# @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. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 27 

### TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC P12AM21A 2K1 FOR A330-200/300 AND FCPC M21A 2K0 FOR A330-300 BASIC A/C WITH MECHANICAL RUDDER **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 55440S18650 200360S30853 200359S30852 201687S31873 201688S31874 MINOR None NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES When there are significant differences between all airspeed sources, the flight controls revert to alternate law, the autopilot (AP) and the autothrust (A/THR) automatically disconnect and the Flight Directors (FD) bars are automatically removed. It has been identified that, after such an event, if two airspeed sources become similar while still erroneous, the flight guidance computers: - Display FD Bars again. - Enable autopilot and autothrust re-engagement. However, in some cases, the autopilot orders may be inappropriate, such as possible abrupt pitch command. To address these inappropriate orders, operational recommendations were issued beginning of January 2011 in red OEB 35 (formerly OEB 82/1 up until 2011) and it is associated OEB PROC 35 (formerly OEB 82 up until 2011) in the Quick Reference Handbook (QRH). This Service Bulletin is published to advise all operators of A330 aircraft of the issue of AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 and/or LA2K0-27-023. DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 1 5

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# @A330 SERVICE BULLETIN SUMMARY This Service Bulletin recommends either replacing the existing FCPCs with hardware 2K1 and 2K0 by FCPCs with hardware 2K1, 2K0 and new standard P12A/M21A or modifying the existing FCPCs with hardware 2K1 and 2K0 into new standard P12A/M21A by means of On-Board Replaceable Modules (OBRMs) as per AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 and/or LA2K0-27-023. New software standard P12A/M21A on FCPC 2K1 and 2K0 hardware has been defined to take into account the last FCPC software evolutions. The main FCPC improvements are: - Inhibit autopilot engagement under unreliable airspeed condition in the here above situation described in FOT Ref.999.0112/10 dated on 20 December 2010, - Improvement of aircraft behavior in case of erratic ADIRU outputs, - Improvement of the reconfiguration logics in case of electrical transients during rotation at take off (TFU No. 27.90.00.035), - Improvement of the Ground Spoiler (GS) and Partial Lift Damping (PLD) logics, - Reduction of high Vertical Speed (VZ) at touchdown with new parameters recording in the Digital Flight Data Recorder (DFDR), - Improvement of aircraft behaviour in case of two consistently erroneous Angle Of Attack (AOA) information: limitation of Trimmable Horizontal Stabilizer (THS) at pitch-up. Accomplishment of this Service Bulletin will cancel the red OEB 35 (formerly OEB 82/1 up until 2011) and the Airplane Flight Manuel (AFM) TR 149 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 5

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# @A330 SERVICE BULLETIN SUMMARY **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA02 1 See SB FCPCs **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA03 1 See SB FCPCs EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

ACA ACI AEA AFR AGC ALK AZA BEL BER BMA BTV CPA CRL CYP DGA EDW EIN EVA FWI GFA GIA GRL HDA HFY HVN IAC JST KAL KKK MAS MON OHY PAL QAF QTR RSY SAS SWR TAM TAP TCX THA THY TSC UAE USA VKG VLK VOZ XAX XLF CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification(s): Service Bulletin No. A330-27-3132 Mod. No. 49965S16501 51341S16795 53503S18051 53504S18052 A330-31-3048 49632S16354 REFERENCES / REPERCUSSIONS TFU 27.90.00.035 OEB 23 35 AOT None SIL 00-022 LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER FOT Ref. 999.0112/10 dated 20 December 2010 OTHER OIT SE 999.0035/11 dated 28 April 2011 NATURE OF THE WORK AIRCRAFT NO

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 3 5

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# @A330 SERVICE BULLETIN SUMMARY EQUIPMENT YES HARD YES SOFT NO OBRM YES MANPOWER **CONF 001 Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming of their OBRMs. TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 Additional manhours 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 REVISION No.: 00 - Dec 21/11 Page: 4 5

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# @A330 SERVICE BULLETIN SUMMARY Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming of their OBRMs. In the Main Rack 800VU and on the FWD Shelf 915VU, modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs. AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-023 Task 273177-831-802-001: Modification by replacement of the three FCPCs. TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 APPENDICES **CONF ALL None

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 5 5

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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 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 27 

### TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC P12AM21A 2K1 FOR A330-200/300 AND FCPC M21A 2K0 FOR A330-300 BASIC A/C WITH MECHANICAL RUDDER MODIFICATION No.: 55440S18650 200360S30853 200359S30852 201687S31873 201688S31874 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE: These modifications are applicable by Service Bulletin only. NOTE: This Service Bulletin is only applicable to aircraft on which Mod. No. 49144S16279 (INSTALL RUDDER FLY-BY WIRE ON A330/A340) is not embodied. (1) Models 330-202 330-203 330-223 330-243 330-301 330-321 330-322 330-323 330-341 330-342 330-343 (2) Effectivity by MSN 0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0069-0073 0077 0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116 0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288
DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 1 5

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# @A330 SERVICE BULLETIN

0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522 0525-0527 0529-0530 0532 0535-0536 0539 0548 0550-0551 0565 0567-0568 0581 0584 0597 0627 0635 0657 (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0461 0551 0597 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 AGC 0324 ALK 0303 0306 0311 0313 0404 0627 AZA 0272 0339 BEL 0030 0037 0045 0082 0095 0229 BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 BMA 0398 0401 BTV 0205 0330 CPA 0012 0017 0071 0102 0113 0118 0121 0155 0244 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 CRL 0285 0320 CYP 0505 0526 DGA 0240 EDW 0291 EIN 0269 0397 EVA 0530 0535 FWI 0253 GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 GIA 0138 0140 0144 0148 0153 0165 GRL 0230 HDA 0083 0099 0106 0109 0234 0405 0479 0512 0581 HFY 0096 0211 HVN 0255 0262 0275 0294 0299 0366 IAC 0353 0362 JST 0506 0508 0513 0522 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0425 0428 0484 0490 0550

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 2 5

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# @A330 SERVICE BULLETIN

OPERATOR MSN KKK 0343 0358 0364 MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300 MON 0261 0265 OHY 0072 0087 0098 0143 PAL 0183 0184 0188 0189 0191 0198 0200 0203 QAF 0487 QTR 0441 0473 0489 0511 0521 RSY 0171 SAS 0496 0497 0515 0568 SWR 0249 TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 TAP 0181 0195 0223 0305 0308 0312 0317 TCX 0254 0266 0301 0427 0456 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 THY 0463 0504 TSC 0111 0132 0177 0250 0271 0369 0407 0480 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382 0384 0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509 0518 0525 0536 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 VKG 0309 0349 0356 0357 VLK 0055 0070 0086 VOZ 0365 0372 XAX 0054 XLF 0501 0635 (4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064 0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083 0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109 0110 0112 0113 0116 0118 0119 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177 0183 0184 0188 0189 0191 0198 0200 0203 0206 0209 0219 0224 0231 0234 0241 0244 0256 0267 003

0111 0277 0279 0284 002 003

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 3 5

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# @A330 SERVICE BULLETIN

MSN CONFIGURATION 0181 0195 0205 0211 0222 0223 0226 0229 0230 0232 0238 0240 0247 0248 0249 0250 0251 0253 0254 0255 0258 0259 0261 0262 0265 0266 0269 0271 0272 0275 0276 0281 0283 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328 0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345 0346 0348 0349 0350 0351 0356 0357 0358 0361 0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403 0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422 0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487 0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513 0515 0516 0518 0519 0521 0522 0525 0526 0527 0529 0530 0532 0535 0536 0539 0548 0550 0551 0565 0567 0568 0581 0584 0597 0627 0635 0657 002

0353 0362 001 002 (5) Configuration definition **CONF 001 Config. 001 is valid for aircraft on which Service Bulletin No. A330-27-3080 (Mod. No. 47735S14929) is embodied and on which Service Bulletin No. A330-27-3079 (Mod. No. 47587S14930) and Service Bulletin No. A330-27-3144 (Mod. No. 55440S18650) are not embodied. **CONF 002 Config. 002 is valid for aircraft on which Service Bulletin No. A330-27-3080 (Mod. No. 47735S14929) and Service Bulletin No. A330-27-3144 (Mod. No 55440S18650) are embodied and on which Service Bulletin No. A330-27-3079 (Mod. No. 47587S14930) is not embodied. **CONF 003 Config. 003 is valid for aircraft on which Service Bulletin No. A330-27-3079 (Mod. No. 47587S14930 and Service Bulletin No. A330-27-3144 (Mod. No. 55439S18649) are embodied and on which Service Bulletin No. A330-27-3080 (Mod. No. 47735S14929) is not embodied. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Equipment BFEA01 1

