@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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC STD P11AM20A

2K2 ON A330 AIRCRAFT FAMILY

MODIFICATION No.: 200360S30853 200359S30852 201654S31872

This page transmits Revision No.02 of Service Bulletin No.A330-27-3176

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 02 issued to modify the validity of Config. 001, Config. 002 and Config. 003.

CHANGES

FRONT MATTER

FLIGHT CONTROLS - FCPC -

INTRODUCE NEW FCPC STD

P11AM20A 2K2 ON A330 AIRCRAFT

FAMILY

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 003 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REASON

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 273176- 831-801-001-Modification

of the three FCPCs (FINs 2CE1, 2CE2

and 2CE3) by replacement or

reprogramming of their OBRMs

Subtask 273176-831-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

TASK 273176- 831-802-001-Replacement

of the three FCPCs (FINs 2CE1, 2CE2

and 2CE3)

Subtask 273176-960-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES 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

Revision No. 01 issued to:

create new Config. 002 and Config. 003 valid for aircraft post Service Bulletin No. A330-27-3144,

increase the effectivity with aircraft concerned by the Service Bulletin No. A330-27-3144,

new Mod. No. 200360S30853 and 200359S30852 added,

update the aircraft operation affected,

apply minor changes.

REVISION SEQUENCE

ORIGINAL: Jul 26/11

REVISION No. : 01 - Mar 27/12

REVISION No. : 02 - Apr 24/12

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 2

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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.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC STD P11AM20A

2K2 ON A330 AIRCRAFT FAMILY

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 200360S30853 200359S30852 201654S31872

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.

To address this aircraft behaviour, 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).

New Flight Control Primary Computer (FCPC) standards have been developed in order to inhibit

autopilot engagement in the here above situation described in FOT Ref.999.0112/10 dated 20

December 2010.

New software standard P11A/M20A on FCPC 2K2 hardware has been defined to take into account the

last FCPC software evolution.

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

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

FRANCE SAS Service Bulletin No. LA2K2-27-016.

This Service Bulletin recommends either replacing the existing FCPCs with hardware 2K2 by FCPCs

with hardware 2K2 and new standard P11A/M20A, or modifying the existing FCPCs with hardware 2K2

into new standard P11A/M20A by means of On-Board Replaceable Modules (OBRMs) as per AIRBUS

FRANCE SAS Service Bulletin No. LA2K2-27-016.

Accomplishment of this Service Bulletin allow the possibility for aircraft on which standard P10M19 2K1

or M19 2K0 are installed to upgrade to P11A/M20A 2K2 standard as per replacement by Aircraft

Maintenance Manual (AMM).

Accomplishment of this Service Bulletin will inhibit autopilot engagement under unreliable airspeed

condition.

Accomplishment of this Service Bulletin will cancel the red OEB 35 (formerly OEB 82/1 up until 2011)

and Flight Manual (FM) TR 149 mandated by EASA Airworthiness Directive No. 2010-0271, refer to

EASA Airworthiness Directive No. 2011-0199R1 for cancellation of operational limitation.

Accomplishment of this Service Bulletin for Config. 002 and Config. 003 will also cancel the red OEB

23 (formerly OEB 74 up until 2011) and Flight Manual (FM) TR 4.02.00/46 mandated by EASA

Airworthiness Directive No. 2009-0012E, refer to EASA Airworthiness Directive No. 2011-0199R1 for

cancellation of operational limitation.

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 FCPC

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA02 1 See SB FCPC

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA03 1 See SB FCPC

EFFECTIVITY

**CONF ALL

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

11S 46W AAR AAW ACA ACI AEA AFL AFR ALK ASY AVA AZA

BEC BEL BER BMA BTV CAL CCA CES CHH CPA CRK CRL CSC

CSN DAH DAL DGA DLH EDW EIN ETD EVA FIN FST FWI GFA

GIA GRL HAL HDA HFY HVN IAC ISS IWD IYE JAI JAV JST

KAL KFR KKK KLM MAS MAU MEA MLR MON MSR OBS OHY OMA

PAL QAF QFA QTR RJA RSF RSY RYN SAA SAS SIA SVA SWR

TAM TAP TCX THA THY TSC UAE UAF USA VIR VKG VLK VOZ

XAX XLF

CONCURRENT REQUIREMENTS

**CONF 001

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

following Service Bulletin or the equivalent production modification:

