the new PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Do the BITE test of the EFCS (SYSTEM TEST), refer to AMM Task
27-96-00-740-802.
4
 If the airline operates the aircraft in CAT III conditions, do the LAND CAT III
capability test, refer to AMM Task 22-97-00-740-801.
**CONF 002
(1) Subtask 273223-700-003-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 22-97-00-740-801
Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-802
Task 27-96-00-740-807
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 49
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(a) Job set-up:
1
 Remove the safety clips and/or tags and close/unlock the circuit breakers as
specified in the installation of the FCPCs (2CE1, 2CE2 and 2CE3), refer to
AMM Task 27-93-34-400-801.
(b) Procedure:
1
 After power-up, on the FLT CTL section of the overhead panel 241VU
(212VU), make sure that the PRIM 1, (PRIM 2), (PRIM 3) pushbutton
switch(es) is (are) pushed (the OFF and FAULT legends of this (these)
pushbutton switch(es) are off).
If a FAULT is present, do a reset with the concerned pushbutton switch.
If FAULT persists, replace the concerned computer, refer to AMM Task
27-93-34-000-801 and AMM Task 27-93-34-400-801.
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the new PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Do the BITE test of the EFCS (SYSTEM TEST), refer to AMM Task
27-96-00-740-802.
4
 If the airline operates the aircraft in CAT III conditions, do the LAND CAT III
capability test, refer to AMM Task 22-97-00-740-801.
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 273223-942-003-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up procedure as specified in the installation of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 50
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**CONF 002
(1) Subtask 273223-942-003-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up procedure as specified in the installation of the FCPCs (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 51
5
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SERVICE BULLETIN
Service Bulletin REPORTING
TITLE: FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY COMPUTER (FCPC)
- INSTALL NEW FCPC M25-2K0 OR P16M25-2K1
MODIFICATION No.: 206412S33844 206413S33845
SB Reporting status
This Service Bulletin will only be incorporated into affected customized Maintenance and Flight
Operations Products if it is duly reported to Airbus.
General information
The SB Reporting policy is published in ISI 00.00.00135. This document provides information regarding:
the SB Reporting means and benefits, the update of customized Maintenance Products and customized
Flight Operations Products.
If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations Products" for
further information on the update of affected Flight Operations Products.
SB Reporting procedure
Standard practice to report SB is to use the online reporting application on AirbusWorld.
Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus. Question 2 "What are the standard
practices for SB reporting?"
- If this SB requires previous or simultaneous accomplishment of other SBs, Question 3 "What about
the reporting of prerequisite Service Bulletin?"
NOTE:
 ISI 00.00.00179 covers all the frequently asked questions about SB Reporting. It is revised on a
regular basis.
DATE: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 1
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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: Jun 06/17 SERVICE BULLETIN No.: A330-27-3223
REVISION No.: 00 - Jun 06/17 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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