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 4 5

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# @A330 SERVICE BULLETIN

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

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 5 5

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# @A330 SERVICE BULLETIN This Service Bulletin recommends either replacing the existing FCPCs with hardware 2K1 and 2K0 by FCPCs with hardware 2K1, 2K0 and new standard P12A/M21A or modifying the existing FCPCs with hardware 2K1 and 2K0 into new standard P12A/M21A by means of On-Board Replaceable Modules (OBRMs) as per AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 and/or LA2K0-27-023. (3) Advantages New software standard P12A/M21A on FCPC 2K1 and 2K0 hardware has been defined to take into account the last FCPC software evolutions. The main FCPC improvements are: - Inhibit autopilot engagement under unreliable airspeed condition in the here above situation described in FOT Ref.999.0112/10 dated on 20 December 2010, - Improvement of aircraft behavior in case of erratic ADIRU outputs, - Improvement of the reconfiguration logics in case of electrical transients during rotation at take off (TFU No. 27.90.00.035), - Improvement of the Ground Spoiler (GS) and Partial Lift Damping (PLD) logics, - Reduction of high Vertical Speed (VZ) at touchdown with new parameters recording in the Digital Flight 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 REVISION No.: 00 - Dec 21/11 Page: 6 5

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# @A330 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 REVISION No.: 00 - Dec 21/11 Page: 7 5

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# @A330 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 5

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# @A330 SERVICE BULLETIN
Task 273177-831-801-001: Modification of the three FCPCs by replacement or reprogramming of their OBRMs. ELAPSED TIME (HOURS) 2.50 Additional manhours 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 REVISION No.: 00 - Dec 21/11 Page: 9 5

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# @A330 SERVICE BULLETIN

**CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Airworthiness Directive (AD) Airworthiness Directive No. 2010-0271 Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-97-00 27-93-34 27-96-00 31-51-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-27-3079 A330-27-3080 A330-27-3132 A330-27-3144 A330-31-3048 Service Information Letter (SIL) SIL 00-022 Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 **CONF 002 Airworthiness Directive (AD) Airworthiness Directive No. 2010-0271 Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-97-00 27-93-34 27-96-00 31-51-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-27-3079 A330-27-3080 A330-27-3132 A330-27-3144 A330-31-3048 Service Information Letter (SIL) SIL 00-022 Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 10 5

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# @A330 SERVICE BULLETIN

**CONF 003 Airworthiness Directive (AD) Airworthiness Directive No. 2010-0271 Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-97-00 27-93-34 27-96-00 31-51-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-27-3079 A330-27-3080 A330-27-3132 A330-27-3144 A330-31-3048 Service Information Letter (SIL) SIL 00-022 Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-023 **CONF ALL K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 27-93-00 Aircraft Wiring List (AWL) Flight Crew Operating Manuel (FCOM) Flight Manual (FM) Illustrated Parts Catalog (IPC) 27-93-08 Master Minimum Equipment List (MMEL) This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in advance, in case you need your operational documentation to be amended by a revision priorto 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 REVISION No.: 00 - Dec 21/11 Page: 11 5

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# @A330 SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES FCPC LA2K1A100DA0000 LA2K1A100DE0000 03 NO (1) (2) (3) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. NOTE (1): On non-enhanced A330-300 aircraft model, FCPC standard M21A 2K0 (PN LA2K01500AE0000) is interchangeable with FCPC standard P12A/M21A 2K1 (PN LA2K1A100DE0000) and interchangeable and mixable with FCPC standard P11A/M20A 2K2 (PN LA2K2B100DF0000). NOTE (2): On non-enhanced A330-200 aircraft model, FCPC standard P12A/M21A 2K1 (PN LA2K1A100DE0000) is interchangeable and mixable with FCPC standard P11A/M20A 2K2 (PN LA2KB100DF0000). NOTE (3): Interchangeability code 03 becomes 01 provided that the three FCPCs are replaced at the same time. Mixability not authorized. Replacement of the three FCPCs has to be done simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph C. ofthis 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. ofthis Service Bulletin. DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 12 5

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# @A330 SERVICE BULLETIN

**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. ofthis Service Bulletin. NOTE (2): On non-enhanced A330-300 aircraft model, FCPC standard M21A 2K0 (PN LA2K01500AE0000) is interchangeable with FCPC standard P12A/M21A 2K1 (PN LA2K1A100DE0000) and interchangeable and mixable with FCPC standard P11A/M20A 2K2 (PN LA2K2B100DF0000). NOTE (3): On non-enhanced A330-200 aircraft model, FCPC standard 2K0 cannot be installed. **CONF ALL M. SPARES FCPC LA2K01500AC0000 FCPC LA2K1A100DA0000 FCPC LA2K1A100DC0000

