# Airbus Mandatory Service Bulletin A330-27-3177

Copy: No revision named ("U.S. DOT/FAA - Service Bulletin - A330-27-3177 R00"), 49 pages: PDF https://openairdocs.org/files/sha256/cd/d7/cdd7814d6f4aebc91bd905de4e88575a7afc9d63b921df057c59db03122659e0; text https://openairdocs.org/service-documents/airbus/a330-27-3177/file/cdd7814d6f4a.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2013-0329; AD 2013-19-14 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Mandatory Service Bulletin)
- Number: A330-27-3177
- Page: https://openairdocs.org/service-documents/airbus/a330-27-3177

## ADs that cite it (2) (OpenAirDocs)

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

- [AD 2013-19-14](https://openairdocs.org/ad/2013-19-14.md), effective Dec 19, 2013: No revision named
- [AD 2013-05-08](https://openairdocs.org/ad/2013-05-08.md), effective Jun 13, 2013: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-27-3177/proposed.md).

## Text (49 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2013-0329; AD 2013-19-14 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 - FCPC - INTRODUCE NEW FCPC P12AM21A 2K1
FOR A330-200/300 AND FCPC M21A 2K0 FOR A330-300 BASIC A/C
WITH MECHANICAL RUDDER
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 55440S18650
 200360S30853
 200359S30852
 201687S31873
 201688S31874
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
When there are significant differences between all airspeed sources, the flight controls revert to
alternate law, the autopilot (AP) and the autothrust (A/THR) automatically disconnect and the Flight
Directors (FD) bars are automatically removed.
It has been identified that, after such an event, if two airspeed sources become similar while still
erroneous, the flight guidance computers:
- Display FD Bars again.
- Enable autopilot and autothrust re-engagement.
However, in some cases, the autopilot orders may be inappropriate, such as possible abrupt pitch
command.
To address these inappropriate orders, operational recommendations were issued beginning of January
2011 in red OEB 35 (formerly OEB 82/1 up until 2011) and it is associated OEB PROC 35 (formerly
OEB 82 up until 2011) in the Quick Reference Handbook (QRH).
This Service Bulletin is published to advise all operators of A330 aircraft of the issue of AIRBUS
OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 and/or LA2K0-27-023.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A330
SERVICE BULLETIN
SUMMARY
This Service Bulletin recommends either replacing the existing FCPCs with hardware 2K1 and 2K0 by
FCPCs with hardware 2K1, 2K0 and new standard P12A/M21A or modifying the existing FCPCs
with hardware 2K1 and 2K0 into new standard P12A/M21A by means of On-Board Replaceable
Modules (OBRMs) as per AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 and/or
LA2K0-27-023.
New software standard P12A/M21A on FCPC 2K1 and 2K0 hardware has been defined to take into
account the last FCPC software evolutions. The main FCPC improvements are:
- Inhibit autopilot engagement under unreliable airspeed condition in the here above situation
described in FOT Ref.999.0112/10 dated on 20 December 2010,
- Improvement of aircraft behavior in case of erratic ADIRU outputs,
- Improvement of the reconfiguration logics in case of electrical transients during rotation at take off
(TFU No. 27.90.00.035),
- Improvement of the Ground Spoiler (GS) and Partial Lift Damping (PLD) logics,
- Reduction of high Vertical Speed (VZ) at touchdown with new parameters recording in the Digital
Flight Data Recorder (DFDR),
- Improvement of aircraft behaviour in case of two consistently erroneous Angle Of Attack (AOA)
information: limitation of Trimmable Horizontal Stabilizer (THS) at pitch-up.
Accomplishment of this Service Bulletin will cancel the red OEB 35 (formerly OEB 82/1 up until
2011) and the Airplane Flight Manuel (AFM) TR 149 m andated by EASA Airworthiness Directive No.
2010-0271.
Accomplishment of this Service Bulletin will also cancel the red OEB 23 (formerly OEB 74 up until
2011) and Flight Manual (FM) TR 4.02.00/46.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 MANDATORY (1)
 CANCELS INSPECTION SB
 NO
POTENTIAL AD
 YES
 A/C OPERATION AFFECTED
 YES
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
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
SUMMARY
**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
**CONF 003
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEA03
 1
 See SB
 FCPCs
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
ACA ACI AEA AFR AGC ALK AZA BEL BER BMA BTV CPA CRL
CYP DGA EDW EIN EVA FWI GFA GIA GRL HDA HFY HVN IAC
JST KAL KKK MAS MON OHY PAL QAF QTR RSY SAS SWR TAM
TAP TCX THA THY TSC UAE USA VKG VLK VOZ XAX XLF
CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the
following Service Bulletin or the equivalent production modification(s):
Service Bulletin No. A330-27-3132 Mod. No. 49965S16501
51341S16795
53503S18051
53504S18052
A330-31-3048 49632S16354
REFERENCES / REPERCUSSIONS
TFU
 27.90.00.035
OEB
 23
35
AOT
 None
SIL
 00-022
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 FOT Ref. 999.0112/10 dated 20 December 2010
OTHER
 OIT SE 999.0035/11 dated 28 April 2011
NATURE OF THE WORK
AIRCRAFT
 NO
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A330
SERVICE BULLETIN
SUMMARY
EQUIPMENT
 YES
HARD
 YES
SOFT
 NO
OBRM
 YES
MANPOWER
**CONF 001
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours relat ed to Vendor SB; refer to:
In the Main Rack 800VU and on the FWD Shelf 915VU,
modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by
replacement or reprogramming of their OBRMs.
AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K1-27-015
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
**CONF 002
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours relat ed to Vendor SB; refer to:
In the Main Rack 800VU and on the FWD Shelf 915VU,
modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by
replacement or reprogramming of their OBRMs.
AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K1-27-015
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
**CONF 003
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours relat ed to Vendor SB; refer to:
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A330
SERVICE BULLETIN
SUMMARY
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
In the Main Rack 800VU and on the FWD Shelf 915VU,
modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by
replacement or reprogramming of their OBRMs.
AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K0-27-023
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
APPENDICES
**CONF ALL
None
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
FR20
2CE1
2CE2
2CE3
A
B
A
B
Z120
G_SB_273177_5_SAAA_01_00
915VU
800VU
Figure A-FSAAA - Sheet 01
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### 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 - FCPC - INTRODUCE NEW FCPC P12AM21A 2K1
FOR A330-200/300 AND FCPC M21A 2K0 FOR A330-300 BASIC A/C
WITH MECHANICAL RUDDER
MODIFICATION No.: 55440S18650 200360S30853 200359S30852 201687S31873 201688S31874
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
: These modifications are applicable by Service Bulletin only.
NOTE
: This Service Bulletin is only applicable to aircraft on which Mod. No.
49144S16279 (INSTALL RUDDER FLY-BY WIRE ON A330/A340) is not
embodied.
(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 0064-0067 0069-0073 0077
0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116
0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172
0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 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
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A330
SERVICE BULLETIN
0290-0291 0293-0296 0299-0301 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 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
ACA
 0277 0279 0284 0344 0400 0408 0412 0419
ACI
 0507 0510
AEA
 0461 0551 0597
AFR
 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519
0567 0584 0657
AGC
 0324
ALK
 0303 0306 0311 0313 0404 0627
AZA
 0272 0339
BEL
 0030 0037 0045 0082 0095 0229
BER
 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493
BMA
 0398 0401
BTV
 0205 0330
CPA
 0012 0017 0071 0102 0113 0118 0121 0155 0244 0386 0389 0393
0418 0420 0421 0423 0439 0539 0548 0565
CRL
 0285 0320
CYP
 0505 0526
DGA
 0240
EDW
 0291
EIN
 0269 0397
EVA
 0530 0535
FWI
 0253
GFA
 0276 0281 0286 0287 0334 0340 0527 0529 0532
GIA
 0138 0140 0144 0148 0153 0165
GRL
 0230
HDA
 0083 0099 0106 0109 0234 0405 0479 0512 0581
HFY
 0096 0211
HVN
 0255 0262 0275 0294 0299 0366
IAC
 0353 0362
JST
 0506 0508 0513 0522
KAL
 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350
0351 0368 0425 0428 0484 0490 0550
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A330
SERVICE BULLETIN
OPERATOR
 MSN
KKK
 0343 0358 0364
MAS
 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300
MON
 0261 0265
OHY
 0072 0087 0098 0143
PAL
 0183 0184 0188 0189 0191 0198 0200 0203
QAF
 0487
QTR
 0441 0473 0489 0511 0521
RSY
 0171
SAS
 0496 0497 0515 0568
SWR
 0249
TAM
 0232 0238 0247 0259 0361 0466 0472 0477 0486
TAP
 0181 0195 0223 0305 0308 0312 0317
TCX
 0254 0266 0301 0427 0456
THA
 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346
THY
 0463 0504
TSC
 0111 0132 0177 0250 0271 0369 0407 0480
UAE
 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382
0384 0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509
0518 0525 0536
USA
 0315 0323 0333 0337 0342 0370 0375 0380 0388
VKG
 0309 0349 0356 0357
VLK
 0055 0070 0086
VOZ
 0365 0372
XAX
 0054
XLF
 0501 0635
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064
0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083
0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109
0110 0112 0113 0116 0118 0119 0120 0121 0122 0127 0132
0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172
0177 0183 0184 0188 0189 0191 0198 0200 0203 0206 0209
0219 0224 0231 0234 0241 0244 0256 0267
003
0111 0277 0279 0284
 002 003
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A330
SERVICE BULLETIN
MSN
 CONFIGURATION
0181 0195 0205 0211 0222 0223 0226 0229 0230 0232 0238
0240 0247 0248 0249 0250 0251 0253 0254 0255 0258 0259
0261 0262 0265 0266 0269 0271 0272 0275 0276 0281 0283
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 0356 0357 0358 0361 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
002
0353 0362
 001 002
(5) Configuration definition
**CONF 001
Config. 001 is valid for aircraft on which Service Bulletin No. A330-27-3080 (Mod. No.
47735S14929) is embodied and on which Service Bulletin No. A330-27-3079 (Mod. No.