Service Bulletin No. A330-27-3164 Mod. No. 200285S19541

**CONF 002

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

following Service Bulletin or the equivalent production modification:

Service Bulletin No. A330-27-3144 Mod. No. 55440S18650

**CONF 003

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

following Service Bulletin or the equivalent production modification:

Service Bulletin No. A330-27-3144 Mod. No. 55439S18649

REFERENCES / REPERCUSSIONS

**CONF ALL

TFU 27.90.00.035

OEB 23

35

AOT None

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

SUMMARY

SIL 00-022

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER FOT 999.0112/10 dated 20 December 2010

OTHER OIT 999.0035/11 dated 28 April 2011

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD YES

SOFT NO

OBRM YES

MANPOWER

**CONF 001

Task 273176-831-801-001: Modification of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs

TOTAL MANHOURS 1.50

ELAPSED TIME (HOURS) 1.50

Additional manhours related to Vendor SB; refer to:

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

replacement or reprogramming of their OBRMs

AIRBUS FRANCE SAS Service

Bulletin No. LA2K2-27-016

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 002

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 003

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

APPENDICES

**CONF ALL

None

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 4

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC STD P11AM20A

2K2 ON A330 AIRCRAFT FAMILY

MODIFICATION No.: 200360S30853 200359S30852 201654S31872

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: This modification is embodied before delivery on aircraft MSN 1136 , 1148 ,

1164 , 1175 , 1180 , 1238-1249 , 1251 and subsequent.

(1) Models

330-202 330-203 330-223 330-243 330-243F 330-301 330-302 330-303

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

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

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

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

0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558

0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588

0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618

0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650

0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688

0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718

0720-0722 0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747

0749-0752 0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782

0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811

0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863

0865-0869 0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901

0903-0909 0911 0913-0916 0918-0920 0922-0923 0925-0928 0930-0932 0934-0937

0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-1004

1006-1016 1018-1023 1025-1026 1028-1029 1031-1039 1041-1049 1051-1055

1057-1063 1065-1067 1069-1078 1080-1082 1084-1090 1092-1101 1103-1108 1110

1112 1114-1116 1118 1120 1123-1124 1126-1127 1129-1133 1135 1137-1138 1141

1143 1145-1147 1149-1151 1153 1155-1157 1159-1161 1163 1165 1167-1174

1177-1178 1181 1183-1184 1186-1193 1195-1196 1198-1206 1208-1229 1231-1237

1250

(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

11S 1053

46W 0871

AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211

AAW 0999 1043

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597 0733 0745 0749 0814 0931 0950

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232

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

0567 0584 0657

ALK 0303 0306 0311 0313 0404 0456

ASY 0747 0951 0969 1036 1183

AVA 0948 0967 1009 1016 1073 1208 1224

AZA 0272 0339 1123 1135 1218 1225

BEC 0863

BEL 0030 0037 0045 0082 0095 0229 0249

BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 0739

0828 0911

BMA 0398 0401

BTV 0205 0330

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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@A330

SERVICE BULLETIN

OPERATOR MSN

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920 1177 1206 1215

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187

1199 1216 1237

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830

0836 0851 0862 0866 0916 0928 0936 0942

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190

CPA 0012 0017 0071 0102 0113 0118 0121 0155 0244 0386 0389 0393

0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 0776

0850 0855 0895 0915 0959 1163 1196 1222

CRK 1031 1034 1039 1042 1051 1054 1059 1062 1115

CRL 0285 0320

CSC 1082 1138

CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964 1096 1116 1129 1202 1220 1233