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 13 5

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# @A330 SERVICE BULLETIN

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# @A330 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 REVISION No.: 00 - Dec 21/11 Page: 15 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 LA2K1A100DE0000 3 FCPC LA2K1A100DA0000 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Modification of removed equipment should be negotiated directly with AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin No. LA2K1-27-015. Equipment BFEA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES LA2K1A100DE0000 3 FCPC LA2K1A100DC0000 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Modification of removed equipment should be negotiated directly with AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin No. LA2K1-27-015. Equipment BFEA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES LA2K01500AE0000 3 FCPC LA2K01500AC0000 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Modification of removed equipment should be negotiated directly with AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin No. LA2K0-27-023. E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 16 5

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# @A330 SERVICE BULLETIN

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 REVISION No.: 00 - Dec 21/11 Page: 17 5

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# @A330 SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 273177-831-801-001 - Modification of the three FCPCs by replacement or reprogramming of their OBRMs. WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. CAUTION: REFER TO AMM 20-15-00, Page Block 201 AND AIRBUS SIL 00-022 FOR ELECTROSTATIC DISCHARGE PRECAUTIONS. NOTE: This Task concerns the modification of the FCPCs by replacement or by reprogramming of theirs OBRMs. Task Associated Data **CONF 001 Zone 120 Modified FIN 2CE1 2CE2 2CE3 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 Additional manhours related to Vendor SB; refer to: AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 **CONF 002 Zone 120

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 19 5

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# @A330 SERVICE BULLETIN

Modified FIN 2CE1 2CE2 2CE3 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 Additional manhours related to Vendor SB; refer to: AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015 **CONF 003 Zone 120 Modified FIN 2CE1 2CE2 2CE3 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 Additional manhours related to Vendor SB; refer to: AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-023 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 273177-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 273177-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 20 5

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# @A330 SERVICE BULLETIN

**CONF 003 (1) Subtask 273177-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 273177-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-93-34-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801). **CONF 002 (1) Subtask 273177-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-93-34-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 21 5

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# @A330 SERVICE BULLETIN

**CONF 003 (1) Subtask 273177-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-93-34-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 273177-831-001-003 - In the Main Rack 800VU and on the FWD Shelf 915VU, modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs. Work Zones and Access Panels Zone Access/Work location 120 References Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801 Task 27-93-34-400-801 Task 27-96-00-740-807 Task 31-51-00-610-802 Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K1-27-015 (a) Before replacement or reprogramming of the OBRMs: 1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the OFF and FAULT legends of this (these) pushbutton switch(es) is (are) off). 2 Do the BITE test of the EFCS (LRU IDENT), (Refer to AMM Task 27-96-00-740-807) and make sure that the old P/N of the FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015). NOTE: Print the LRU IDENTIFICATION page (if the printer is not available, a visual check is acceptable).

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 22 5

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# @A330 SERVICE BULLETIN

3 Open, safety/lock and tag the circuit breakers specified as per removal of the Flight control Primary Computer (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801). 4 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-015. 5 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801). (b) OEB cancellation: 1 On A/C equipped with OEB REMINDER function, if the ECAM warning has been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the following codes should be deleted from the FWC database. CODE WARN STS 34/10/050/061 YES NO 34/10/060/063 YES NO 34/10/070/065 YES NO 34/10/020/055 YES NO 34/10/030/057 YES NO 34/10/040/059 YES NO Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from FWCs using MCDUs". **CONF 002 (1) Subtask 273177-831-001-004 - In the Main Rack 800VU and on the FWD Shelf 915VU, modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs. Work Zones and Access Panels Zone Access/Work location 120 References Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801 Task 27-93-34-400-801 Task 27-96-00-740-807 Task 31-51-00-610-802 Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K1-27-015 (a) Before replacement or reprogramming of the OBRMs: 1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the OFF and FAULT legends of this (these) pushbutton switch(es) is (are) off).