47587S14930) and Service Bulletin No. A330-27-3144 (Mod. No. 55440S18650) are not
embodied.
**CONF 002
Config. 002 is valid for aircraft on which Service Bulletin No. A330-27-3080 (Mod. No.
47735S14929) and Service Bulletin No. A330-27-3144 (Mod. No 55440S18650) are
embodied and on which Service Bulletin No. A330-27-3079 (Mod. No. 47587S14930) is
not embodied.
**CONF 003
Config. 003 is valid for aircraft on which Service Bulletin No. A330-27-3079 (Mod. No.
47587S14930 and Service Bulletin No. A330-27-3144 (Mod. No. 55439S18649) are
embodied and on which Service Bulletin No. A330-27-3080 (Mod. No. 47735S14929) is
not embodied.
(6) Material Effectivity
**CONF 001
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEA01
 1
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A330
SERVICE BULLETIN
**CONF 002
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEA02
 1
**CONF 003
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEA03
 1
**CONF ALL
B. CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of
the following Service Bulletin or the equivalent production modification(s):
Service Bulletin No. A330-27-3132 Mod. No. 49965S16501
51341S16795
53503S18051
53504S18052
A330-31-3048 49632S16354
C. REASON
(1) History
When there are significant differences between all airspeed sources, the flight controls
revert to alternate law, the autopilot (AP) and the autothrust (A/THR) automatically
disconnect and the Flight Directors (FD) bars are automatically removed.
It has been identified that, after such an event, if two airspeed sources become similar
while still erroneous, the flight guidance computers:
- Display FD Bars again.
- Enable autopilot and autothrust re-engagement.
However, in some cases, the autopilot orders may be inappropriate, such as possible
abrupt pitch command.
To address these inappropriate orders, operational recommendations were issued
beginning of January 2011 in red OEB 35 (formerly OEB 82/1 up until 2011) and it is
associated OEB PROC 35 (formerly OEB 82 up until 2011) in the Quick Reference
Handbook (QRH).
(2) Objective/Action
This Service Bulletin is published to advise all operators of A330 aircraft of the issue of
AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 and/or LA2K0-27-023.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A330
SERVICE BULLETIN
This Service Bulletin recommends either replacing the existing FCPCs with hardware
2K1 and 2K0 by FCPCs with hardware 2K1, 2K0 and new standard P12A/M21A
or modifying the existing FCPCs with hardware 2K1 and 2K0 into new standard
P12A/M21A by means of On-Board Replaceable Modules (OBRMs) as per AIRBUS
OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 and/or LA2K0-27-023.
(3) Advantages
New software standard P12A/M21A on FCPC 2K1 and 2K0 hardware has been defined
to take into account the last FCPC software evolutions. The main FCPC improvements
are:
- Inhibit autopilot engagement under unreliable airspeed condition in the here above
situation described in FOT Ref.999.0112/10 dated on 20 December 2010,
- Improvement of aircraft behavior in case of erratic ADIRU outputs,
- Improvement of the reconfiguration logics in case of electrical transients during
rotation at take off (TFU No. 27.90.00.035),
- Improvement of the Ground Spoiler (GS) and Partial Lift Damping (PLD) logics,
- Reduction of high Vertical Speed (VZ) at touchdown with new parameters recording
in the Digital Flight Da ta Recorder (DFDR),
- Improvement of aircraft behaviour in case of two consistently erroneous Angle Of
Attack (AOA) information: limitation of Trimmable Horizontal Stabilizer (THS) at
pitch-up.
(4) Operational/Maintenance Consequences
Accomplishment of this Service Bulletin will cancel the red OEB 35 (formerly OEB 82/1
up until 2011) and the Airplane Flight Manuel (AFM) TR 149 mandat ed by EASA
Airworthiness Directive No. 2010-0271.
Accomplishment of this Service Bulletin will also cancel the red OEB 23 (formerly OEB
74 up until 2011) and Flight Manual (FM) TR 4.02.00/46.
D. DESCRIPTION
NOTE
: To accomplish this Service Bulletin, you have two possibilities:
- either you modify the three FCPCs by replacement or reprogramming of
their OBRMs as described in TASK 273177-831-801 001 Modification of
the three FCPCs by replacement or reprogramming of their OBRMs. ,
- or you replace them as described in TASK 273177-831-802 001
Modification by replacement of the three FCPCs. .
To accomplish this Service Bulletin it is necessary to :
**CONF 001
Task 273177-831-801-001: Modification of the three FCPCs by replacement or
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 6
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SERVICE BULLETIN
reprogramming of their OBRMs.
(1) In the Main Rack 800VU and on the FWD Shelf 915VU, modify the three FCPCs
(FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs.
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
(1) In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs
(FINs 2CE1, 2CE2 and 2CE3).
**CONF 002
Task 273177-831-801-001: Modification of the three FCPCs by replacement or
reprogramming of their OBRMs.
(1) In the Main Rack 800VU and on the FWD Shelf 915VU, modify the three FCPCs
(FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs.
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
(1) In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs
(FINs 2CE1, 2CE2 and 2CE3).
**CONF 003
Task 273177-831-801-001: Modification of the three FCPCs by replacement or
reprogramming of their OBRMs.
