@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 - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

MODIFICATION No.: None

This page transmits Revision No.03 of Service Bulletin No.A330-34-3215

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 03 issued to inform the operators that this Service Bulletin is rendered mandatory and to

remove the terminating action in accordance with SB A330-34-3087 (INSTALL ANGLE OF ATTACK

SENSORS ROSEMOUNT PN 0861ED).

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Advantages ADVANTAGES UPDATED R

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

SPARES SPARES UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL SET UPDATED

R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials CONSUMABLE MATERIALS UPDATED R

Equipment EQUIPMENT UPDATED R

Equipement BFEA01 PART MATERIAL SET UPDATED

NOTE UPDATED

R

TOOLING

Tools TOOLS UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 343215- 832-801-001-Inspection TASK SOLUTION UPDATED

NOTE UPDATED

CAUTION UPDATED

R

Subtask 343215-941-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 343215-832-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER UPDATED

NOTE UPDATED

FIN UPDATED

REFERENCES UPDATED

R

Subtask 343215-700-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 2

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 343215-942-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

TASK 343215- 833-801-001-Repair TASK SOLUTION UPDATED

CAUTION UPDATED

NOTE UPDATED

R

Task associated data - 001 Minor editorial or document structure change R

Subtask 343215-941-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 343215-960-001-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 343215-960-002-001 SUBTASK SOLUTION UPDATED

MANPOWER RESSOURCE UPDATED

REFERENCED DOCUMENTATION UPDATED

PART NUMBER UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 343215-700-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 343215-942-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Fig. A-FBAAA

Fig. A-FBAAA Sheet 01 SHEET UPDATED R

Fig. A-FBBAA

Fig. A-FBBAA Sheet 01 SHEET UPDATED R

Appendix 1 : Inspection Report

APPENDIX CONTENT APPENDIX CONTENT UPDATED R

Fig. A-FAAAA

Fig. A-FAAAA Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to add aircraft which can be potentially fitted with the affected PN thanks to IPC

interchangeability conditions and to modify the flow chart accordingly.

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Revision No. 02 issued to update the effectivity and to add Service Bulletin No. A330-34-3228 as

terminating action.

REVISION SEQUENCE

ORIGINAL: May 28/08

REVISION No.: 01 - Dec 03/08

REVISION No. : 02 - Mar 29/10

REVISION No. : 03 - Jul 23/15

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 4

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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 - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The THALES Angle Of Attack (AOA) sensor Part Number (PN) C16291AA, basic standard fitted on SA

and LR aircraft, experience an ageing issue of the heating element, which means that after a given

number of Flight Hours (FH), the vane of the AOA sensor may not be able to de-ice properly in severe

icing conditions.

For aircraft on which one more THALES PN C16291AA sensors are installed, this Inspection Service

Bulletin mandates the periodic functional test of the heating of the AOA sensor and replacing the AOA

sensor if the test fails.

Accomplishment of this Inspection Service Bulletin will allow the detection of any defective THALES PN

C16291AA AOA sensors, up to the embodiment of the terminating action.

The accomplishment of the Service Bulletin No. A330-34-3228 (Install THALES AOA sensors PN

C16291AB) cancels this inspection requirement and cancels the Maintenance Planning Document

(MPD) task 341300-02-1.

The Operational/Maintenance Consequences of this Service Bulletin are covered by the update of the

affected publications detailed in "PLANNING INFORMATION".

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

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB AOA Sensor

EFFECTIVITY

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

38W 43P 44W AAR AAW ABD ACA ACI AEA AFL AFR AIB ALK

ARA ARG AZA AZU BEC BEL BER BGH CRK CRL CSA DAH DAL

DGA DLH EDW EIN ETD EVE FWI G8E GFA GIA GRL HFY HVN

I2L KAL KLM MAS MAU MLM MON MSR OHY PAL QAF QTR RJA

RSY SAI SWR TAE TAM TAP TCX THY TOW TSC UAE USA VKG

WRC XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 34.10.00.038

OEB None

AOT None

SIL None

ISI None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHERS Operator Information Transmission (OIT) No. 999.0036/08

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 343215-832-801-001: Inspection

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

Task 343215-833-801-001: Repair

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

APPENDICES

Appendix 1 : Inspection Report

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 3

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR19

FR18

A

A

A

3FP2

3FP3

A

3FP1

G_SB_343215_5_SUAA_01_00

Figure A-FSUAA - Sheet 01

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 4

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

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

NOTE: This Inspection Service Bulletin is only applicable to A330 aircraft on which

modification No. 58555S30640 (Service Bulletin No. A330-34-3228) is not

embodied.

