@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC M19 2K0 AND P10/M19 2K1.

MODIFICATION No.: 55439S18649 55440S18650

This page transmits Revision No.01 of Service Bulletin No.A330-27-3144

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to modify industry support information.

CHANGES

SUMMARY

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

DESCRIPTION DESCRIPTION UPDATED R

MANPOWER MANPOWER UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

MATERIAL INFORMATION

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Equipment

Equipement BFEA01 PART MATERIAL SET UPDATED

NOTE UPDATED

R

Equipement BFEA02 PART MATERIAL SET UPDATED

NOTE UPDATED

R

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

REVISION No.: 01 - Jul 16/09 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

ACCOMPLISHMENT INSTRUCTIONS

TASK 273144- 831-801-001-Modification TASK SOLUTION UPDATED

TASK TITLE UPDATED

R

TASK 273144- 831-802-001-Modification TASK SOLUTION UPDATED

TASK TITLE UPDATED

R

Subtask 273144-960-001-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

R

Subtask 273144-960-002-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Apr 02/09

REVISION No. : 01 - Jul 16/09

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

REVISION No.: 01 - Jul 16/09 Page: 2

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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.

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC M19 2K0 AND P10/M19 2K1.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 55439S18649 55440S18650

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

New software standards M19 and P10/M19 on the Flight Control Primary Computer (FCPC) 2K0 and

2K1 hardware were defined in order to take into account the last FCPC software evolutions.

This Service Bulletin is published to advise all operators of A330 aircraft of the issue of AIRBUS

FRANCE S.A.S. Service Bulletin No. LA2K0-27-019 and LA2K1-27-011.

Accomplishment of this Service Bulletin requires introducing new software M19 (PN

LA2K01500AC0000) or P10/M19 (PN LA2K1A100DC0000) on the three FCPCs by means of On-Board

Replaceable Module (OBRM) replacement or reprogramming or FCPCs replacement.

Accomplishment of this Service Bulletin introduces the following new functions and improvements :

- new elevator position monitoring,

- improvement of the monitoring of the flight control computer push button switches,

- improvement of the monitoring to detect jamming of the Trimmable Horizontal Stabilizer (THS)

actuator manual command,

- improvement of the double pressurization logic on the elevator,

- new monitoring to avoid mixability between FCPC standards,

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

REVISION No.: 01 - Jul 16/09 Page: 1

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SERVICE BULLETIN

SUMMARY

- modification for aircraft with mechanical rudder to allow speed brake extension with flaps fully

extended,

- Maximum Operating Speed/Maximum Operating Mach (VMO/MMO) and Autopilot (AP)

disconnection logic.

This Service Bulletin has for operational consequences the modification of the Flight Crew Operating

Manual (FCOM) Vol. 1 and Vol. 3 (due to the speed brake logic modification).

The "new elevator position monitoring" function, that allow to cancel red Operations Engineering Bulletin

(OEB) No. 50, will be active at aircraft level only if Mod. No. 55696S18546 (FLIGHT CONTROLS -

FCSC - INTRODUCE FCSC STD L20M19 FOR IN-SERVICE AIRCRAFT (Service Bulletin No.

A330-27-3145)) or Mod. No. 55697S18547 (FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD

L19M18 ON A330 AIRCRAFT (Service Bulletin No. A330-27-3146)) is associated with FCPC standard

M19 2K0 or P10/M19 2K1.

It is anticipated that an Airworthiness Directive (AD) will be issued to allow cancellation of this OEB No.

50.

After AD issuance, this Service Bulletin will cancel red OEB No. 50 and Aircraft Flight Manual

(AFM) Temporary Revision (TR) No. 4.02.00/25 if associated with FCSC L20M19 (Service Bulletin

No. A330-27-3145) or with FCSC L19M18 (Service Bulletin No. A330-27-3146). Operators having

programmed an OEB reminder should delete the reminder(s) from their system.

This Service Bulletin has for operational consequences the modification of the Flight Manual (FM) only

in case of FCPC/FCSC associations described above.

