@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: 34

TITLE: NAVIGATION - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A330-34-3232

ADDITIONAL WORK

**CONF ALL

ADDITIONAL WORK is required by this revision for aircraft inspected by the original issue of this

Service Bulletin and with PN C16291AB installed.

The ADDITIONAL WORK is issued to ensure that the correct Serial Number (SN) of AOA Probe PN

C16291AB was installed.

No ADDITIONAL WORK is required for aircraft with PN C16291AA installed by the original issue of this

Service Bulletin.

REASON

Revision No. 01 issued to add Serial Number of Angle Of Attack PN C16291AB to be inspected.

NOTE: The original issue of this Inspection Service Bulletin was focusing on a batch of SN

having all the PN C16291AA. However, in the mean time, some units may have been

upgraded to PN C16291AB by THALES Service Bulletin C16291A-34-009 without fixing

the oil residue anomaly.

The ADDITIONAL WORK for this Service Bulletin is issue to also inspect PN

C16291AB. The batch is unchanged in terms of SN.

CHANGES

The main changes of the Revision No. 01 are:

- to add ADDITIONAL WORK for aircraft on which AOA Probes PN C16291AB are installed by the

original issue of this Service Bulletin,

- to add Config. 002 valid for aircraft on which AOA PN C16291AB is installed,

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- to modify Fig. A-FFAAA,

- to add Fig. A-FFBAA and Fig. A-FFAAB,

- to modify REASON paragraph,

- to update the effectivity.

FRONT MATTER

NAVIGATION - SENSORS, POWER

SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

APPENDICES APPENDICES UPDATED R

Fig. A-FSAAA FIGURE SOLUTION ADDED N

Fig. A-FSAAA Sheet 01 SHEET ADDED N

Fig. A-FSU FIGURE DELETED FOR APPLICABLE MSN D

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition CONFIGURATION LIST UPDATED R

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION ADDED N

REASON

Objective/Action OBJECTIVE/ACTION UPDATED R

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED

CONFIGURATION UPDATED

R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE ADDED N

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

REFERENCES REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

R

REFERENCED DOCUMENTATION ADDED N

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 2

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED R

Price and Availability PRICE AND AVAILABILITY UPDATED R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 343232- 832-801-001-Inspection TASK SOLUTION UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 343232-839-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-839-001-001 SUBTASK SOLUTION ADDED N

Subtask 343232-941-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-941-001-001 SUBTASK SOLUTION ADDED N

Subtask 343232-832-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIGURE REFERENCE UPDATED

FIN UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 343232-832-001-002 SUBTASK SOLUTION ADDED N

Subtask 343232-942-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

FIN UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-942-001-001 SUBTASK SOLUTION ADDED N

TASK 343232- 831-801-001-Replacement

of the THALES AOA Probes by Part

Number C16291AB whose SN is not listed

in THALES AVIONICS Service Bulletin

No. C16291A-34-007 Revision No. 01 (or

any later revision).

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 343232-839-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-839-003-001 SUBTASK SOLUTION ADDED N

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 343232-941-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-941-003-001 SUBTASK SOLUTION ADDED N

Subtask 343232-960-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 343232-960-002-002 SUBTASK SOLUTION ADDED N

Subtask 343232-700-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-700-002-001 SUBTASK SOLUTION ADDED N

Subtask 343232-942-007-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-942-007-001 SUBTASK SOLUTION ADDED N

TASK 343232- 831-802-001-Replacement

of the THALES AOA Probes by Part

Number C16291AA whose Serial Number

is not listed in the THALES VSB

C16291A-34-007 Revision No. 01 (or any

later revision).

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 343232-839-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-941-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-960-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

NOTE UPDATED

R

Subtask 343232-700-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-942-006-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 4

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

TASK 343232- 831-804-001-Replacement

of the THALES AOA Probes through

Airbus RFC/RMO Process.

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 343232-839-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-839-005-001 SUBTASK SOLUTION ADDED N

Subtask 343232-941-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-941-005-001 SUBTASK SOLUTION ADDED N

Subtask 343232-960-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

NOTE UPDATED

R

Subtask 343232-960-004-002 SUBTASK SOLUTION ADDED N

Subtask 343232-700-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-700-004-001 SUBTASK SOLUTION ADDED N

Subtask 343232-942-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-942-005-001 SUBTASK SOLUTION ADDED N

TASK 343232- 831-805-001-Replacement

of the THALES AOA Probes by Part

Number post Vendor Service Bulletin

THALES AVIONICS C16291A-34-007

Revision No. 01 (or any later revision).

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 343232-839-006-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 343232-839-006-001 SUBTASK SOLUTION ADDED N

Subtask 343232-941-006-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-941-006-001 SUBTASK SOLUTION ADDED N

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 343232-960-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PART NUMBER UPDATED

FIN UPDATED

MANPOWER RESSOURCE UPDATED

REFERENCES UPDATED

R

Subtask 343232-831-002-001 SUBTASK SOLUTION ADDED N

Subtask 343232-831-003-001 SUBTASK SOLUTION ADDED N

Subtask 343232-960-005-003 SUBTASK SOLUTION ADDED N

Subtask 343232-831-002-001 SUBTASK SOLUTION ADDED N

Subtask 343232-831-003-002 SUBTASK SOLUTION ADDED N

Subtask 343232-700-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 343232-700-005-001 SUBTASK SOLUTION ADDED N

Subtask 343232-942-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343232-942-004-001 SUBTASK SOLUTION ADDED N

TASK 343232- 832-802-001-Inspection -

ADDITIONAL WORK for Aircraft modified

by Original Issue.

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 343232-839-007-001 SUBTASK SOLUTION ADDED N

Subtask 343232-941-007-001 SUBTASK SOLUTION ADDED N

Subtask 343232-832-002-001 SUBTASK SOLUTION ADDED N

Subtask 343232-942-008-001 SUBTASK SOLUTION ADDED N

Fig. A-FFAAA FIGURE SOLUTION ADDED N

Fig. A-FFAAA Sheet 01 SHEET ADDED N

Fig. A-FFAAB FIGURE SOLUTION ADDED N

Fig. A-FFAAB Sheet 01 SHEET ADDED N

Fig. A-FFBAA FIGURE SOLUTION ADDED N

Fig. A-FFBAA Sheet 01 SHEET ADDED N

Fig. A-FRAAA FIGURE SOLUTION ADDED N

Fig. A-FRAAA Sheet 01 SHEET ADDED N

Fig. A-FBB FIGURE DELETED FOR APPLICABLE MSN D

APPENDIX APPENDIX DELETED D

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 6

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Jan 20/10

REVISION No. : 01 - Sep 17/13

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 7

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 8

5

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@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During Airbus Final Assembly Line reception flight test, AOA (Angle of Attack) data from two aircraft

(one per A/C) were found inaccurate during the in-flight production tests and confirmed during DFDR

(Digital Flight Data Recorder) analysis.