(1) Models

330-202 330-203 330-223 330-243 330-301 330-302 330-322 330-323

330-341 330-342 330-343

(2) Effectivity by MSN

0030 0037 0045 0054-0055 0070 0072 0082 0086-0087 0095-0096 0111 0116 0120

0127 0138 0140 0143-0144 0148 0153 0162 0165 0171-0172 0181 0183-0184

0188-0189 0191 0195 0198 0200 0203 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

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 1

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@A330

SERVICE BULLETIN

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 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

0927 0931 0934 0939 0943 0946 0950 0952 0962-0963 0965-0966 0970-0971

0973-0975 0979 0989 0991-0992 1000-1002 1008 1011 1014 1018-1019 1021-1022

1026 1029 1031 1033-1034 1039 1041-1043 1045-1048 1053-1055 1057-1059

1065-1066 1072

(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

38W 0401

43P 1053

44W 0970

AAR 0640 0676 0708 0772 0803 0845 1001 1055

AAW 1043

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

0992

AFL 0963 0973 1014 1045 1047 1058 1065 1072

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

0567 0584 0657

AIB 0345 0437

ALK 0303 0306 0311 0313 0404 0456 0627

ARA 0891 0927

ARG 0290 0300

AZA 0272 0339

AZU 0365 0372 0462 0494

BEC 0863

BEL 0030 0037 0045 0082 0095 0229 0249 0324

BER 0288 0322 0403

BGH 0255

CRK 1031 1034 1039 1042 1054 1059

CRL 0285 0320

CSA 0425

DAH 0644 0647 0650 0653 0667

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 2

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

EIN 0269 0330 0397

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

0832 0852 0854 0868 0975 0991

EVE 0833

FWI 0253 0758 0965 1021

G8E 0184 0189 0191

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HFY 0096 0127 0211 0262 1008

HVN 0275 0294 0299 0366 0943 0946 0962 1019

I2L 0625 0632

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

0351 0368 0428 0484 0490 0550

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900

MAS 0116

MAU 0883 1057

MLM 0451

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

OHY 0072 0087 0143 0353 0362

PAL 0183 0188 0198 0200 0203

QAF 0487 0605

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 0979 1002

RSY 0120 0171

SAI 0055 0070 0086

SWR 1000 1018 1026 1029

TAE 0348

TAM 0232 0238 0247 0259 0361 0466 0472 0700

TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486 0877 0899 0904

0914 0934

TCX 0254 0266 0301 0398

THY 0463 0504 0869 0874 0876 0939

TOW 1033 1046

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 0452 0455 0491 0509 0518 0525 0536

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 3

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SERVICE BULLETIN

OPERATOR MSN

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

VKG 0309 0349 0356 0357

WRC 0296

XAX 0054 0952 0974 1048 1066

XLF 0501 0635

(4) Configuration by MSN

MSN CONFIGURATION

0030 0037 0045 0054 0055 0070 0072 0082 0086 0087 0095

0096 0111 0116 0120 0127 0138 0140 0143 0144 0148 0153

0162 0165 0171 0172 0181 0183 0184 0188 0189 0191 0195

0198 0200 0203 0206 0211 0219 0222 0223 0226 0229 0230

0232 0238 0240 0241 0247 0248 0249 0250 0251 0253 0254

0255 0256 0258 0259 0261 0262 0265 0266 0267 0269 0271

0272 0275 0276 0277 0279 0281 0283 0284 0285 0286 0287

0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303

0305 0306 0308 0309 0311 0312 0313 0314 0315 0316 0317

0320 0322 0323 0324 0326 0328 0330 0333 0334 0337 0338

0339 0340 0342 0343 0344 0345 0348 0349 0350 0351 0353

0356 0357 0361 0362 0365 0366 0368 0369 0370 0372 0375

0380 0382 0384 0388 0392 0396 0397 0398 0400 0401 0403

0404 0408 0409 0412 0419 0422 0425 0427 0428 0437 0441

0443 0448 0451 0452 0455 0456 0458 0461 0462 0463 0465

0466 0472 0473 0477 0480 0481 0484 0486 0487 0489 0490

0491 0494 0498 0500 0501 0502 0503 0504 0505 0507 0509

0510 0511 0516 0518 0519 0521 0524 0525 0526 0533 0536

0542 0549 0550 0551 0552 0567 0570 0571 0576 0578 0579

0584 0588 0591 0597 0600 0605 0609 0610 0612 0614 0616

0618 0620 0621 0623 0625 0627 0629 0631 0632 0633 0635

0636 0637 0638 0640 0642 0644 0645 0647 0648 0650 0653

0657 0658 0659 0663 0666 0667 0670 0674 0676 0680 0682

0683 0684 0686 0687 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 0833 0834 0843 0845 0849 0852 0854 0857 0858

0859 0863 0865 0868 0869 0874 0876 0877 0883 0891 0893

0896 0899 0900 0904 0905 0907 0913 0914 0918 0922 0927

0931 0934 0939 0943 0946 0950 0952 0962 0963 0965 0966

0970 0971 0973 0974 0975 0979 0989 0991 0992 1000 1001

1002 1008 1011 1014 1018 1019 1021 1022 1026 1029 1031

1033 1034 1039 1041 1042 1043 1045 1046 1047 1048 1053

1054 1055 1057 1058 1059 1065 1066 1072

001

(5) Configuration definition

**CONF 001

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

standard configuration.