DAH 0644 0647 0650 0653 0667

DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799

0806 0817 0827 0843 0857 0858 0859 0865

DGA 0240

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922 0989

EDW 0291 1193

EIN 0269 0397 0841 0847 0985 1025 1106

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852

0854 0868 0975 0991 1032 1070 1071 1081 1167 1205 1226

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755

FIN 0994 1007 1013 1023 1067 1078 1088 1173

FST 1033 1046

FWI 0253 0758 0965 1021

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052 1184 1214

GRL 0230

HAL 1104 1114 1171 1217

HDA 0083 0099 0106 0109 0234 0405 0479 0512 0581 0654 0662 0692

0716 0741 0786

HFY 0096 0211 1008

HVN 0262 0275 0294 0299 0366 0943 0962 1019

IAC 0353 0362

ISS 0665 0802 0822

IWD 0670 1097

IYE 0625 0632

JAI 0751 0807 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956

JAV 0255

JST 0506 0508 0513 0522 0842 0853 0940 0945 1198

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SERVICE BULLETIN

OPERATOR MSN

KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0425 0428 0484 0490 0550 1133 1155 1200 1203

KFR 0874 0891 0927 0939 0946

KKK 0343 0358 0364

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 0925 1161

MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300

1209 1219 1229 1234

MAU 0883 1057

MEA 0926 0984 0995 0998

MLR 0627

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143

OBS 0833

OHY 0072 0087 0098 0143

OMA 1038 1044 1049 1063 1093 1120 1227

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887 0892

0898 0976 1061 1094 1169 1174

QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659

0680 0684 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820

0826 0849 0893 0907 0918

RJA 0970 0979 1002

RSF 0980 0996 1235

RSY 0171

RYN 1231

SAA 1191 1210 1223 1236

SAS 0496 0497 0515 0568

SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099 1105

1107 1124 1132 1146 1149 1156 1157

SVA 1108 1127 1137 1141 1147 1153 1189 1192

SWR 0324 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0869 0876

0949 0961 0968 0977 1112 1118 1213 1221

TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934

TCX 0254 0266 0301

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

0990 1003 1035 1037 1060 1074 1086 1090

THY 0463 0504 0697 0704 0742 0754 0774 1004 1092 1150 1160 1170

1172 1204 1212 1228

TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 0795 0966 0971

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

UAF 1080 1186 1250

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041

1069 1076 1095 1100

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@A330

SERVICE BULLETIN

OPERATOR MSN

VIR 1195 1201

VKG 0309 0349 0356 0357

VLK 0055 0070 0086

VOZ 0365 0372

XAX 0054 0952 0974 1048 1066 1075 1126 1131 1165

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 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 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 0505

0507 0509 0510 0511 0512 0515 0516 0518 0519 0521 0525

0526 0527 0529 0530 0532 0535 0536 0539 0548 0550 0551

0565 0567 0568 0581 0584 0597 0627 0635 0657

002 003

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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MSN CONFIGURATION