Investigation of the removed probes revealed oil residue between the stator and the rotor parts of the

AOA vane position resolvers. The presence of this oil residue results from a quality escape during the

manufacturing process of the AOA resolvers, which led to a poor cleaning of machining oil.

The oil residue has been found to become viscous at low temperatures (typically in cruise) causing lag

of AOA vane movement.

This Inspection Service Bulletin requires the inspection of THALES AOA probes PN C16291AA and

PN C16291AB. For those AOA probes corresponding to the batch of serial numbers listed in VSB

C16291A-34-007 revision 01 or any later revision, replacement of the AOA probe is required.

Accomplishment of this Service Bulletin will ensure that AOA probes potentially affected by the oil

residue issue are replaced on aircraft.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

11S 38W 39V 62S AAR AAW ABD ACA ACI AEA AFL AFR AIB

ALK ARA ARG AZA BEC BEL BER CHH CRK CRL CSA CSC DAH

DAL DGA DLH EDW EIN ETD FWI GFA GIA GRL HAL HFY HVN

I2L IAC IAW IBE IYE JAV KAL KLM MAS MAU MON MSR NMB

OBS OHY PAL QAF QTR RJA RSY SAI SWR SYA TAE TAM TAP

TCX THY TOW TSC UAE USA VKG VOZ WRC XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER OIT SE 999.0065/09

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 343232-832-801-001: Inspection

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 2

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SERVICE BULLETIN

SUMMARY

Task 343232-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-804-001: Replacement of the THALES AOA Probes through Airbus RFC/RMO

Process.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-805-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

**CONF 002

Task 343232-832-801-001: Inspection

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-804-001: Replacement of the THALES AOA Probes through Airbus RFC/RMO

Process.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-805-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 3

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@A330

SERVICE BULLETIN

SUMMARY

Task 343232-832-802-001: Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

APPENDICES

**CONF ALL

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 4

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR19

FR18

A

3FP1

3FP2

3FP3

A

A

AREA TO BE INSPECTED

TYPICAL INSTALLATION

A

G_SB_343232_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 5

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@A330

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 6

5

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: 34

TITLE: NAVIGATION - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

MODIFICATION No.: None

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

(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

0030 0037 0042 0045 0054-0055 0070 0072 0077 0082 0086-0087 0095-0096 0107

0111 0116 0119-0120 0127 0138 0140 0143-0144 0148 0153 0162 0165 0171-0172

0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0211 0219

0222-0223 0226 0229-0230 0232 0238 0240-0241 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 0342-0345 0348-0351 0353 0356-0357 0361-0362

0365-0366 0368-0370 0372 0375 0380 0382 0384 0388 0392 0396-0398 0400-0401

0403-0404 0408-0409 0412 0419 0422 0425 0427-0428 0437 0441 0443 0448

0451-0452 0455-0456 0458 0461-0463 0465-0466 0472-0473 0477 0480-0481 0484

0486-0487 0489-0491 0494 0498 0500-0505 0507 0509-0511 0516 0518-0519 0521

0524-0526 0533 0536 0542 0549-0552 0567 0570-0571 0576 0578-0579 0584 0588

0591 0597 0600 0605 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 1

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@A330

SERVICE BULLETIN

0629 0631-0633 0635-0638 0640 0642 0644-0645 0647-0648 0650 0653 0657-0659

0663 0666-0667 0670 0674 0676 0680 0682-0684 0686-0688 0690 0696 0700-0701

0703 0708-0709 0711 0717-0718 0721-0722 0724 0726 0729-0730 0733-0734

0737-0738 0743 0745-0746 0749 0751 0758 0760 0770 0772 0778 0784 0788-0789

0792 0795-0796 0799 0801 0803 0806-0807 0809 0811 0813-0814 0817 0819-0820

0824 0826-0827 0832-0834 0843 0845 0849 0852 0854 0857-0859 0863 0865

0868-0869 0874 0876-0877 0883 0891 0893 0896 0899-0900 0904-0905 0907

0913-0914 0918 0922 0925 0927 0931 0934 0939 0943 0946 0950 0952 0962-0963

0965-0966 0970-0971 0973-0975 0979 0989 0991-0992 0999-1002 1008 1011 1014

1018-1019 1021-1022 1026 1029 1031-1034 1039 1041-1043 1045-1048 1053-1055

1057-1059 1065-1066 1069-1072 1075-1077 1081-1082 1084 1089 1095 1097

1100-1101 1103-1104 1114 1123 1126 1131 1133 1135 1138 1143 1145 1151 1155

1161 1165 1167 1171 1181 1188 1193 1200 1203 1205 1211 1217-1218 1225-1226

1230 1238 1241 1245-1246 1248 1252 1259 1264-1265 1275-1276 1283 1287 1290

1294-1295 1300 1302 1308 1310 1312-1313 1316 1321 1326-1327 1334 1339-1340

1354-1355 1359 1363 1376-1377 1381 1385 1389-1390 1393 1399 1403-1405 1411

1414-1415 1417 1419 1422-1423 1426 1433 1435 1437 1439 1441 1451 1455 1464

1466 1469 1472 1480-1481 1486 1488 1490 1496 1498-1499 1502 1507 1511-1512

1515 1518 1521 1524 1526 1530 1533 1535 1549 1556 1558 1564

(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

38W 0401

39V 0874 0939 0946

62S 1321

AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340

1435 1464 1518

AAW 0999 1043 1472 1499 1535

ABD 0343

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597 0670 0733 0745 0749 0814 0931 0950

