@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

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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 mandated 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

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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

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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 related 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 related 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 related to Vendor SB; refer to:

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177

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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

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@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

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

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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

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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

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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

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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

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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 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.

(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 mandated 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

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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 Aviation Safety Agency (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

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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 related 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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Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

ELAPSED TIME (HOURS) 2.50

Additional manhours related 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 related 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

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**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

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**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, online through the SB Reporting service or alternatively by fax to :

SEDOR4 - AIRBUS Customer Services Technical Data

Fax No.: (33) 5 61 93 28 06

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

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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

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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

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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

Tel : (33) 5 67 19 06 22

E-mail : monitored.retrofit@airbus.com

Fax : (33) 5 61 93 27 45

C. LIST OF COMPONENTS

No Kit

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177

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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

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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. LA2K1-27-015 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

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DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177

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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

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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

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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

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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).

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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

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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

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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

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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

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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

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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

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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

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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

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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

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**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

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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

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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 concerned (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

FAX: (+33) 5 61 93 28 06

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

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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

FAX : (33) 5 61 93 42 51

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

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