(1) In the Main Rack 800VU and on the FWD Shelf 915VU, modify the three FCPCs
(FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs.
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
(1) In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs
(FINs 2CE1, 2CE2 and 2CE3).
**CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
This Service Bulletin has been classified Mandatory by the issue of an Airworthiness
Directive (AD) published by the European Av iation Safety Agenc y (EASA). The AD must
be used as the reference document for the mandated accomplishment timescale.
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organization Approval No. EASA.21J.031.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 7
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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 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
Get Access
 1.00
Tests
 0.50
Close-Up
 1.00
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours relat ed to Vendor SB; refer to:
In the Main Rack 800VU and on the FWD Shelf
915VU, modify the three FCPCs (FINs 2CE1, 2CE2
and 2CE3) by replacement or reprogramming of their
OBRMs.
AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K1-27-015
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
Get Access
 1.00
On Aircraft
In the Main Rack 800VU and on the FWD Shelf
915VU, replace the three FCPCs (FINs 2CE1, 2CE2
and 2CE3).
1.50
Tests
 1.00
Close-Up
 1.00
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
**CONF 002
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
Get Access
 1.00
Tests
 0.50
Close-Up
 1.00
TOTAL MANHOURS
 2.50
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 8
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SERVICE BULLETIN
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
ELAPSED TIME (HOURS)
 2.50
Additional manhours relat ed to Vendor SB; refer to:
In the Main Rack 800VU and on the FWD Shelf
915VU, modify the three FCPCs (FINs 2CE1, 2CE2
and 2CE3) by replacement or reprogramming of their
OBRMs.
AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K1-27-015
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
Get Access
 1.00
On Aircraft
In the Main Rack 800VU and on the FWD Shelf
915VU, replace the three FCPCs (FINs 2CE1, 2CE2
and 2CE3).
1.50
Tests
 1.00
Close-Up
 1.00
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
**CONF 003
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming
of their OBRMs.
Get Access
 1.00
Tests
 0.50
Close-Up
 1.00
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours relat ed to Vendor SB; refer to:
In the Main Rack 800VU and on the FWD Shelf
915VU, modify the three FCPCs (FINs 2CE1, 2CE2
and 2CE3) by replacement or reprogramming of their
OBRMs.
AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K0-27-023
Task 273177-831-802-001: Modification by replacement of the three FCPCs.
Get Access
 1.00
On Aircraft
In the Main Rack 800VU and on the FWD Shelf
915VU, replace the three FCPCs (FINs 2CE1, 2CE2
and 2CE3).
1.50
Tests
 1.00
Close-Up
 1.00
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 9
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SERVICE BULLETIN
**CONF ALL
H. WEIGHT AND BALANCE
Not Changed
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Airworthiness Directive (AD)
 Airworthiness Directive No.
2010-0271
Aircraft Maintenance Manual (AMM)
 12-34-24 20-15-00 22-97-00
27-93-34 27-96-00 31-51-00
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Service Bulletin (SB)
 A330-27-3079
A330-27-3080
A330-27-3132
A330-27-3144
A330-31-3048
Service Information Letter (SIL)
 SIL 00-022
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K1-27-015
**CONF 002
Airworthiness Directive (AD)
 Airworthiness Directive No.
2010-0271
Aircraft Maintenance Manual (AMM)
 12-34-24 20-15-00 22-97-00
27-93-34 27-96-00 31-51-00
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Service Bulletin (SB)
 A330-27-3079
A330-27-3080
A330-27-3132
A330-27-3144
A330-31-3048
Service Information Letter (SIL)
 SIL 00-022
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K1-27-015
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 10
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SERVICE BULLETIN
**CONF 003
Airworthiness Directive (AD)
 Airworthiness Directive No.
2010-0271
Aircraft Maintenance Manual (AMM)
 12-34-24 20-15-00 22-97-00
27-93-34 27-96-00 31-51-00
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Service Bulletin (SB)
 A330-27-3079
A330-27-3080
A330-27-3132
A330-27-3144
A330-31-3048
Service Information Letter (SIL)
 SIL 00-022
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K0-27-023
**CONF ALL
K. PUBLICATION AFFECTED
Aircraft Maintenance Manual (AMM)
 27-93-00
Aircraft Wiring List (AWL)
Flight Crew Operating Manuel (FCOM)
Flight Manual (FM)
Illustrated Parts Catalog (IPC)
 27-93-08
Master Minimum Equipment List (MMEL)
This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in
advance, in case you need your operational documentation to be amended by a revision prior
to Service Bulletin embodiment. For this purpose, please request the revision by e-mail, on-
line through the SB Reporting service or alternatively by fax to :
SEDOR4 - AIRBUS Customer Services Technical Data
F a xN o . :( 3 3 )56 19 32 80 6
E-mail: sb.reporting@airbus.com
SB Reporting service is accessible on-line through AIRBUSWorld from :
My on-line services’ section, available on all AIRBUSWorld pages.
The Maintenance and Engineering Community, in :
- Modify and Upgrade page,
- Access SB and VSB section.