1097

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1264

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

0567 0584 0657

AIB 0042

ALK 0303 0306 0311 0313 0404 0456 0627 1564

ARA 0891 0927

ARG 0290 0300

AZA 0272 0339 1123 1135 1218 1225 1252 1283 1308 1313 1327 1354

BEC 0863

BEL 0030 0037 0045 0082 0095 0229 0249 0324

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SERVICE BULLETIN

OPERATOR MSN

BER 0288 0322 0403

CHH 1558

CRK 1031 1034 1039 1042 1054 1059

CRL 0285 0320 1359 1376

CSA 0425

CSC 0462 1082 1138 1241

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

ETD 0658 0688 0717 0724 0729 0730 0737 0751 0788 0807 0809 0824

0832 0852 0854 0868 0975 0991 1032 1070 1071 1081 1167 1205

1226 1245 1414 1486 1521 1524

FWI 0253 0758 0965 1021 1265

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404

1422 1469 1488 1496 1511 1530

HFY 0096 0127 0211 0262 1008

HVN 0275 0294 0299 0366 0943 0962 1019

I2L 0205 0992

IAC 0353 0362

IAW 1339

IBE 1377 1385 1405 1426 1437 1490 1507 1515

IYE 0625 0632

JAV 0255

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

0351 0368 0428 0484 0490 0550 1133 1155 1200 1203 1393 1556

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

1287 1294 1300 1381

MAS 0077 0107 0116 0119

MAU 0883 1057

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246

NMB 1451 1466

OBS 0833

OHY 0072 0087 0143

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

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SERVICE BULLETIN

OPERATOR MSN

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

RSY 0120 0171

SAI 0055 0070 0086

SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290

1355 1403

SYA 0345

TAE 0348

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

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

TCX 0254 0266 0301 0398

THY 0463 0504

TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498

TSC 0111 0250 0271 0369 0427 0480 0795 0966 0971

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0382 0384 0392

0396 0409 0437 0451 0452 0455 0491 0494 0509 0518 0525 0536

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

1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526

VKG 0309 0349 0356 0357

VOZ 0365 0372

WRC 0296

XAX 0054 0330 0952 0974 1048 1066 1075 1126 1131 1165 1411 1423

1433 1481 1533 1549

XLF 0501 0635

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0030 0037 0045 0054 0055 0070 0072 0077 0082 0086 0087

0095 0096 0107 0111 0116 0119 0120 0127 0138 0140 0143

0144 0148 0153 0162 0165 0171 0172 0181 0184 0195 0205

0206 0211 0219 0222 0223 0226 0229 0230 0232 0238 0241

0247 0249 0250 0253 0254 0255 0256 0258 0259 0262 0265

0266 0267 0271 0272 0275 0276 0281 0286 0287 0288 0290

0291 0294 0296 0299 0300 0301 0303 0305 0306 0308 0309

0311 0312 0313 0315 0317 0322 0323 0324 0330 0333 0334

0337 0338 0339 0340 0342 0343 0345 0349 0350 0351 0353

0356 0357 0361 0362 0365 0366 0368 0369 0370 0372 0375

0380 0388 0398 0401 0403 0404 0425 0427 0428 0456 0466

0472 0477 0480 0484 0486 0489 0490 0494 0501 0505 0507

0510 0524 0526 0533 0542 0549 0550 0551 0552 0570 0576

0578 0579 0588 0591 0597 0600 0609 0610 0612 0614 0616

0618 0620 0621 0627 0629 0631 0633 0635 0636 0637 0638

0640 0642 0644 0645 0647 0648 0650 0653 0658 0659 0663

0666 0667 0670 0674 0683 0684 0687 0688 0690 0696 0700

0701 0708 0709 0711 0717 0718 0721 0722 0724 0726 0729

0730 0733 0734 0737 0743 0745 0746 0749 0751 0758 0760

0772 0778 0784 0788 0789 0792 0795 0796 0799 0806 0807

0809 0813 0814 0817 0824 0826 0827 0832 0833 0843 0845

0852 0854 0857 0858 0859 0863 0865 0868 0869 0874 0876

0877 0883 0891 0896 0899 0904 0905 0913 0914 0918 0922

0927 0931 0934 0939 0943 0946 0950 0952 0962 0965 0966

0970 0971 0974 0975 0979 0989 0991 0992 1002 1008 1011

1019 1021 1022 1031 1033 1034 1039 1041 1042 1046 1048

1053 1054 1057 1059 1066

001 002

0042 001

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SERVICE BULLETIN

MSN CONFIGURATION

0183 0188 0189 0191 0198 0200 0203 0240 0248 0251 0261

0269 0277 0279 0283 0284 0285 0293 0295 0314 0316 0320

0326 0328 0344 0348 0382 0384 0392 0396 0397 0400 0408

0409 0412 0419 0422 0437 0441 0443 0448 0451 0452 0455

0458 0461 0462 0463 0465 0473 0481 0487 0491 0498 0500

0502 0503 0504 0509 0511 0516 0518 0519 0521 0525 0536

0567 0571 0584 0605 0623 0625 0632 0657 0676 0680 0682

0686 0703 0738 0770 0801 0803 0811 0819 0820 0834 0849

0893 0900 0907 0925 0963 0973 0999 1000 1001 1014 1018

1026 1029 1032 1043 1045 1047 1055 1058 1065 1069 1070

1071 1072 1075 1076 1077 1081 1082 1084 1089 1095 1097

1100 1101 1103 1104 1114 1123 1126 1131 1133 1135 1138

1143 1145 1151 1155 1161 1165 1167 1171 1181 1188 1193

1200 1203 1205 1211 1217 1218 1225 1226 1230 1238 1241

1245 1246 1248 1252 1259 1264 1265 1275 1276 1283 1287

1290 1294 1295 1300 1302 1308 1310 1312 1313 1316 1321

1326 1327 1334 1339 1340 1354 1355 1359 1363 1376 1377

1381 1385 1389 1390 1393 1399 1403 1404 1405 1411 1414

1415 1417 1419 1422 1423 1426 1433 1435 1437 1439 1441

1451 1455 1464 1466 1469 1472 1480 1481 1486 1488 1490

1496 1498 1499 1502 1507 1511 1512 1515 1518 1521 1524

1526 1530 1533 1535 1549 1556 1558 1564

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Mod No. 58555S30640 (Service Bulletin

A330-34-3228) is not embodied.

**CONF 002

Config. 002 is valid for aircraft on which Mod No. 58555S30640 (Service Bulletin

A330-34-3228) is embodied.