0463 0504 0506 0508 0513 0522 0524 0533 0542 0549 0552

0553 0555 0558 0564 0570 0571 0573 0574 0576 0578 0579

0587 0588 0591 0593 0595 0600 0602 0603 0605 0607 0609

0610 0612 0614 0616 0618 0620 0621 0623 0625 0629 0631

0632 0633 0634 0636 0637 0638 0640 0641 0642 0644 0645

0647 0648 0649 0650 0652 0653 0654 0655 0656 0658 0659

0661 0662 0663 0664 0665 0666 0667 0669 0670 0671 0673

0674 0675 0676 0678 0679 0680 0682 0683 0684 0686 0687

0688 0690 0691 0692 0693 0695 0696 0697 0699 0700 0701

0703 0704 0705 0707 0708 0709 0711 0712 0713 0714 0716

0717 0718 0720 0721 0722 0724 0725 0726 0728 0729 0730

0732 0733 0734 0735 0737 0738 0739 0741 0742 0743 0745

0746 0747 0749 0750 0751 0752 0754 0755 0756 0758 0759

0760 0769 0770 0772 0773 0774 0776 0777 0778 0780 0781

0782 0784 0785 0786 0788 0789 0791 0792 0795 0796 0797

0799 0801 0802 0803 0805 0806 0807 0809 0810 0811 0813

0814 0815 0817 0818 0819 0820 0821 0822 0823 0824 0825

0826 0827 0828 0830 0831 0832 0833 0834 0836 0838 0839

0840 0841 0842 0843 0845 0847 0849 0850 0851 0852 0853

0854 0855 0857 0858 0859 0860 0861 0862 0863 0865 0866

0867 0868 0869 0871 0873 0874 0875 0876 0877 0879 0881

0882 0883 0884 0885 0887 0888 0889 0890 0891 0892 0893

0895 0896 0898 0899 0900 0901 0903 0904 0905 0906 0907

0908 0909 0911 0913 0914 0915 0916 0918 0919 0920 0922

0923 0925 0926 0927 0928 0930 0931 0932 0934 0935 0936

0937 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948

0949 0950 0951 0952 0954 0956 0957 0958 0959 0961 0962

0963 0964 0965 0966 0967 0968 0969 0970 0971 0973 0974

0975 0976 0977 0978 0979 0980 0982 0983 0984 0985 0986

0988 0989 0990 0991 0992 0994 0995 0996 0997 0998 0999

1000 1001 1002 1003 1004 1006 1007 1008 1009 1010 1011

1012 1013 1014 1015 1016 1018 1019 1020 1021 1022 1023

1025 1026 1028 1029 1031 1032 1033 1034 1035 1036 1037

1038 1039 1041 1042 1043 1044 1045 1046 1047 1048 1049

1051 1052 1053 1054 1055 1057 1058 1059 1060 1061 1062

1063 1065 1066 1067 1069 1070 1071 1072 1073 1074 1075

1076 1077 1078 1080 1081 1082 1084 1085 1086 1087 1088

1089 1090 1092 1093 1094 1095 1096 1097 1098 1099 1100

1101 1103 1104 1105 1106 1107 1108 1110 1112 1114 1115

1116 1118 1120 1123 1124 1126 1127 1129 1130 1131 1132

1133 1135 1137 1138 1141 1143 1145 1146 1147 1149 1150

1151 1153 1155 1156 1157 1159 1160 1161 1163 1165 1167

1168 1169 1170 1171 1172 1173 1174 1177 1178 1181 1183

1184 1186 1187 1188 1189 1190 1191 1192 1193 1195 1196

1198 1199 1200 1201 1202 1203 1204 1205 1206 1208 1209

1210 1211 1212 1213 1214 1215 1216 1217 1218 1219 1220

1221 1222 1223 1224 1225 1226 1227 1228 1229 1231 1232

1233 1234 1235 1236 1237 1250

001

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(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which FCPCs PN LA2K2B100DE0000 is installed.

**CONF 002

Config. 002 is valid for aircraft on which FCPCs PN LA2K1A100DC0000 is installed.

**CONF 003

Config. 003 is valid for aircraft on which FCPCs PN LA2K01500AC0000 is installed.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

**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

**CONF 001

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

the following Service Bulletin or the equivalent production modification:

Service Bulletin No. A330-27-3164 Mod. No. 200285S19541

**CONF 002

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

the following Service Bulletin or the equivalent production modification:

Service Bulletin No. A330-27-3144 Mod. No. 55440S18650

**CONF 003

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

the following Service Bulletin or the equivalent production modification:

Service Bulletin No. A330-27-3144 Mod. No. 55439S18649

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**CONF ALL

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.

To address this aircraft behaviour, 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).

New Flight Control Primary Computer (FCPC) standards have been developed in

order to inhibit autopilot engagement in the here above situation described in FOT

Ref.999.0112/10 dated 20 December 2010.

New software standard P11A/M20A on FCPC 2K2 hardware has been defined to take

into account the last FCPC software evolution.

(2) Objective/Action

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

AIRBUS FRANCE SAS Service Bulletin No. LA2K2-27-016.

This Service Bulletin recommends either replacing the existing FCPCs with hardware

2K2 by FCPCs with hardware 2K2 and new standard P11A/M20A, or modifying the

existing FCPCs with hardware 2K2 into new standard P11A/M20A by means of OnBoard Replaceable Modules (OBRMs) as per AIRBUS FRANCE SAS Service Bulletin

No. LA2K2-27-016.