NOTE: Refer to Modification Operational Impact (MOI No. 55439 and MOI No. 55440) for

further details.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED 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

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB FCPC

Equipment BFEA02 1 See SB FCPC

EFFECTIVITY

This Service Bulletin is applicable to this (these) operator(s) :

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

SUMMARY

ACA ACI ADH AFR ALK BEL BMA CPA CRL CYP EDW EIN EVA

FWI GFA GIA GRL HDA HFY HVN IAC IWD JST KAL KKK LTU

LVG MAS MON MPD OBS PAL QAF QTR SAS SWR TAM TAP TCX

THA THY TSC UAE USA VKG VLK 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 :

Service Bulletin No. A330-27-3132 Mod. No. 49965S16501

51341S16795

53503S18051

53504S18052

A330-31-3048 49632S16354

REFERENCES / REPERCUSSIONS

TFU None

OEB 50

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD YES

SOFT NO

OBRM YES

MANPOWER

Task 273144-831-801-001: Modification

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In Avionics Compartment, in the Main Rack 800VU and on

the FWD Shelf 915VU, Modify the three FCPCs (FINs

2CE1, 2CE2 and 2CE3).

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K0-27-019

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K1-27-011

Task 273144-831-802-001: Modification

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.00

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

SUMMARY

APPENDICES

Appendix 1 : Elapsed Time Assumptions

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR20

915VU

800VU

2CE1

2CE2

2CE3

A

B

A

B

Z120

G_SB_273144_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

REVISION No.: 01 - Jul 16/09 Page: 6

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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

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC M19 2K0 AND P10/M19 2K1.

MODIFICATION No.: 55439S18649 55440S18650

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 0059-0060 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

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

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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@A330

SERVICE BULLETIN

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

ADH 0272 0339

AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657

ALK 0303 0306 0311 0313

BEL 0030 0037 0045 0082

BMA 0398 0401 0404

CPA 0012 0017 0071 0083 0099 0102 0109 0113 0118 0121 0155 0244

0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565

CRL 0285 0320

CYP 0505 0526

EDW 0369

EIN 0055 0059 0086 0269 0330 0397

EVA 0530 0535

FWI 0240 0253

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HDA 0098 0106 0132 0177 0234 0405 0407 0479 0512 0581

HFY 0096

HVN 0087 0255 0262 0275 0366

IAC 0353 0362

IWD 0072

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

KKK 0358 0364

LTU 0120 0127 0171 0403 0432 0444 0454 0469 0476 0493

LVG 0551 0597 0627

MAS 0067 0069 0073 0077 0095 0100 0107 0110 0116 0119 0143 0290

0296 0300

MON 0261 0265

MPD 0205 0211

OBS 0461

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

OPERATOR MSN

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487

QTR 0441 0473 0489 0511 0521

SAS 0496 0497 0515 0568

SWR 0229 0249 0288 0291 0294 0299 0322 0324 0343

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486

TAP 0181 0195 0223 0305 0308 0312 0317

TCX 0254 0266 0301 0309 0357 0427 0456

THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346

THY 0463 0504

TSC 0111 0250 0271 0480

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0365

0372 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 0349 0356

VLK 0070

XAX 0054

XLF 0501 0635

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0059 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 0111 0112 0113 0116 0118 0119 0120 0121 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 0223 0224 0226

0229 0230 0231 0232 0234 0238 0240 0241 0244 0247 0248

0249 0250 0251 0253 0254 0255 0256 0258 0259 0261 0262

0265 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281

0283 0284 0285 0286 0287 0288 0290 0291 0293 0294 0295

0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312

0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328

0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345

0346 0348 0349 0350 0351 0353 0356 0357 0358 0361 0362

0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384

0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403

0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422

0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448

0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466

0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487

0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0502

0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513

0515 0516 0518 0519 0521 0522 0525 0526 0527 0529 0530

0532 0535 0536 0539 0548 0550 0551 0565 0567 0568 0581

0584 0597 0627 0635 0657

001

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

Equipment BFEA02 1

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin or the equivalent production modification :

Service Bulletin No. A330-27-3132 Mod. No. 49965S16501

51341S16795

53503S18051

53504S18052

A330-31-3048 49632S16354

C. REASON

(1) History

New software standards M19 and P10/M19 on the Flight Control Primary Computer

(FCPC) 2K0 and 2K1 hardware were defined in order to take into account the last FCPC

software evolutions.