(6) Material Effectivity

No Material Set

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

During Airbus Final Assembly Line reception flight test, AOA (Angle of Attack) data from

two aircraft (one per A/C) were found inaccurate during the in-flight production tests and

confirmed during DFDR (Digital Flight Data Recorder) analysis.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Investigation of the removed probes revealed oil residue between the stator and the

rotor parts of the AOA vane position resolvers. The presence of this oil residue results

from a quality escape during the manufacturing process of the AOA resolvers, which led

to a poor cleaning of machining oil.

The oil residue has been found to become viscous at low temperatures (typically in

cruise) causing lag of AOA vane movement.

(2) Objective/Action

This Inspection Service Bulletin requires the inspection of THALES AOA probes PN

C16291AA and PN C16291AB. For those AOA probes corresponding to the batch

of serial numbers listed in VSB C16291A-34-007 revision 01 or any later revision,

replacement of the AOA probe is required.

(3) Advantages

Accomplishment of this Service Bulletin will ensure that AOA probes potentially affected

by the oil residue issue are replaced on aircraft.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

NOTE: For Config. 001, depending on the result of the inspection, four possibilities

are available:

- either replace the affected AOA probes as described in TASK

343232-831-801 001 Replacement of the THALES AOA Probes by Part

Number C16291AB whose SN is not listed in THALES AVIONICS Service

Bulletin No. C16291A-34-007 Revision No. 01 (or any later revision).

- or replace them as described in TASK 343232-831-802 001 Replacement

of the THALES AOA Probes by Part Number C16291AA whose Serial

Number is not listed in the THALES VSB C16291A-34-007 Revision No.

01 (or any later revision).

- or replace them as described in TASK 343232-831-804 001 Replacement

of the THALES AOA Probes through Airbus RFC/RMO Process.

- or replace them as described in TASK 343232-831-805 001 Replacement

of the THALES AOA Probes by Part Number post Vendor Service Bulletin

THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

NOTE: For Config. 002, depending on the result of the inspection, three possibilities

are available:

- either replace the affected AOA probes as described in TASK

343232-831-801 001 Replacement of the THALES AOA Probes by Part

Number C16291AB whose SN is not listed in THALES AVIONICS Service

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Bulletin No. C16291A-34-007 Revision No. 01 (or any later revision).

- or replace them as described in TASK 343232-831-804 001 Replacement

of the THALES AOA Probes through Airbus RFC/RMO Process.

- or replace them as described in TASK 343232-831-805 001 Replacement

of the THALES AOA Probes by Part Number post Vendor Service Bulletin

THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 343232-832-801-001: Inspection

(1) Inspection of the three AOA probes (3FP1, 3FP2, 3FP3)

Task 343232-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

(1) Replace the affected THALES AOA Probes by PN C16291AB whose SN is not listed

in THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01 (or any

later revision).

Task 343232-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

(1) Replace the affected THALES AOA Probes by PN C16291AA whose Serial Number

is not listed in the THALES VSB C16291A-34-007 Revision No. 01 (or any later

revision).

Task 343232-831-804-001: Replacement of the THALES AOA Probes through Airbus

RFC/RMO Process.

(1) Replace the affected AOA Probes through Airbus RFC/RMO Process.

Task 343232-831-805-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

(1) Remove the affected AOA Probes.

(2) Modify the AOA Probes.

(3) Install the AOA Probes.

**CONF 002

Task 343232-832-801-001: Inspection

(1) Inspection of the three AOA probes (FINs 3FP1, 3FP2 and 3FP3).

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Task 343232-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

(1) Replace the affected THALES AOA Probes by PN C16291AB whose SN is not listed

in THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01 (or any

later revision).

Task 343232-831-804-001: Replacement of the THALES AOA Probes through Airbus

RFC/RMO Process.

(1) Replace the affected AOA Probes through Airbus RFC/RMO Process.

Task 343232-831-805-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

(1) Remove the affected AOA Probes.

(2) Modify the AOA Probes.

(3) Install the AOA Probes.

Task 343232-832-802-001: Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

(1) Do a Detailed Inspection of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3).

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

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.

Table 1, Config. 001 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

All aircraft potentially

fitted with PN

C16291AA

Inspect in accordance

with TASK

343232-832-801 001

Inspection

NOTE*

At the earliest

maintenance opportunity

after ISB receipt and

before end of April 2010

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Table 1, Config. 001 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

Part Number C16291AA

installed with AOA

Serial Number listed in

Vendor SB

C16291A-34-007

Revision No. 01 (or any

later revision) and Mod

No.53368S18144 (or

Service Bulletin

A330-34-3213)

embodied

Replace the affected

AOA probes as per

TASK 343232-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 343232-831-802

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AA whose Serial

Number is not listed in

the THALES VSB

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 343232-831-804

001 Replacement of the

THALES AOA Probes

through Airbus

RFC/RMO Process.

or

TASK 343232-831-805

001 Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of April 2010 None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Table 1, Config. 001 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

Replace the affected

AOA probes as per

TASK 343232-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 343232-831-802

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AA whose Serial

Number is not listed in

the THALES VSB

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 343232-831-804

001 Replacement of the

THALES AOA Probes

through Airbus

RFC/RMO Process.

or

TASK 343232-831-805

001 Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of April 2011 None

AND

Part Number C16291AA

installed with AOA

Serial Number listed in

VSB C16291A-34-007

Revision No. 01 (or any

later revision) and

53368S18144 (or

Service Bulletin

A330-34-3213) not

embodied

No further action None None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Table 1, Config. 001 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

Part Number C16291AA

not installed or PN

C16291AA installed but

AOA Serial Number not

listed in VSB

C16291A-34-007

Revision No. 01 (or any

later revision)

No further action None None

NOTE*: A review of aircraft maintenance records is acceptable to determine the SN of the AOA

Probes.

**CONF 002

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.

Table 1, Config. 002 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

All aircraft potentially

fitted with PN

C16291AB

Inspect in accordance

with TASK

343232-832-801 001

Inspection

NOTE*

At the earliest

maintenance opportunity

after ISB receipt and

before end of

September 2013

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Table 1, Config. 002 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

Replace the affected

AOA probes as per

TASK 343232-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 343232-831-804

001 Replacement of the

THALES AOA Probes

through Airbus

RFC/RMO Process.

or

TASK 343232-831-805

001 Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of

September 2013

None

AND

Part Number C16291AB

installed with AOA

Serial Number listed in

Vendor SB

C16291A-34-007

Revision No. 01 (or any

later revision)

No further action None None

Part Number C16291AB

not installed or PN

C16291AB installed but

AOA Serial Number not

listed in VSB

C16291A-34-007

Revision No. 01 (or any

later revision)

No further action None None

NOTE*: A review of aircraft maintenance records is acceptable to determine the SN of the AOA

Probes.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Table 2, Config. 002 - ADDITIONAL WORK - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

All aircraft potentially

fitted with PN

C16291AB

Inspect in accordance

with TASK

343232-832-802 001

Inspection -

ADDITIONAL WORK for

Aircraft modified by

Original Issue.

