# @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 5

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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 5

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# @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. 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 5

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# @A330 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 REVISION No.: 01 - Jul 16/09 Page: 2 5

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# @A330 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 REVISION No.: 01 - Jul 16/09 Page: 3 5

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# @A330 SERVICE BULLETIN SUMMARY APPENDICES Appendix 1 : Elapsed Time Assumptions

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 4 5

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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 REVISION No.: 01 - Jul 16/09 Page: 5 5

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# @A330 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 5

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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 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 REVISION No.: 01 - Jul 16/09 Page: 1 5

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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 REVISION No.: 01 - Jul 16/09 Page: 2 5

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# @A330 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 REVISION No.: 01 - Jul 16/09 Page: 3 5

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# @A330 SERVICE BULLETIN (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 REVISION No.: 01 - Jul 16/09 Page: 4 5

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# @A330 SERVICE BULLETIN - 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 REVISION No.: 01 - Jul 16/09 Page: 5 5

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# @A330 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 REVISION No.: 01 - Jul 16/09 Page: 6 5

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# @A330 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 REVISION No.: 01 - Jul 16/09 Page: 7 5

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# @A330 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 REVISION No.: 01 - Jul 16/09 Page: 8 5

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# @A330 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 REVISION No.: 01 - Jul 16/09 Page: 9 5

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# @A330 SERVICE BULLETIN

D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components None (3) Equipment Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 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 REVISION No.: 01 - Jul 16/09 Page: 10 5

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# @A330 SERVICE BULLETIN (3) Special Tools None

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 11 5

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# @A330 SERVICE BULLETIN

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DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 12 5

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# @A330 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

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 13 5

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# @A330 SERVICE BULLETIN

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

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 14 5

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# @A330 SERVICE BULLETIN (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).

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 15 5

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# @A330 SERVICE BULLETIN (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

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 16 5

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# @A330 SERVICE BULLETIN (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 REVISION No.: 01 - Jul 16/09 Page: 17 5

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# @A330 SERVICE BULLETIN

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# @A330 SERVICE BULLETIN

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 REVISION No.: 01 - Jul 16/09 Page: 19 5

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# @A330 SERVICE BULLETIN

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.

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 20 5

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# @A330 SERVICE BULLETIN
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

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 21 5

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# @A330 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 DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 22 5

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# @A330 SERVICE BULLETIN

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

DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 23 5

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# @A330 SERVICE BULLETIN

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 REVISION No.: 01 - Jul 16/09 Page: 24 5

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# @A330 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

1.00 1.00 1 TEST 1.00 1.00 1

4 2 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 DATE: Apr 02/09 SERVICE BULLETIN No.: A330-27-3144 REVISION No.: 01 - Jul 16/09 Page: 1 5

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# @A330 SERVICE BULLETIN 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

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# @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

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