(2) Objective/Action

This Service Bulletin is published to advise all operators of A330 aircraft of the issue of

AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K0-27-019 and LA2K1-27-011.

(3) Advantages

Accomplishment of this Service Bulletin requires introducing new software M19 (PN

LA2K01500AC0000) or P10/M19 (PN LA2K1A100DC0000) on the three FCPCs by

means of On-Board Replaceable Module (OBRM) replacement or reprogramming or

FCPCs replacement.

Accomplishment of this Service Bulletin introduces the following new functions and

improvements :

- new elevator position monitoring,

- improvement of the monitoring of the flight control computer push button switches,

- improvement of the monitoring to detect jamming of the Trimmable Horizontal

Stabilizer (THS) actuator manual command,

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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- improvement of the double pressurization logic on the elevator,

- new monitoring to avoid mixability between FCPC standards,

- modification for aircraft with mechanical rudder to allow speed brake extension with

flaps fully extended,

- Maximum Operating Speed/Maximum Operating Mach (VMO/MMO) and Autopilot

(AP) disconnection logic.

(4) Operational/Maintenance Consequences

This Service Bulletin has for operational consequences the modification of the Flight

Crew Operating Manual (FCOM) Vol. 1 and Vol. 3 (due to the speed brake logic

modification).

The "new elevator position monitoring" function, that allow to cancel red Operations

Engineering Bulletin (OEB) No. 50, will be active at aircraft level only if Mod. No.

55696S18546 (FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L20M19

FOR IN-SERVICE AIRCRAFT (Service Bulletin No. A330-27-3145)) or Mod. No.

55697S18547 (FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L19M18

ON A330 AIRCRAFT (Service Bulletin No. A330-27-3146)) is associated with FCPC

standard M19 2K0 or P10/M19 2K1.

It is anticipated that an Airworthiness Directive (AD) will be issued to allow cancellation

of this OEB No. 50.

After AD issuance, this Service Bulletin will cancel red OEB No. 50 and Aircraft Flight

Manual (AFM) Temporary Revision (TR) No. 4.02.00/25 if associated with FCSC

L20M19 (Service Bulletin No. A330-27-3145) or with FCSC L19M18 (Service Bulletin

No. A330-27-3146). Operators having programmed an OEB reminder should delete the

reminder(s) from their system.

This Service Bulletin has for operational consequences the modification of the Flight

Manual (FM) only in case of FCPC/FCSC associations described above.

NOTE: Refer to Modification Operational Impact (MOI No. 55439 and MOI No.

55440) for further details.

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 273144-831-801 001 Modification ,

- or you replace them as described in TASK 273144-831-802 001

Modification .

To accomplish this Service Bulletin it is necessary to :

Task 273144-831-801-001: Modification

(1) In Avionics Compartment, in the Main Rack 800VU and on the FWD Shelf 915VU,

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

Modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).

Task 273144-831-802-001: Modification

(1) In Avionics Compartment, on the FWD Shelf 915VU, Replace the FCPC (FINs

2CE1).

(2) In Avionics Compartment, in the Main Rack 800VU, replace the two FCPCs (FINs

2CE2 and 2CE3).

E. COMPLIANCE

(1) Classification

RECOMMENDED

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

Task 273144-831-801-001: Modification

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 Avionics Compartment, in the Main Rack 800VU and

on the FWD Shelf 915VU, Modify the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3).

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K0-27-019

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K1-27-011

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

Task 273144-831-802-001: Modification

Get Access 1.00

On Aircraft

In Avionics Compartment, on the FWD Shelf 915VU,

Replace the FCPC (FINs 2CE1).

0.50

In Avionics Compartment, in the Main Rack 800VU,

replace the two FCPCs (FINs 2CE2 and 2CE3).