NOTE*

At the earliest

maintenance opportunity

after ISB receipt and

before end of

September 2013

None

Replace the affected

AOA probes as per

TASK 343232-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 343232-831-804

001 Replacement of the

THALES AOA Probes

through Airbus

RFC/RMO Process.

or

TASK 343232-831-805

001 Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of

September 2013

None

AND

Part Number C16291AB

installed with AOA

Serial Number listed in

Vendor SB

C16291A-34-007

Revision No. 01 (or any

later revision)

No further action None None

Part Number C16291AB

not installed or PN

C16291AB installed but

AOA Serial Number not

listed in VSB

C16291A-34-007

Revision No. 01 (or any

later revision)

No further action None None

NOTE*: A review of aircraft maintenance records is acceptable to determine the SN of the AOA

Probes.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

**CONF ALL

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 343232-832-801-001: Inspection

Get Access 0.50

On Aircraft

Inspection of the three AOA probes (3FP1, 3FP2,

3FP3)

1.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

Get Access 0.50

On Aircraft

Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

Get Access 0.50

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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Task 343232-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

On Aircraft

Replace the affected THALES AOA Probes by PN

C16291AA whose Serial Number is not listed in the

THALES VSB C16291A-34-007 Revision No. 01 (or

any later revision).

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-804-001: Replacement of the THALES AOA Probes through Airbus RFC/RMO

Process.

Get Access 0.50

On Aircraft

Replace the affected AOA Probes through Airbus

RFC/RMO Process.

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-805-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

Get Access 0.50

On Aircraft

Remove the affected AOA Probes. 0.50

Install the AOA Probes. 0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

**CONF 002

Task 343232-832-801-001: Inspection

Get Access 0.50

On Aircraft

Inspection of the three AOA probes (FINs 3FP1, 3FP2

and 3FP3).

1.50

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Task 343232-832-801-001: Inspection

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

Get Access 0.50

On Aircraft

Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-804-001: Replacement of the THALES AOA Probes through Airbus RFC/RMO

Process.

Get Access 0.50

On Aircraft

Replace the affected AOA Probes through Airbus

RFC/RMO Process.

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 343232-831-805-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

Get Access 0.50

On Aircraft

Remove the affected AOA Probes. 0.50

Install the AOA Probes. 0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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Task 343232-832-802-001: Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

Get Access 0.50

On Aircraft

Do a Detailed Inspection of the three AOA Probes

(FINs 3FP1, 3FP2 and 3FP3).

1.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-53 12-34-24 34-11-19

52-10-00

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

Service Bulletin (SB) A330-34-3087

A330-34-3228

Vendor Service Bulletin (VSB) THALES AVIONICS Service

Bulletin No. C16291A-34-007

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-53 12-34-24 34-11-19

52-10-00

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

Service Bulletin (SB) A330-34-3087

Vendor Service Bulletin (VSB) THALES AVIONICS Service

Bulletin No. C16291A-34-007

**CONF ALL

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

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M. SPARES

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with THALES

AVIONICS as per instructions given in THALES AVIONICS Service Bulletin No.

C16291A-34-007.

(2) Price and Availability

No AIRBUS kit will be provided.

Refer to the THALES AVIONICS Service Bulletin No. C16291A-34-007 for the

equipment modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the THALES AVIONICS Service Bulletin No. C16291A-34-007 for the industry

support terms of the Vendor Service Bulletin parts and labor.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 343232-832-801-001 - Inspection

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: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition or acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

NOTE: The purpose of flow charts is to supplement the information given in the

Procedure and Compliance paragraphs and not to serve as the primary

source for tasks or compliance times given in this Service Bulletin.

**CONF 001

(1) Subtask 343232-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 343232-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

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**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 343232-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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**CONF 002

(1) Subtask 343232-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 343232-832-001-001 - Inspection of the three AOA probes (3FP1, 3FP2,

3FP3)

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) At the threshold given in PLANNING INFORMATION paragraph E.(2):

Do a Detailed Inspection of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3).

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

1 Check the SN of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3), refer to

THALES AVIONICS Service Bulletin No. C16291A-34-007 Rev. 01 or any later

revision.

NOTE: If PN or/and SN are not clearly visible, remove the AOA

Probe, without disconnecting the connector, refer to AMM Task

34-11-19-000-801 to do the Inspection Requirements.

NOTE: A review of aircraft maintenance records is acceptable to

determine the SN of the AOA Probes.

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a If the AOA Probe is part of the affected SN:

<1> At the threshold given in PLANNING INFORMATION paragraph

E.(2), do TASK 343232-831-801 001 Replacement of the THALES

AOA Probes by Part Number C16291AB whose SN is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision

No. 01 (or any later revision).

or

Do TASK 343232-831-802 001 Replacement of the THALES AOA

Probes by Part Number C16291AA whose Serial Number is not

listed in the THALES VSB C16291A-34-007 Revision No. 01 (or any

later revision).

or

Do TASK 343232-831-804 001 Replacement of the THALES AOA

Probes through Airbus RFC/RMO Process.

or

Do TASK 343232-831-805 001 Replacement of the THALES AOA

Probes by Part Number post Vendor Service Bulletin THALES

AVIONICS C16291A-34-007 Revision No. 01 (or any later revision).

<2> No further action is required.

b If the AOA Probe is not part of the affected SN:

<1> No further action is required.

(b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA.

**CONF 002

(1) Subtask 343232-832-001-002 - Inspection of the three AOA probes (FINs 3FP1,

3FP2 and 3FP3).

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

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References

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAB

Flow Chart

Sheet 01

(a) At the threshold given in PLANNING INFORMATION paragraph E.(2):

Do a Detailed Inspection of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3).

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAB

1 Check the SN of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3), refer to

THALES AVIONICS Service Bulletin No. C16291A-34-007 Rev. 01 or any later

revision.