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 23 5

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# @A330 SERVICE BULLETIN

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 5

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# @A330 SERVICE BULLETIN (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

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# @A330 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 22-97-00-740-801 Task 27-93-34-000-801 Task 27-93-34-400-801 Task 27-96-00-740-802 Task 27-96-00-740-807 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 5

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# @A330 SERVICE BULLETIN (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 5

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# @A330 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 5

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# @A330 SERVICE BULLETIN

**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 5

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# @A330 SERVICE BULLETIN

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DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 30 5

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# @A330 SERVICE BULLETIN Task 273177-831-802-001 - Modification by replacement of the three FCPCs. **CONF ALL WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. NOTE: This Task concerns the replacement of the three FCPCs. Task Associated Data **CONF 001 Zone 120 Modified FIN 2CE1 2CE2 2CE3 Manpower TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 **CONF 002 Zone 120 Modified FIN 2CE1 2CE2 2CE3 Manpower TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 31 5

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# @A330 SERVICE BULLETIN

**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 5

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# @A330 SERVICE BULLETIN

**CONF ALL B. PREPARATION **CONF 001 (1) Subtask 273177-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-93-34-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801). **CONF 002 (1) Subtask 273177-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-93-34-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801). **CONF 003 (1) Subtask 273177-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-93-34-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802).

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 33 5

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# @A330 SERVICE BULLETIN (b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 273177-960-002-001 - In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES LA2K1A100DE0000 3 FCPC NOTE: Modification of removed equipment should be negotiated directly with AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin No. LA2K1-27-015. References Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801 Task 27-93-34-400-801 Task 31-51-00-610-802 (a) Replacement of the FCPCs: 1 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1): Refer to AMM Task 27-93-34-000-801 FIN 2CE1 1 FCPC LA2K1A100DA0000 2 On the FWD Shelf 915VU, install the FCPC (FIN 2CE1): Refer to AMM Task 27-93-34-400-801

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 34 5

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# @A330 SERVICE BULLETIN

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 5

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# @A330 SERVICE BULLETIN
Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES LA2K1A100DE0000 3 FCPC NOTE: Modification of removed equipment should be negotiated directly with AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin No. LA2K1-27-015. References Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801 Task 27-93-34-400-801 Task 31-51-00-610-802 (a) Replacement of the FCPCs: 1 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1): Refer to AMM Task 27-93-34-000-801 FIN 2CE1 1 FCPC LA2K1A100DC0000 2 On the FWD Shelf 915VU, install the FCPC (FIN 2CE1): Refer to AMM Task 27-93-34-400-801 FIN 2CE1 1 FCPC LA2K1A100DE0000 3 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3): Refer to AMM Task 27-93-34-000-801 FIN 2CE2 1 FCPC LA2K1A100DC0000 and FIN 2CE3 1 FCPC LA2K1A100DC0000 4 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3): Refer to AMM Task 27-93-34-400-801 DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 36 5

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# @A330 SERVICE BULLETIN

FIN 2CE2 1 FCPC LA2K1A100DE0000 and FIN 2CE3 1 FCPC LA2K1A100DE0000 (b) OEB cancellation: 1 On A/C equipped with OEB REMINDER function, if the ECAM warning has been flagged as described in OEB 23 (formerly OEB 74 up until 2011), the following codes should be deleted from the FWC database. CODE WARN STS 34/10/050/061 YES NO 34/10/060/063 YES NO 34/10/070/065 YES NO 34/10/020/055 YES NO 34/10/030/057 YES NO 34/10/040/059 YES NO Refer to AMM Task 31-51-00-610-802 "Delete OEB REMINDER data from FWCs using MCDUs". **CONF 003 (1) Subtask 273177-960-002-003 - In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES LA2K01500AE0000 3 FCPC NOTE: Modification of removed equipment should be negotiated directly with AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin No. LA2K0-27-023.

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 37 5

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# @A330 SERVICE BULLETIN

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

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# @A330 SERVICE BULLETIN

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

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 39 5

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# @A330 SERVICE BULLETIN

**CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 273177-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in installation of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801). (c) Remove the access platform(s). (d) Restore the systems and the aircraft to normal operating condition. **CONF 002 (1) Subtask 273177-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in installation of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801). (c) Remove the access platform(s). (d) Restore the systems and the aircraft to normal operating condition. **CONF 003 (1) Subtask 273177-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 40 5

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# @A330 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in installation of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801). (c) Remove the access platform(s). (d) Restore the systems and the aircraft to normal operating condition.

DATE: Dec 21/11 SERVICE BULLETIN No.: A330-27-3177 REVISION No.: 00 - Dec 21/11 Page: 41 5

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC P12AM21A 2K1 FOR A330-200/300 AND FCPC M21A 2K0 FOR A330-300 BASIC A/C WITH MECHANICAL RUDDER MODIFICATION No.: 55440S18650 200360S30853 200359S30852 201687S31873 201688S31874 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft 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 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 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 5

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