1.00

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.00

NOTE: For detail concerning elapsed time assumptions, refer to Appendix 1 : Elapsed

Time Assumptions .

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 12-34-24 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

Modification Operational Impact (MOI) MOI No. 55439

MOI No. 55440

Service Bulletin (SB) A330-27-3132

A330-27-3145

A330-27-3146

A330-31-3048

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K0-27-019

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K1-27-011

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

Flight Crew Operating Manual (FCOM) Vol. 1 Vol. 3

Illustrated Parts Catalog (IPC) 27-93-08 27-93-34

Modification Operational Impact (MOI) 55439

55440

Trouble Shooting Manual (TSM) 27-90-00

Aircraft Flight Manual (AFM) Temporary Revision (TR) No. 4.02.00/25

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

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 an

intermediate revision prior to Service Bulletin embodiment. For this purpose, please request

the intermediate revision by fax, telex or mail to :

SEDCC, AIRBUS - Customer Services Directorate

Fax No. : 33 (0) 5 61 93 28 06

Sita No. : TLSBP7X

E-mail : sb.reporting@airbus.com

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 Directorate (SEDCC).

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K01500AB0000 LA2K01500AC0000 03 NO (1) (2)

FCPC LA2K1A100DA0000 LA2K1A100DC0000 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 P10/M19 2K1

(PN LA2K1A100DC0000) is interchangeable and mixable with FCPC standard

M19 2K0 (PN LA2K01500AC0000) and interchangeable and mixable with

FCPC standard P9/M18 2K2 (PN LA2K2B100DB0000).

NOTE (3): On non-enhanced A330-200 aircraft model, FCPC standard P10/M19 2K1

(PN LA2K1A100DC0000) is interchangeable and mixable with FCPC standard

P9/M18 2K2 (PN LA2K2B100DB0000).

M. SPARES

FCPC LA2K01500AB0000

FCPC LA2K1A100DA0000

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Equipment BFEA01

Equipment BFEA02

This Service Bulletin is the subject of an

AIRBUS monitored retrofit campaign.

Vendor parts are to be procured from :

AIRBUS FRANCE S.A.S.

Avionics and simulation products

316, route de Bayonne

31060 TOULOUSE Cedex 09

FRANCE

Tel : (33) 5 61 93 55 55

Telex : AISPA 531546F

(2) Price and Availability

Equipment BFEA01

Refer to the vendor Service Bulletin No. LA2K0-27-019 for the equipment modification

sales terms.

Equipment BFEA02

Refer to the vendor Service Bulletin No. LA2K1-27-011 for the equipment modification

sales terms.

B. INDUSTRY SUPPORT INFORMATION

For the organisation 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

Modification of parts/equipment is at no charge for the operator. The manhours indicated in

this Service Bulletin will remain at the operators’ cost.

C. LIST OF COMPONENTS

No Kit

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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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

LA2K01500AC0000 3 FCPC LA2K01500AB0000 03 (1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Modification of removed equipment should be negotiated directly with

AIRBUS FRANCE S.A.S. as per instructions given in Service Bulletin No.

LA2K0-27-019.

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

LA2K1A100DC0000 3 FCPC LA2K1A100DA0000 03 (1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Modification of removed equipment should be negotiated directly with

AIRBUS FRANCE S.A.S. as per instructions given in Service Bulletin No.

LA2K1-27-011.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

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

FRANCE S.A.S. Service Bulletin No. LA2K0-27-019 or AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K1-27-011.

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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(3) Special Tools

None

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 273144-831-801-001 - Modification

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS

CONTAMINATION, REFER TO ESPM 20-55-00.

CAUTION: THE ELECTROSTATIC DISCHARGE PRECAUTIONS DESCRIBED IN ARINC

REPORT 606 ARE RECOMMENDED.

NOTE: This Task concerns the modification of the three FCPCs by replacement or

reprogramming of the OBRMs.