These amendments will be confirmed by the next normal revision of operational
documentation, once your Service Bulletin accomplishment report has been sent, as usual, to
our Customer Services Aircraft In-Service Data (SEDOR4).
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 11
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SERVICE BULLETIN
L. INTERCHANGEABILITY/MIXABILITY
**CONF 001
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
FCPC
 LA2K1A100DA0000
 LA2K1A100DE0000
 03
 NO
 (1) (2) (3)
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)
: On non-enhanced A330-300 aircraft model, FCPC standard M21A 2K0 (PN
LA2K01500AE0000) is interchangeable with FCPC standard P12A/M21A
2K1 (PN LA2K1A100DE0000) and interchangeable and mixable with FCPC
standard P11A/M20A 2K2 (PN LA2K2B100DF0000).
NOTE
 (2)
: On non-enhanced A330-200 aircraft model, FCPC standard P12A/M21A 2K1
(PN LA2K1A100DE0000) is interchangeable and mixable with FCPC standard
P11A/M20A 2K2 (PN LA2KB100DF0000).
NOTE
 (3)
: Interchangeability code 03 becomes 01 provided that the three FCPCs are
replaced at the same time. Mixability not authorized. Replacement of the
three FCPCs has to be done simultaneously as per ACCOMPLISHMENT
INSTRUCTIONS paragraph C. of this Service Bulletin.
**CONF 002
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
FCPC
 LA2K1A100DC0000
 LA2K1A100DE0000
 03
 NO
 (1) (2) (3)
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)
: On non-enhanced A330-300 aircraft model, FCPC standard M21A 2K0 (PN
LA2K01500AE0000) is interchangeable with FCPC standard P12A/M21A
2K1 (PN LA2K1A100DE0000) and interchangeable and mixable with FCPC
standard P11A/M20A 2K2 (PN LA2K2B100DF0000).
NOTE
 (2)
: On non-enhanced A330-200 aircraft model, FCPC standard P12A/M21A 2K1
(PN LA2K1A100DE0000) is interchangeable and mixable with FCPC standard
P11A/M20A 2K2 (PN LA2KB100DF0000).
NOTE
 (3)
: Interchangeability code 03 becomes 01 provided that the three FCPCs are
replaced at the same time. Mixability not authorized. Replacement of the
three FCPCs has to be done simultaneously as per ACCOMPLISHMENT
INSTRUCTIONS paragraph C. of this Service Bulletin.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 12
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**CONF 003
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
FCPC
 LA2K01500AC0000
 LA2K01500AE0000
 03
 NO
 (1) (2) (3)
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)
: Interchangeability code 03 becomes 01 provided that the three FCPCs are
replaced at the same time. Mixability not authorized. Replacement of the
three FCPCs has to be done simultaneously as per ACCOMPLISHMENT
INSTRUCTIONS paragraph C. of this Service Bulletin.
NOTE
 (2)
: On non-enhanced A330-300 aircraft model, FCPC standard M21A 2K0 (PN
LA2K01500AE0000) is interchangeable with FCPC standard P12A/M21A
2K1 (PN LA2K1A100DE0000) and interchangeable and mixable with FCPC
standard P11A/M20A 2K2 (PN LA2K2B100DF0000).
NOTE
 (3)
: On non-enhanced A330-200 aircraft model, FCPC standard 2K0 cannot be
installed.
**CONF ALL
M. SPARES
FCPC LA2K01500AC0000
FCPC LA2K1A100DA0000
FCPC LA2K1A100DC0000
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 13
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This Page Intentionally Left Blank
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 14
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SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
Equipment BFEA01
Equipment BFEA02
Modification of removed equipment should be
negotiated directly with AIRBUS OPERATION
S.A.S. as per instructions given in AIRBUS
OPERATION S.A.S. Service Bulletin No.
LA2K1-27-015.
Equipment BFEA03
 Modification of removed equipment should be
negotiated directly with AIRBUS OPERATION
S.A.S. as per instructions given in AIRBUS
OPERATION S.A.S. Service Bulletin No.
LA2K0-27-023.
(2) Price and Availability
No AIRBUS kit will be provided.
Refer to the Vendor Service Bulletin No. LA2K1-27-015 or LA2K0-27-023 for the
equipment modification sales terms.
B. INDUSTRY SUPPORT INFORMATION
Refer to the Vendor Service Bulletin No. LA2K1-27-015 or LA2K0-27-023 for the industry
support terms of the Vendor Service Bulletin parts and labor.
For the organization of this retrofit, operators 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
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 15
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SERVICE BULLETIN
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
LA2K1A100DE0000
 3
 FCPC
 LA2K1A100DA0000
 03
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: Modification of removed equipment should be negotiated directly with
AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin
No. LA2K1-27-015.
Equipment BFEA02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K1A100DE0000
 3
 FCPC
 LA2K1A100DC0000
 03
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: Modification of removed equipment should be negotiated directly with
AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin
No. LA2K1-27-015.
Equipment BFEA03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K01500AE0000
 3
 FCPC
 LA2K01500AC0000
 03
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: Modification of removed equipment should be negotiated directly with
AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin
No. LA2K0-27-023.