NOTE: If PN or/and SN are not clearly visible, remove the AOA

Probe, without disconnecting the connector, refer to AMM Task

34-11-19-000-801 to do the Inspection Requirements.

NOTE: A review of aircraft maintenance records is acceptable to

determine the SN of the AOA Probes.

a If the AOA Probe is part of the affected SN:

<1> At the threshold given in PLANNING INFORMATION paragraph

E.(2), do TASK 343232-831-801 001 Replacement of the THALES

AOA Probes by Part Number C16291AB whose SN is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision

No. 01 (or any later revision).

or

Do TASK 343232-831-804 001 Replacement of the THALES AOA

Probes through Airbus RFC/RMO Process.

or

Do TASK 343232-831-805 001 Replacement of the THALES AOA

Probes by Part Number post Vendor Service Bulletin THALES

AVIONICS C16291A-34-007 Revision No. 01 (or any later revision).

<2> No further action is required.

b If the AOA Probe is not part of the affected SN:

<1> No further action is required.

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(b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 343232-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

NOTE: If you intend to accomplish an associated Repair Task during the same

layover period, the subsequent Close-up procedure is not necessary.

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 343232-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

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References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

NOTE: If you intend to accomplish an associated Repair Task during the same

layover period, the subsequent Close-up procedure is not necessary.

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

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Task 343232-831-801-001 - Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

**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: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition or acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 33

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Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 343232-839-003-001 - 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 343232-839-003-001 - 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: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 34

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**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 343232-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

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(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

**CONF 002

(1) Subtask 343232-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 343232-960-002-001 - Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Task 34-11-19-400-801

Service Bulletin (SB) A330-34-3228

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Remove (Refer to AMM Task 34-11-19-000-801) :

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

3 3FP3, AOA probe, C16291AA.

(b) Install (Refer to AMM Task 34-11-19-400-801) :

NOTE: The replacement of the AOA probes is covered by Service Bulletin

No. A330-34-3228.

NOTE: Install AOA Probes whose Serial Number is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01

(or any later revision).

1 3FP1, AOA probe, C16291AB.

- and/or

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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2 3FP2, AOA probe, C16291AB.

- and/or

3 3FP3, AOA probe, C16291AB.

**CONF 002

(1) Subtask 343232-960-002-002 - Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Task 34-11-19-400-801

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Remove:

Refer to AMM Task 34-11-19-000-801

1 3FP1, AOA probe, C16291AB.

and/or

2 3FP2, AOA probe, C16291AB.

and/or

3 3FP3, AOA probe, C16291AB.

(b) Install:

Refer to AMM Task 34-11-19-400-801

NOTE: Install AOA Probes whose Serial Number is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01

(or any later revision).

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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1 3FP1, AOA probe, C16291AB.

and/or

2 3FP2, AOA probe, C16291AB.

and/or

3 3FP3, AOA probe, C16291AB.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 343232-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Job Set-up:

1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s)

as specified after the installation of the AOA Probes (FINs 3FP1, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

1 Do the test procedure as specified after the installation of the AOA Probes

(FINs 3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

**CONF 002

(1) Subtask 343232-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Job Set-up:

1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s)

as specified after the installation of the AOA Probes (FINs 3FP1, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

(b) Test:

1 Do the test procedure as specified after the installation of the AOA Probes

(FINs 3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 343232-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 343232-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 41

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This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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Task 343232-831-802-001 - Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

**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: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition or acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 43

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SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

None

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 343232-839-004-001 - 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

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 343232-941-004-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

**CONF 002

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 343232-960-003-001 - Replace the affected THALES AOA Probes by PN

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007

Revision No. 01 (or any later revision).

Work Zones and Access Panels

Zone Access/Work location

121

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 45

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122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Task 34-11-19-400-801

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Remove (Refer to AMM Task 34-11-19-000-801) :

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

3 3FP3, AOA probe, C16291AA.

(b) Install (Refer to AMM Task 34-11-19-400-801) :

NOTE: You must install AOA probes whose Serial Number is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 Rev. 01

or any later revision.

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

3 3FP3, AOA probe, C16291AA.

**CONF 002

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 46

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**CONF ALL

D. TEST

**CONF 001

(1) Subtask 343232-700-003-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Job set-up :

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the AOA probes (3FP1, 3FP2, 3FP3) (Refer to AMM

Task 34-11-19-400-801).

(b) Test :

1 Do the test procedure as specified after the installation of the AOA probes

(3FP1, 3FP2, 3FP3) (Refer to AMM Task 34-11-19-400-801).

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 343232-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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(d) Remove the access platform(s).

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

**CONF 002

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 48

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SERVICE BULLETIN

Task 343232-831-804-001 - Replacement of the THALES AOA Probes through Airbus

RFC/RMO Process.

**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: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition or acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 49

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Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 343232-839-005-001 - 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 343232-839-005-001 - 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: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 50

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**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 343232-941-005-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

**CONF 002

(1) Subtask 343232-941-005-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 52

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 343232-960-004-001 - Replace the affected AOA Probes through Airbus

RFC/RMO Process.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Task 34-11-19-400-801

Service Bulletin (SB) A330-34-3087

(a) Remove (Refer to AMM Task 34-11-19-000-801) :

1 3FP1, AOA probe, C16291AA.

- and

2 3FP2, AOA probe, C16291AA.

- and

3 3FP3, AOA probe, C16291AA.

(b) Install (Refer to AMM Task 34-11-19-400-801) :

NOTE: The replacement of the three THALES AOA probes by three

GOODRICH PN 0861ED is covered by Service Bulletin No.

A330-34-3087 or by RFC/RMO procedure.

1 3FP1, AOA probe, 0861ED.

- and

2 3FP2, AOA probe, 0861ED.

- and

3 3FP3, AOA probe, 0861ED.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

**CONF 002

(1) Subtask 343232-960-004-002 - Replace the affected AOA Probes through Airbus

RFC/RMO Process.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Task 34-11-19-400-801

Service Bulletin (SB) A330-34-3087

(a) Remove:

Refer to AMM Task 34-11-19-000-801

1 3FP1, AOA probe, C16291AB.

- and

2 3FP2, AOA probe, C16291AB.

- and

3 3FP3, AOA probe, C16291AB.

(b) Install:

Refer to AMM Task 34-11-19-400-801

NOTE: The replacement of the three THALES AOA probes by three

GOODRICH PN 0861ED is covered by Service Bulletin No.