Task Associated Data

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Access

Door 811

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer

to:

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K0-27-019

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K1-27-011

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A. GENERAL

(1) Subtask 273144-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

(1) Subtask 273144-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

Task 27-93-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-869-002).

(b) Put access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the three FCPCs FINs

2CE1, 2CE2 and 2CE3 (Refer to AMM Task 27-93-34-000-801).

C. PROCEDURE

(1) Subtask 273144-831-001-001 - In Avionics Compartment, in the Main Rack 800VU and

on the FWD Shelf 915VU, Modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 800VU

Electrical panel 915VU

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-807

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. LA2K0-27-019

AIRBUS FRANCE S.A.S. LA2K1-27-011

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(a) 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).

(b) Do the Built-In Test Equipment (BITE) of the Electrical Flight Control System

(EFCS) (LRU IDENT) (Refer to AMM Task 27-96-00-740-807) and make sure that

the old PN of the FCPCs are :

LA2K01500AB0000 or LA2K1A100DA0000.

NOTE: Print the LRU IDENTIFICATION page (if the printer is not available,

a visual check is acceptable).

(c) Make sure that the circuit breaker defined in the removal of the FCPCs FINs 2CE1,

2CE2 and 2CE3 (Refer to AMM Task 27-93-34-000-801) are open, safetied and

tagged.

(d) In avionics compartment, 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.

Refer to AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K0-27-019 or AIRBUS

FRANCE S.A.S. Service Bulletin No. LA2K1-27-011

(e) Close the circuit breakers defined in the installation of the FCPCs FINs 2CE1,

2CE2 and 2CE3 (Refer to AMM Task 27-93-34-400-801).

D. TEST

(1) Subtask 273144-700-001-001 - 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

(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).

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(b) Do the BITE test of the EFCS (LRU IDENT) (Refer to AMM Task

27-96-00-740-807) and make sure that the new PN of the FCPCs are :

LA2K01500AC0000 or LA2K1A100DC0000

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 Category (CAT) 3 conditions, do the LAND CAT

III capability test (Refer to AMM Task 22-97-00-740-801).

(2) Subtask 273144-700-002-001 - Test After Cancellation of the OEB No. 50 (to be done if

new FCPCs are associated with FCSCs L20M19 or FCSCs L19M18).

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-51-00-610-802

(a) On aircraft equipped with OEB REMINDER function, if the Electronic Centralized

Aircraft Monitoring (ECAM) warning has been flagged as described in OEB No. 50,

the following codes should be deleted from the Flight Warning Computer (FWC)

database :

Refer to AMM Task 31-51-00-610-802 ("delete OEB REMINDER information from

FWCs using MCDUs")

CODE WARN STS

PRIM 1 FAULT

27/90/050/113

NO YES

PRIM 1 PITCH FAULT

27/90/200/109

NO YES

ELEV SERVO FAULT

27/30/050/083

NO YES

G SYS LO PR

29/11/060/091

NO YES

E. CLOSE-UP

(1) Subtask 273144-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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(a) 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).

(b) Remove the access platform(s).

(c) Restore the systems and the aircraft to normal operating condition.

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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Task 273144-831-802-001 - Modification

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS

CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: This Task concerns the replacement of the three FCPCs.

Task Associated Data

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Access

Door 811

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.00

A. GENERAL

(1) Subtask 273144-839-002-001 - 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: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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B. PREPARATION

(1) Subtask 273144-941-002-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

Task 27-93-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-869-002).

(b) Put access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the three FCPCs FINs

2CE1, 2CE2 and 2CE3 (Refer to AMM Task 27-93-34-000-801).

C. PROCEDURE

(1) Subtask 273144-960-001-001 - In Avionics Compartment, on the FWD Shelf 915VU,

Replace the FCPC (FINs 2CE1).

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 915VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K01500AC0000 1 FCPC (1)

NOTE (1): Modification of removed equipment should be negotiated directly with

AIRBUS FRANCE S.A.S. as per instructions given in Service Bulletin No.

LA2K0-27-019.

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Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K1A100DC0000 1 FCPC (1)

NOTE (1): Modification of removed equipment should be negotiated directly with

AIRBUS FRANCE S.A.S. as per instructions given in Service Bulletin No.