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
None
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 16
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F. TOOLING
(1) Tooling - Price and Availability
None
(2) Tools
To accomplish this Service Bulletin it is necessary to use the tools defined in AIRBUS
OPERATION S.A.S. Service Bulletin No. LA 2K1-27-015 or AIRBUS OPERATION S.A.S.
Service Bulletin No. LA2K0-27-023.
(3) Special Tools
None
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 17
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This Page Intentionally Left Blank
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 18
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3. ACCOMPLISHMENT INSTRUCTIONS
Task 273177-831-801-001 - Modification of the three FCPCs by replacement or
reprogramming of their OBRMs.
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.
IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.
CAUTION
: REFER TO AMM 20-15-00, Page Block 201 AND AIRBUS SIL 00-022 FOR
ELECTROSTATIC DISCHARGE PRECAUTIONS.
NOTE
: This Task concerns the modification of the FCPCs by replacement or by
reprogramming of theirs OBRMs.
Task Associated Data
**CONF 001
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Manpower
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours related to Vendor SB; refer to:
AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015
**CONF 002
Zone
120
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 19
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SERVICE BULLETIN
Modified FIN
2CE1 2CE2 2CE3
Manpower
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours related to Vendor SB; refer to:
AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015
**CONF 003
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Manpower
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Additional manhours related to Vendor SB; refer to:
AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-023
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 273177-839-001-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
(a) Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF 002
(1) Subtask 273177-839-001-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
(a) Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 20
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**CONF 003
(1) Subtask 273177-839-001-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
(a) 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 273177-941-001-001 - 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
(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 three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).
**CONF 002
(1) Subtask 273177-941-001-001 - 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
(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 three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 21
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**CONF 003
(1) Subtask 273177-941-001-001 - 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
(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 three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 273177-831-001-003 - In the Main Rack 800VU and on the FWD Shelf
915VU, modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or
reprogramming of their OBRMs.
Work Zones and Access Panels
Zone
 Access/Work location
120
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-807
Task 31-51-00-610-802
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S. LA2K1-27-015
(a) Before replacement or 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) is (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 P/N of the FCPCs are correct,
(Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015).
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 22
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3
 Open, safety/lock and tag the circuit breakers specified as per removal of the
Flight control Primary Computer (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM
Task 27-93-34-000-801).
4
 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1,
2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No.
LA2K1-27-015.
5
 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers
as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM
Task 27-93-34-400-801).
(b) OEB cancellation:
1
 On A/C equipped with OEB REMINDER function, if the ECAM warning has
been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the
following codes should be deleted from the FWC database.
CODE
 WARN
 STS
34/10/050/061
 YES
 NO
34/10/060/063
 YES
 NO
34/10/070/065
 YES
 NO
34/10/020/055
 YES
 NO
34/10/030/057
 YES
 NO
34/10/040/059
 YES
 NO
Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from
FWCs using MCDUs".
**CONF 002
(1) Subtask 273177-831-001-004 - In the Main Rack 800VU and on the FWD Shelf
915VU, modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or
reprogramming of their OBRMs.
Work Zones and Access Panels
Zone
 Access/Work location
120
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-807
Task 31-51-00-610-802
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S. LA2K1-27-015
(a) Before replacement or 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) is (are) off).
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 23
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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 P/N of the FCPCs are correct,
(Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015).
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 specified as per removal
of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task
27-93-34-000-801).
4
 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1,
2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No.
LA2K1-27-015.
5
 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers
as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM
Task 27-93-34-400-801).
(b) OEB cancellation:
1
 On A/C equipped with OEB REMINDER function, if the ECAM warning has
been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the
following codes should be deleted from the FWC database.
CODE
 WARN
 STS
34/10/050/061
 YES
 NO
34/10/060/063
 YES
 NO
34/10/070/065
 YES
 NO
34/10/020/055
 YES
 NO
34/10/030/057
 YES
 NO
34/10/040/059
 YES
 NO
Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from
FWCs using MCDUs".
**CONF 003
(1) Subtask 273177-831-001-005 - In the Main Rack 800VU and on the FWD Shelf
915VU, modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or
reprogramming of their OBRMs.
Work Zones and Access Panels
Zone
 Access/Work location
120
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-807
Task 31-51-00-610-802
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S. LA2K0-27-023
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 24
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(a) Before replacement or 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) is (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 P/N of the FCPCs are correct,
(Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-023).
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 specified as per removal
of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task
27-93-34-000-801).
4
 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1,
2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No.
LA2K0-27-023.
5
 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers
as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM
Task 27-93-34-400-801).
(b) OEB cancellation:
1
 On A/C equipped with OEB REMINDER function, if the ECAM warning has
been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the
following codes should be deleted from the FWC database.
CODE
 WARN
 STS
34/10/050/061
 YES
 NO
34/10/060/063
 YES
 NO
34/10/070/065
 YES
 NO
34/10/020/055
 YES
 NO
34/10/030/057
 YES
 NO
34/10/040/059
 YES
 NO
Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from
FWCs using MCDUs".
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 273177-700-001-002 - Test
Manpower Resources
Skills
 NON SPECIFIC
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 25
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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
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S. LA2K1-27-015
(a) 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) is (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).