Accomplishment of this Service Bulletin allow the possibility for aircraft on which

standard P10M19 2K1 or M19 2K0 are installed to upgrade to P11A/M20A 2K2 standard

as per replacement by Aircraft Maintenance Manual (AMM).

(3) Advantages

Accomplishment of this Service Bulletin will inhibit autopilot engagement under unreliable

airspeed condition.

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(4) Operational/Maintenance Consequences

Accomplishment of this Service Bulletin will cancel the red OEB 35 (formerly OEB

82/1 up until 2011) and Flight Manual (FM) TR 149 mandated by EASA Airworthiness

Directive No. 2010-0271, refer to EASA Airworthiness Directive No. 2011-0199R1 for

cancellation of operational limitation.

Accomplishment of this Service Bulletin for Config. 002 and Config. 003 will also cancel

the red OEB 23 (formerly OEB 74 up until 2011) and Flight Manual (FM) TR

4.02.00/46 mandated by EASA Airworthiness Directive No. 2009-0012E, refer to EASA

Airworthiness Directive No. 2011-0199R1 for cancellation of operational limitation.

D. DESCRIPTION

NOTE: To accomplish the Config. 001 of this Service Bulletin, two possibilities are

available:

- either modify the FCPCs described in TASK 273176-831-801 001

Modification of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs

- or replace them as described in TASK 273176-831-802 001 Replacement

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

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 273176-831-801-001: Modification of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs

(1) Modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or

reprogramming of their OBRMs

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

(1) Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

**CONF 002

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

(1) Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

**CONF 003

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

(1) Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

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**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.

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 273176-831-801-001: Modification of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs

Get Access 0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 1.50

ELAPSED TIME (HOURS) 1.50

Additional manhours related to Vendor SB; refer to:

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

by replacement or reprogramming of their OBRMs

AIRBUS FRANCE SAS Service

Bulletin No. LA2K2-27-016

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

Get Access 0.50

On Aircraft

Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3) 1.00

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Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 002

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

Get Access 0.50

On Aircraft

Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3) 1.00

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 003

Task 273176-831-802-001: Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

Get Access 0.50

On Aircraft

Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3) 1.00

Tests 1.00

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Airworthiness Directive (AD) Airworthiness Directive No.

2009-0012E

Airworthiness Directive No.

2010-0271

Airworthiness Directive No.

2011-0199R1

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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

Flight Manual (FM)

Service Bulletin (SB) A330-27-3164

Service Information Letter (SIL) SIL 00-022

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS Service

Bulletin No. LA2K2-27-016

**CONF 002

Airworthiness Directive (AD) Airworthiness Directive No.

2009-0012E

Airworthiness Directive No.

2010-0271

Airworthiness Directive No.

2011-0199R1

Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 27-93-34

31-51-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-55-00

Flight Manual (FM)

Service Bulletin (SB) A330-27-3144

Service Information Letter (SIL) SIL 00-022

**CONF 003

Airworthiness Directive (AD) Airworthiness Directive No.

2009-0012E

Airworthiness Directive No.

2010-0271

Airworthiness Directive No.

2011-0199R1

Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 27-93-34

31-51-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-55-00

Flight Manual (FM)

Service Bulletin (SB) A330-27-3144

Service Information Letter (SIL) SIL 00-022

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

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Flight Crew Operating Manual (FCOM)

Flight Manual (FM)

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

This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in

advance, in case you need your operational documentation to be amended by a revision prior

to Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to :

SEDOR4 - AIRBUS Customer Services Technical Data

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

E-mail: sb.reporting@airbus.com

SB Reporting service is accessible on-line through AIRBUS World from:

My on-line services’ section, available on all AIRBUS World 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).

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K2B100DE0000 LA2K2B100DF0000 03 NO (1)

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): When the old PN LA2K2B100DE0000 is removed, it may be replaced with the

new PN LA2K2B100DF0000 only if the complete set of old PN is replaced

with a set of new PN.

When the new PN LA2K2B100DF0000 is removed, it must be replaced with

the new PN.

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**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K1A100DC0000 LA2K2B100DF0000 03 NO (1)

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): When the old PN LA2K100DC0000 is removed, it may be replaced with the

new PN LA2K2B100DF0000 only if the complete set of old PN is replaced

with a set of new PN.