LA2K1-27-011.

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

(a) On the FWD shelf 915VU, remove :

Refer to AMM Task 27-93-34-000-801

FIN 2CE1

1 FCPC LA2K01500AB0000

or

FIN 2CE1

1 FCPC LA2K1A100DA0000

(b) On the FWD shelf 915VU, install :

Refer to AMM Task 27-93-34-400-801

FIN 2CE1

1 FCPC LA2K01500AC0000

or

FIN 2CE1

1 FCPC LA2K1A100DC0000

(2) Subtask 273144-960-002-001 - In Avionics Compartment, in the Main Rack 800VU,

replace the two FCPCs (FINs 2CE2 and 2CE3).

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 800VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

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SERVICE BULLETIN

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K01500AC0000 2 FCPC (1)

NOTE (1): Modification of removed equipment should be negotiated directly with

AIRBUS FRANCE S.A.S. as per instructions given in Service Bulletin No.

LA2K0-27-019.

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K1A100DC0000 2 FCPC (1)

NOTE (1): Modification of removed equipment should be negotiated directly with

AIRBUS FRANCE S.A.S. as per instructions given in Service Bulletin No.

LA2K1-27-011.

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

(a) In the main rack 800VU, remove :

Refer to AMM Task 27-93-34-000-801

FIN 2CE2

1 FCPC LA2K01500AB0000

and

FIN 2CE3

1 FCPC LA2K01500AB0000

or

FIN 2CE2

1 FCPC LA2K1A100DA0000

and

FIN 2CE3

1 FCPC LA2K1A100DA0000

(b) In the main rack 800VU, install :

Refer to AMM Task 27-93-34-400-801

FIN 2CE2

1 FCPC LA2K01500AC0000

and

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FIN 2CE3

1 FCPC LA2K01500AC0000

or

FIN 2CE2

1 FCPC LA2K1A100DC0000

and

FIN 2CE3

1 FCPC LA2K1A100DC0000

D. TEST

(1) Subtask 273144-700-003-001 - 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 three FCPCs FINs 2CE1, 2CE2 and 2CE3

(Refer to AMM Task 27-93-34-400-801).

(2) Subtask 273144-700-004-001 - Test After Cancellation of the OEB No. 50 (to be done if

new FCPCs are associated with FCSCs L20M19 or FCSCs L19M18).

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 31-51-00-610-802

(a) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB No. 50, the following codes should be deleted from

the FWC database :

Refer to AMM Task 31-51-00-610-802 ("delete OEB REMINDER information from

FWCs using MCDUs")

CODE WARN STS

PRIM 1 FAULT

27/90/050/113

NO YES

PRIM 1 PITCH FAULT

27/90/200/109

NO YES

ELEV SERVO FAULT

27/30/050/083

NO YES

G SYS LO PR

29/11/060/091

NO YES

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E. CLOSE-UP

(1) Subtask 273144-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

(a) 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).

(b) Remove the access platform(s).

(c) Restore the systems and the aircraft to normal operating condition.

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

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SERVICE BULLETIN

Appendix 1 : Elapsed Time Assumptions

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−27−3144

HOURS

MH ET PER

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

4.50

4.00

STEPS

1.00

1.00 1.00

1.00

1

1

0

IN ELECTRONICS PANEL 800VU

REPLACE FCPCs 2CE2 AND 2CE3

CLOSE−UP

GET ACCESS

TEST 1.00 1.00 1

1.00 1.00 1

2 4

0.50 0.50 1 ON SHELF 915VU

REPLACE FCPC 2CE1

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

G_SB_273144_5_AAAA_01_00

Figure A-FAAAA - Sheet 01

Elapsed Time Assumptions

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REPORTING SHEET

TITLE: FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC M19 2K0 AND P10/M19 2K1.

MODIFICATION No.: 55439S18649 55440S18650

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: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

REVISION No.: 01 - Jul 16/09 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- 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: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144

REVISION No.: 01 - Jul 16/09 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.