(b) Do the BITE test of the Electrical Flight Control System (EFCS) (LRU IDENT)
(Refer to AMM Task 27-96-00-740-807) and make sure that the new P/N of the
FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin No.
LA2K1-27-015).
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not available,
a visual check is acceptable).
(c) Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task
27-96-00-740-802).
(d) If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III
capability test (Refer to AMM Task 22-97-00-740-801).
**CONF 002
(1) Subtask 273177-700-001-001 - Test
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
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S. LA2K1-27-015
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 26
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(a) 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) is (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).
(b) Do the BITE test of the Electrical Flight Control System (EFCS) (LRU IDENT)
(Refer to AMM Task 27-96-00-740-807) and make sure that the new P/N of the
FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin No.
LA2K1-27-015).
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not available,
a visual check is acceptable).
(c) Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task
27-96-00-740-802).
(d) If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III
capability test (Refer to AMM Task 22-97-00-740-801).
**CONF 003
(1) Subtask 273177-700-001-003 - Test
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
Vendor Service Bulletin (VSB)
 AIRBUS OPERATION S.A.S. LA2K0-27-023
(a) 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) is (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).
(b) Do the BITE test of the Electrical Flight Control System (EFCS) (LRU IDENT)
(Refer to AMM Task 27-96-00-740-807) and make sure that the new P/N of the
FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin No.
LA2K0-27-023).
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not available,
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 27
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SERVICE BULLETIN
a visual check is acceptable).
(c) Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task
27-96-00-740-802).
(d) If the airline operates the aircraft in CAT 3 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 273177-942-001-001 - 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 procedure as specified in installation of the three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).
(c) Remove the access platform(s).
(d) Restore the systems and the aircraft to normal operating condition.
**CONF 002
(1) Subtask 273177-942-001-001 - 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 procedure as specified in installation of the three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).
(c) Remove the access platform(s).
(d) Restore the systems and the aircraft to normal operating condition.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 28
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**CONF 003
(1) Subtask 273177-942-001-001 - 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 procedure as specified in installation of the three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).
(c) Remove the access platform(s).
(d) Restore the systems and the aircraft to normal operating condition.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 29
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This Page Intentionally Left Blank
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 30
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Task 273177-831-802-001 - Modification by replacement of the three FCPCs.
**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.
IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.
NOTE
: This Task concerns the replacement of the three FCPCs.
Task Associated Data
**CONF 001
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Manpower
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
**CONF 002
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Manpower
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 31
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**CONF 003
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Manpower
TOTAL MANHOURS
 4.50
ELAPSED TIME (HOURS)
 4.50
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 273177-839-002-001 - 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 273177-839-002-001 - 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 003
(1) Subtask 273177-839-002-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 32
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**CONF ALL
B. PREPARATION
**CONF 001
(1) Subtask 273177-941-002-001 - 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
(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 three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).
**CONF 002
(1) Subtask 273177-941-002-001 - 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
(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 three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).
**CONF 003
(1) Subtask 273177-941-002-001 - 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
(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task
12-34-24-860-802).
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 33
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(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 273177-960-002-001 - In the Main Rack 800VU and on the FWD Shelf
915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).
Work Zones and Access Panels
Zone
 Access/Work location
120
Manpower Resources
Manhours
 1.50
Minimum number of person
 1
Subtask elapsed time
 1.50
Skills
 NON SPECIFIC
Material necessary to do the job
Equipment BFEA01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K1A100DE0000
 3
 FCPC
NOTE
: Modification of removed equipment should be negotiated directly with
AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin
No. LA2K1-27-015.
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
Task 31-51-00-610-802
(a) Replacement of the FCPCs:
1
 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1):
Refer to AMM Task 27-93-34-000-801
FIN 2CE1
1 FCPC LA2K1A100DA0000
2
 On the FWD Shelf 915VU, install the FCPC (FIN 2CE1):
Refer to AMM Task 27-93-34-400-801
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 34
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FIN 2CE1
1 FCPC LA2K1A100DE0000
3
 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-000-801
FIN 2CE2
1 FCPC LA2K1A100DA0000
and
FIN 2CE3
1 FCPC LA2K1A100DA0000
4
 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-400-801
FIN 2CE2
1 FCPC LA2K1A100DE0000
and
FIN 2CE3
1 FCPC LA2K1A100DE0000
(b) OEB cancellation:
1
 On A/C equipped with OEB REMINDER function, if the ECAM warning has
been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the
following codes should be deleted from the FWC database.
CODE
 WARN
 STS
34/10/050/061
 YES
 NO
34/10/060/063
 YES
 NO
34/10/070/065
 YES
 NO
34/10/020/055
 YES
 NO
34/10/030/057
 YES
 NO
34/10/040/059
 YES
 NO
Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from
FWCs using MCDUs".
**CONF 002
(1) Subtask 273177-960-002-002 - In the Main Rack 800VU and on the FWD Shelf
915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).
Work Zones and Access Panels
Zone
 Access/Work location
120
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 35
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Manpower Resources
Manhours
 1.50
Minimum number of person
 1
Subtask elapsed time
 1.50
Skills
 NON SPECIFIC
Material necessary to do the job
Equipment BFEA02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K1A100DE0000
 3
 FCPC
NOTE
: Modification of removed equipment should be negotiated directly with
AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin
No. LA2K1-27-015.