A330-34-3087 or by RFC/RMO procedure.

1 3FP1, AOA probe, 0861ED.

- and

2 3FP2, AOA probe, 0861ED.

- and

3 3FP3, AOA probe, 0861ED.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 54

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SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 343232-700-004-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Job Set-up:

1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s)

as specified after the installation of the AOA Probes (FINs 3FP1, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

1 Do the test procedure as specified after the installation of the AOA Probes

(FINs 3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

**CONF 002

(1) Subtask 343232-700-004-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Job Set-up:

1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s)

as specified after the installation of the AOA Probes (FINs 3FP1, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

1 Do the test procedure as specified after the installation of the AOA Probes

(FINs 3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 55

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 343232-942-005-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 343232-942-005-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 56

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SERVICE BULLETIN

Task 343232-831-805-001 - Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

**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: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition or acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 57

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SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

THALES AVIONICS Service Bulletin No. C16291A-34-007

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

THALES AVIONICS Service Bulletin No. C16291A-34-007

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 343232-839-006-001 - 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 343232-839-006-001 - 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: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 58

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SERVICE BULLETIN

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 343232-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 59

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SERVICE BULLETIN

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

**CONF 002

(1) Subtask 343232-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 60

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 343232-960-005-001 - Remove the affected AOA Probes.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

(a) Remove:

Refer to AMM Task 34-11-19-000-801

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

3 3FP3, AOA probe, C16291AA.

(2) Subtask 343232-831-002-001 - Modify the AOA Probes.

References

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Modify the affected AOA Probes (FINs 3FP1 and/or 3FP2 and/or 3FP3) as per

instructions given in THALES AVIONICS Service Bulletin No. C16291A-34-007.

(3) Subtask 343232-831-003-001 - Install the AOA Probes.

Work Zones and Access Panels

Zone Access/Work location

121

122

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 61

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SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Install:

Refer to AMM Task 34-11-19-400-801

1 3FP1, AOA probe, C16291AA post THALES AVIONICS Service Bulletin No.

C16291A-34-007 Rev. 01 or any later revision.

- and/or

2 3FP2, AOA probe, C16291AA post THALES AVIONICS Service Bulletin No.

C16291A-34-007 Rev. 01 or any later revision.

- and/or

3 3FP3, AOA probe, C16291AA post THALES AVIONICS Service Bulletin No.

C16291A-34-007 Rev. 01 or any later revision.

**CONF 002

(1) Subtask 343232-960-005-003 - Remove the affected AOA Probes.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

(a) Remove:

Refer to AMM Task 34-11-19-000-801

1 3FP1, AOA probe, C16291AB.

- and/or

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 62

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SERVICE BULLETIN

2 3FP2, AOA probe, C16291AB.

- and/or

3 3FP3, AOA probe, C16291AB.

(2) Subtask 343232-831-002-001 - Modify the AOA Probes.

References

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Modify the affected AOA Probes (FINs 3FP1 and/or 3FP2 and/or 3FP3) as per

instructions given in THALES AVIONICS Service Bulletin No. C16291A-34-007.

(3) Subtask 343232-831-003-002 - Install the AOA Probes.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Install:

Refer to AMM Task 34-11-19-400-801

1 3FP1, AOA probe, C16291AB post THALES AVIONICS Service Bulletin No.

C16291A-34-007 Rev. 01 or any later revision.

- and/or

2 3FP2, AOA probe, C16291AB post THALES AVIONICS Service Bulletin No.

C16291A-34-007 Rev. 01 or any later revision.

- and/or

3 3FP3, AOA probe, C16291AB post THALES AVIONICS Service Bulletin No.

C16291A-34-007 Rev. 01 or any later revision.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 63

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SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 343232-700-005-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Job Set-up:

1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s)

as specified after the installation of the AOA Probes (FINs 3FP1, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

1 Do the test procedure as specified after the installation of the AOA Probes

(FINs 3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

**CONF 002

(1) Subtask 343232-700-005-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Job Set-up:

1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s)

as specified after the installation of the AOA Probes (FINs 3FP1, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

1 Do the test procedure as specified after the installation of the AOA Probes

(FINs 3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 64

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 343232-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 343232-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 65

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 66

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SERVICE BULLETIN

Task 343232-832-802-001 - Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

**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: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition or acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

Task Associated Data

**CONF 001

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 67

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SERVICE BULLETIN

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

NOTE: The purpose of flow charts is to supplement the information given in the

Procedure and Compliance paragraphs and not to serve as the primary

source for tasks or compliance times given in this Service Bulletin.

**CONF 001

None

**CONF 002

(1) Subtask 343232-839-007-001 - 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 ALL

B. PREPARATION

**CONF 001

None

**CONF 002

(1) Subtask 343232-941-007-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-000-801.

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 343232-832-002-001 - Do a Detailed Inspection of the three AOA Probes

(FINs 3FP1, 3FP2 and 3FP3).

Work Zones and Access Panels

Zone Access/Work location

121

122

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FFBAA

Flow Chart (ADDITIONAL WORK)

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

(a) At the threshold given in PLANNING INFORMATION paragraph E.(2):

Do a Detailed Inspection of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3).

Refer to Fig. A-FBAAA

Refer to Fig. A-FFBAA

1 Check the SN of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3), refer to

THALES AVIONICS Service Bulletin No. C16291A-34-007 Rev. 01 or any later

revision.

NOTE: If PN or/and SN are not clearly visible, remove the AOA

Probe, without disconnecting the connector, refer to AMM Task

34-11-19-000-801 to do the Inspection Requirements.

NOTE: A review of aircraft maintenance records is acceptable to

determine the SN of the AOA Probes.

a If the AOA Probe is part of the affected SN:

<1> At the threshold given in PLANNING INFORMATION paragraph

E.(2), do TASK 343232-831-801 001 Replacement of the THALES

AOA Probes by Part Number C16291AB whose SN is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision

No. 01 (or any later revision).

or

Do TASK 343232-831-804 001 Replacement of the THALES AOA

Probes through Airbus RFC/RMO Process.

or

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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Do TASK 343232-831-805 001 Replacement of the THALES AOA

Probes by Part Number post Vendor Service Bulletin THALES

AVIONICS C16291A-34-007 Revision No. 01 (or any later revision).

<2> No further action is required.

b If the AOA Probe is not part of the affected SN:

<1> No further action is required.