When the new PN LA2K2B100DF0000 is removed, it must be replaced with

the new PN.

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K01500AC0000 LA2K2B100DF0000 03 NO (1)

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): When the old PN LA2K01500AC0000 is removed, it may be replaced with the

new PN LA2K2B100DF0000 only if the complete set of old PN is replaced

with a set of new PN.

When the new PN LA2K2B100DF0000 is removed, it must be replaced with

the new PN.

**CONF ALL

M. SPARES

FCPC LA2K01500AC0000

FCPC LA2K1A100DC0000

FCPC LA2K2B100DE0000

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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 Modification of removed equipment should

be negotiated directly with AIRBUS

FRANCE SAS as per instructions given in

AIRBUS FRANCE SAS Service Bulletin No.

LA2K2-27-016.

Equipment BFEA02

Equipment BFEA03

Vendor parts are to be procured from:

AIRBUS OPERATIONS S.A.S

AVIONICS AND SIMULATION PRODUCTS

VENDOR CODE F6198

EYY - M6525 - 316, route de Bayonne

31060 TOULOUSE Cedex 09

FRANCE

Tel : (33) 5 61 93 55 55

Fax : (33) 5 61 18 04 94

Telex : AISPA 531546F

Email : systems.support@airbus.com

(2) Price and Availability

Equipment BFEA01

No Airbus kit will be provided.

Refer to the Vendor Service Bulletin AIRBUS FRANCE SAS Service Bulletin No.

LA2K2-27-016 for the equipment modification sales terms.

Equipment BFEA02

No AIRBUS kit will be provided.

Procurement terms for the equipment must be negotiated with the equipment supplier.

Equipment BFEA03

No AIRBUS kit will be provided.

Procurement terms for the equipment must be negotiated with the equipment supplier.

B. INDUSTRY SUPPORT INFORMATION

Refer to the Vendor Service Bulletin (AIRBUS FRANCE SAS Service Bulletin No.

LA2K2-27-016) for the industry support terms of the Vendor Service Bulletin parts and labor.

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Industry support terms for the equipment must be negotiated with the equipment supplier.

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

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

LA2K2B100DF0000 3 FCPC LA2K2B100DE0000 03

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

Common Support Data Dictionary (CSDD), Chapter 2.

Equipment BFEA02

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

NOTES

LA2K2B100DF0000 3 FCPC LA2K1A100DC0000 03

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

Common Support Data Dictionary (CSDD), Chapter 2.

Equipment BFEA03

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

NOTES

LA2K2B100DF0000 3 FCPC LA2K01500AC0000 03

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

Common Support Data Dictionary (CSDD), Chapter 2.

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 SAS Service Bulletin No. LA2K2-27-016.

(3) Special Tools

None

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This Page Intentionally Left Blank

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 273176-831-801-001 - Modification of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) 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 SIL 00-022 FOR

ELECTROSTATIC DISCHARGE PRECAUTIONS.

Task Associated Data

**CONF 001

Zone

120 211 212

Modified FIN

2CE1 2CE2 2CE3

Access

Door 811 831 841

Manpower

TOTAL MANHOURS 1.50

ELAPSED TIME (HOURS) 1.50

Additional manhours related to Vendor SB; refer to:

AIRBUS FRANCE SAS Service Bulletin No. LA2K2-27-016

**CONF 002

None

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**CONF 003

None

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 273176-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

(a) Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF 002

None

**CONF 003

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 273176-941-001-001 - 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) Put the access platform(s) in position.

(c) 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

None

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**CONF 003

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 273176-831-001-001 - 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 Access Door 811

Work location Electrical panel 800VU

Electrical panel 915VU

211 Access Door 831, Door 841

Work location Electrical panel 241VU

212 Access Door 831, Door 841

Work location Electrical panel 212VU

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 FRANCE SAS LA2K2-27-016

(a) Before replacement or reprogramming of the OBRMs:

1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure

that PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the

OFF and FAULT legends of this (these) pushbutton switch(es) 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 FRANCE SAS Service Bulletin No. LA2K2-27-016).