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
Task 31-51-00-610-802
(a) Replacement of the FCPCs:
1
 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1):
Refer to AMM Task 27-93-34-000-801
FIN 2CE1
1 FCPC LA2K1A100DC0000
2
 On the FWD Shelf 915VU, install the FCPC (FIN 2CE1):
Refer to AMM Task 27-93-34-400-801
FIN 2CE1
1 FCPC LA2K1A100DE0000
3
 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-000-801
FIN 2CE2
1 FCPC LA2K1A100DC0000
and
FIN 2CE3
1 FCPC LA2K1A100DC0000
4
 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-400-801
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 36
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FIN 2CE2
1 FCPC LA2K1A100DE0000
and
FIN 2CE3
1 FCPC LA2K1A100DE0000
(b) OEB cancellation:
1
 On A/C equipped with OEB REMINDER function, if the ECAM warning has
been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the
following codes should be deleted from the FWC database.
CODE
 WARN
 STS
34/10/050/061
 YES
 NO
34/10/060/063
 YES
 NO
34/10/070/065
 YES
 NO
34/10/020/055
 YES
 NO
34/10/030/057
 YES
 NO
34/10/040/059
 YES
 NO
Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from
FWCs using MCDUs".
**CONF 003
(1) Subtask 273177-960-002-003 - In the Main Rack 800VU and on the FWD Shelf
915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).
Work Zones and Access Panels
Zone
 Access/Work location
120
Manpower Resources
Manhours
 1.50
Minimum number of person
 1
Subtask elapsed time
 1.50
Skills
 NON SPECIFIC
Material necessary to do the job
Equipment BFEA03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K01500AE0000
 3
 FCPC
NOTE
: Modification of removed equipment should be negotiated directly with
AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin
No. LA2K0-27-023.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 37
5
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### Page 44

@A330
SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-93-34-400-801
Task 31-51-00-610-802
(a) Replacement of the FCPCs:
1
 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1):
Refer to AMM Task 27-93-34-000-801
FIN 2CE1
1 FCPC LA2K01500AC0000
2
 On the FWD Shelf 915VU, install the FCPC (FIN 2CE1):
Refer to AMM Task 27-93-34-400-801
FIN 2CE1
1 FCPC LA2K01500AE0000
3
 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-000-801
FIN 2CE2
1 FCPC LA2K01500AC0000
and
FIN 2CE3
1 FCPC LA2K01500AC0000
4
 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3):
Refer to AMM Task 27-93-34-400-801
FIN 2CE2
1 FCPC LA2K01500AE0000
and
FIN 2CE3
1 FCPC LA2K01500AE0000
(b) OEB cancellation:
1
 On A/C equipped with OEB REMINDER function, if the ECAM warning has
been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the
following codes should be deleted from the FWC database.
CODE
 WARN
 STS
34/10/050/061
 YES
 NO
34/10/060/063
 YES
 NO
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 38
5
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### Page 45

@A330
SERVICE BULLETIN
CODE
 WARN
 STS
34/10/070/065
 YES
 NO
34/10/020/055
 YES
 NO
34/10/030/057
 YES
 NO
34/10/040/059
 YES
 NO
Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from
FWCs using MCDUs".
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 273177-700-002-001 - Test
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Do the test after installation of the FCPC (FINs 2CE1, 2CE2 and 2CE3) (Refer to
AMM Task 27-93-34-400-801).
**CONF 002
(1) Subtask 273177-700-002-001 - Test
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Do the test after installation of the FCPC (FINs 2CE1, 2CE2 and 2CE3) (Refer to
AMM Task 27-93-34-400-801).
**CONF 003
(1) Subtask 273177-700-002-001 - Test
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Do the test after installation of the FCPC (FINs 2CE1, 2CE2 and 2CE3) (Refer to
AMM Task 27-93-34-400-801).
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 39
5
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### Page 46

@A330
SERVICE BULLETIN
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 273177-942-002-001 - 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 installation of the three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).
(c) Remove the access platform(s).
(d) Restore the systems and the aircraft to normal operating condition.
**CONF 002
(1) Subtask 273177-942-002-001 - 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 installation of the three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).
(c) Remove the access platform(s).
(d) Restore the systems and the aircraft to normal operating condition.
**CONF 003
(1) Subtask 273177-942-002-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 40
5
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### Page 47

@A330
SERVICE BULLETIN
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 installation of the three FCPCs (FINs
2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).
(c) Remove the access platform(s).
(d) Restore the systems and the aircraft to normal operating condition.
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 41
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 48

@A330
SERVICE BULLETIN
REPORTING SHEET
TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC P12AM21A 2K1
FOR A330-200/300 AND FCPC M21A 2K0 FOR A330-300 BASIC A/C
WITH MECHANICAL RUDDER
MODIFICATION No.: 55440S18650 200360S30853 200359S30852 201687S31873 201688S31874
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 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 49

@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 21/11 SERVICE BULLETIN No.: A330-27-3177
REVISION No.: 00 - Dec 21/11 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

---
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