(b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 343232-942-008-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

NOTE: If you intend to accomplish an associated Repair Task during the same

layover period, the subsequent Close-up procedure is not necessary.

(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 AOA Probes (FINs

3FP1, 3FP2 and 3FP3), refer to AMM Task 34-11-19-400-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

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SERVICE BULLETIN

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 72

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SERVICE BULLETIN

**CONF ALL

FR19

FR18

A

3FP1

3FP2

3FP3

A

A

DETAILED VISUAL INSPECTION AREA

TYPICAL INSTALLATION

NOTE:

A

G_SB_343232_5_BAAA_01_03

Figure A-FBAAA - Sheet 01

Area to be inspected

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 73

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SERVICE BULLETIN

**CONF 001

REFER TO THALES VSB

NO

(OR ANY LATER

NO FURTHER ACTION

REPORT TO AIRBUS

QUESTION

ACTION

FINDING

LISTED IN TABLE,

SN

REVISION)

C16291A−34−007 REVISION 01

OR

NO

REMOVE AFFECTED AOA PROBES 

PN C16291AA REFER TO AMM 

34−11−19−000−801 BEFORE END APRIL 2010

OR

INSTALL AOA PROBES PN C16291AA WHOSE SN IS NOT LISTED IN

OR

INSTALL THREE GOODRICH AOA PROBES PN 0861ED

COVERED BY SB A330−34−3087 OR BY RFC/RMO PROCEDURE

INSTALL AOA PROBES PN C16291AA 

MODIFICATION

No 53368S18144 OR

SB No A330−34−3213

EMBODIED

REMOVE AFFECTED AOA PROBES 

PN C16291AA REFER TO AMM 

34−11−19−000−801 BEFORE END APRIL 2011

POST THALES VSB C16291A−34−007 REVISION 01 (OR ANY LATER REVISION)

YES

YES

THALES VSB C16291A−34−007 REVISION 01 (OR ANY LATER REVISION)

REFER TO TASK 343232−831−802−001

REFER TO TASK 343232−831−804−001

REFER TO TASK 343232−831−805−001

IDENTIFY THE SERIAL NUMBER (SN) OF THE THREE AOA PROBES PART NUMBER (PN) C16291AA

(FINS 3FP1, 3FP2, 3FP3) THROUGH A DETAILED INSPECTION OR AS PER AIRCRAFT RECORDS DATA ANALYSIS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2)

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE

AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN

REFER TO TASK 343232−832−801−001

INSTALL AOA PROBES PN C16291AB

WHOSE SN IS NOT LISTED IN THALES VSB C16291A−34−007 REVISION 01

(OR ANY LATER REVISION) COVERED BY SB A330−34−3228

REFER TO TASK 343232−831−801−001

G_SB_343232_5_FAAA_01_02

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 74

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SERVICE BULLETIN

**CONF 002

REFER TO THALES VSB

NO

(OR ANY LATER

NO FURTHER ACTION

REPORT TO AIRBUS

QUESTION

ACTION

FINDING

LISTED IN TABLE,

SN

REVISION)

C16291A−34−007 REVISION 01

OR

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

POST THALES VSB C16291A−34−007 REVISION 01 (OR ANY LATER REVISION)

YES

REFER TO TASK 343232−831−805−001

REFER TO TASK 343232−832−801−001

IDENTIFY THE SERIAL NUMBER (SN) OF THE THREE AOA PROBES PART NUMBER (PN) C16291AB

(FINS 3FP1, 3FP2, 3FP3) THROUGH A DETAILED INSPECTION OR AS PER AIRCRAFT RECORDS DATA ANALYSIS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2)

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE

AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN

OR

INSTALL THREE GOODRICH AOA PROBES PN 0861ED

COVERED BY SB A330−34−3087 OR BY RFC/RMO PROCEDURE

REFER TO TASK 343232−831−804−001

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

WHOSE SN IS NOT LISTED IN THALES VSB C16291A−34−007 REVISION 01

(OR ANY LATER REVISION)

REFER TO TASK 343232−831−801−001

G_SB_343232_5_FAAB_01_02

Figure A-FFAAB - Sheet 01

Flow Chart

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 75

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SERVICE BULLETIN

**CONF 002

REFER TO THALES VSB

NO

(OR ANY LATER

NO FURTHER ACTION

REPORT TO AIRBUS

QUESTION

ACTION

FINDING

LISTED IN TABLE,

SN

REVISION)

C16291A−34−007 REVISION 01

OR

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

POST THALES VSB C16291A−34−007 REVISION 01

YES

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE

AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN

(OR ANY LATER REVISION)

REFER TO TASK 343232−831−805−001

OR

INSTALL THREE GOODRICH AOA PROBES PN 0861ED

COVERED BY SB A330−34−3087 OR BY RFC/RMO PROCEDURE

REFER TO TASK 343232−831−804−001

REFER TO TASK 343232−832−802−001

IDENTIFY THE SERIAL NUMBER (SN) OF THE THREE AOA PROBES PART NUMBER (PN) C16291AB

(FINS 3FP1, 3FP2, 3FP3) THROUGH A DETAILED INSPECTION OR AS PER AIRCRAFT RECORDS DATA ANALYSIS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2)

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

WHOSE SN IS NOT LISTED IN THALES VSB C16291A−34−007 REVISION 01

(OR ANY LATER REVISION)

REFER TO TASK 343232−831−801−001

G_SB_343232_5_FBAA_01_02

Figure A-FFBAA - Sheet 01

Flow Chart (ADDITIONAL WORK)

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 76

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SERVICE BULLETIN

**CONF ALL

PN IDENTIFICATION

3FP1

SN IDENTIFICATION

REPLACEMENT OF AOA YES

NO

FIN

PROBE

3FP2

YES

NO

3FP3

YES

NO

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGENEERING − SEEA3

NAVIGATION AND FLIGHT GUIDANCE/

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 44 25

NEW AOA PROBE SN

INSTALLED

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A330−34−3232

DATE OF INSPECTION :

INSPECTION METHOD : DETAILED

INSPECTION

MANAGEMENT SYSTEMS

G_SB_343232_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 77

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This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 78

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SERVICE BULLETIN

REPORTING SHEET

TITLE: NAVIGATION - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

MODIFICATION No.: None

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: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 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: Jan 20/10 SERVICE BULLETIN No.: A330-34-3232

REVISION No.: 01 - Sep 17/13 Page: 1

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