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

visual check is acceptable).

3 Open, safety/lock and tag the circuits breakers 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 FCPCs (FINs 2CE1, 2CE2 and 2CE3)

as per Vendor Service Bulletin No. LA2K2-27-016.

5 Remove the safety clips and/or tags and close/unlock these circuit breakers as

per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM

Task 27-93-34-400-801).

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**CONF 002

None

**CONF 003

None

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 273176-700-001-001 - 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 FRANCE SAS LA2K2-27-016

(a) After replacement or reprogramming of OBRMs:

1 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) 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).

2 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 correct

(Refer to AIRBUS FRANCE SAS Service Bulletin No. LA2K2-27-016).

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

a visual check is acceptable).

3 Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task

27-96-00-740-802).

4 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).

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

**CONF 002

None

**CONF 003

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 273176-942-002-001 - 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 the installation of the FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

**CONF 002

None

**CONF 003

None

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

This Page Intentionally Left Blank

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SERVICE BULLETIN

Task 273176-831-802-001 - Replacement of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

**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.

Task Associated Data

**CONF 001

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Access

Door 811

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 002

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Access

Door 811

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

**CONF 003

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Access

Door 811

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 273176-839-002-001 - 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 273176-839-002-001 - 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 003

(1) Subtask 273176-839-002-001 - 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: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 273176-941-002-001 - 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 273176-941-002-001 - 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 273176-941-002-001 - 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: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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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 273176-960-001-001 - Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K2B100DF0000 3 FCPC

References

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

Task 27-93-34-400-801

Task 31-51-00-610-802

(a) Remove :

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

FIN 2CE1

1 FCPC LA2K2B100DE0000

FIN 2CE2

1 FCPC LA2K2B100DE0000

FIN 2CE3

1 FCPC LA2K2B100DE0000

(b) Install :

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

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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FIN 2CE1

1 FCPC LA2K2B100DF0000

FIN 2CE2

1 FCPC LA2K2B100DF0000

FIN 2CE3

1 FCPC LA2K2B100DF0000

**CONF 002

(1) Subtask 273176-960-001-002 - Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K2B100DF0000 3 FCPC

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 Remove:

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

FIN 2CE1

1 FCPC LA2K1A100DC0000

and

FIN 2CE2

1 FCPC LA2K1A100DC0000

and

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

FIN 2CE3

1 FCPC LA2K1A100DC0000

2 Install:

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

FIN 2CE1

1 FCPC LA2K2B100DF0000

and

FIN 2CE2

1 FCPC LA2K2B100DF0000

and

FIN 2CE3

1 FCPC LA2K2B100DF0000

(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 273176-960-001-003 - Replace the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

Material necessary to do the job

Equipment BFEA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K2B100DF0000 3 FCPC

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 Remove:

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

FIN 2CE1

1 FCPC LA2K01500AC0000

and

FIN 2CE2

1 FCPC LA2K01500AC0000

and

FIN 2CE3

1 FCPC LA2K01500AC0000

2 Install:

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

FIN 2CE1

1 FCPC LA2K2B100DF0000

and

FIN 2CE2

1 FCPC LA2K2B100DF0000

and

FIN 2CE3

1 FCPC LA2K2B100DF0000

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

(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 273176-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Procedure:

1 Do the test after installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

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

**CONF 002

(1) Subtask 273176-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Procedure:

1 Do the test after installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

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

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

**CONF 003

(1) Subtask 273176-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Procedure:

1 Do the test after installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

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

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 273176-942-001-001 - 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 the installation of the FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

**CONF 002

(1) Subtask 273176-942-001-001 - 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 the installation of the FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

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SERVICE BULLETIN

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

**CONF 003

(1) Subtask 273176-942-001-001 - 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 the installation of the FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 34

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE NEW FCPC STD P11AM20A

2K2 ON A330 AIRCRAFT FAMILY

MODIFICATION No.: 200360S30853 200359S30852 201654S31872

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: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jul 26/11 SERVICE BULLETIN No.: A330-27-3176

REVISION No.: 02 - Apr 24/12 Page: 1

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