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 4

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SERVICE BULLETIN

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The THALES Angle Of Attack (AOA) sensor Part Number (PN) C16291AA, basic

standard fitted on SA and LR aircraft, experience an ageing issue of the heating

element, which means that after a given number of Flight Hours (FH), the vane of the

AOA sensor may not be able to de-ice properly in severe icing conditions.

(2) Objective/Action

For aircraft on which one more THALES PN C16291AA sensors are installed, this

Inspection Service Bulletin mandates the periodic functional test of the heating of the

AOA sensor and replacing the AOA sensor if the test fails.

(3) Advantages

Accomplishment of this Inspection Service Bulletin will allow the detection of any

defective THALES PN C16291AA AOA sensors, up to the embodiment of the

terminating action.

The accomplishment of the Service Bulletin No. A330-34-3228 (Install THALES

AOA sensors PN C16291AB) cancels this inspection requirement and cancels the

Maintenance Planning Document (MPD) task 341300-02-1.

(4) Operational/Maintenance Consequences

The Operational/Maintenance Consequences of this Service Bulletin are covered by the

update of the affected publications detailed in "PLANNING INFORMATION".

D. DESCRIPTION

NOTE: To accomplish the repair of the affected AOA sensor(s) you have two

possibilities :

- either you replace them as per AMM Task 34-11-19-000-801 and AMM

Task 34-11-19-400-801 in accordance with SUBTASK 343215-960-001

001 OPTION 1 - Replace the Affected AOA Sensor(s) ,

- or you replace them as per Service Bulletin in accordance with SUBTASK

343215-960-002 001 OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action .

To accomplish this Service Bulletin it is necessary to :

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 5

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@A330

SERVICE BULLETIN

Task 343215-832-801-001: Inspection

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

Task 343215-833-801-001: Repair

(1) OPTION 1 - Replace the Affected AOA Sensor(s)

(2) OPTION 2 - Replace the Affected AOA Sensors by Another PN as Terminating

Action

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

Accomplishment of this Inspection Service Bulletin must be done before 17,000 Flight

Hours (FH), since the aircraft first flight.

For the aircraft which were in the effectivity of this Service Bulletin at original issue and

which have exceeded this threshold, a grace period of six months has been agreed from

the issue of this Inspection Service Bulletin at revision 00 for the first inspection.

For the aircraft which were added in the effectivity of this Service Bulletin at revision 01

and which have exceeded this threshold, a grace period of six months has been agreed

from the issue of this Inspection Service Bulletin at revision 01 for the first inspection.

Repeat the inspection of each THALES AOA sensor PN C16291AA at interval not

exceeding 3,800 FH.

NOTE: The accomplishment of the Service Bulletin No. A330-34-3228 as

terminating action cancels this inspection.

F. APPROVAL

The technical content of this document is approved under EASA Design Organisation

Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

G. MANPOWER

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

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

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

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

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

included.

Task 343215-832-801-001: Inspection

Get Access 0.50

On Aircraft

Do a Detailed Inspection of the Three AOA Sensors

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

1.75

Tests 0.25

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 343215-833-801-001: Repair

Get Access 0.50

On Aircraft

OPTION 1 - Replace the Affected AOA Sensor(s) 3.50

OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action

0.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

NOTE: The manpower in the TASK 343215-833-801 001 Repair is for the

replacement of one AOA sensor.

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 12-34-24 30-31-00 34-11-19

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

Service Bulletin (SB) A330-34-3228

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

K. PUBLICATION AFFECTED

A new Maintenance Planning Document (MPD) task 341300-02-1 has been created in A330

MPD to cover this repetitive inspection.

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Vendor parts are to be purchased from :

Equipment BFEA01 THALES AVIONICS

AIR TRANSPORT AVIONICS

105 Avenue du general Eisenhower

BP 63647

31036 TOULOUSE CEDEX 1

FRANCE

(2) Price and Availability

Equipment BFEA01

No AIRBUS kit will be provided.

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

B. INDUSTRY SUPPORT INFORMATION

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

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this Inspection Service Bulletin it is necessary to use the expendable

parts listed in the AMM Task 34-11-19-400-801.

(2) Components

None

(3) Equipment

For the replacement of the AOA sensors as described in SUBTASK 343215-960-001

001 OPTION 1 - Replace the Affected AOA Sensor(s) :

Equipment BFEA01

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

NOTES

C16291AA 3 SENSOR C16291AA

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

NOTE: The components listed above are only necessary if found affected AOA

sensors. The quantity of these items are to be ordered as required.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

To accomplish this Inspection Service Bulletin it is necessary to use the tools listed in

AMM Task 30-31-00-720-801.

(3) Special Tools

None

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 343215-832-801-001 - 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 THERE IS 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 of acronyms.

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.

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: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

Task Associated Data

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

A. GENERAL

(1) Subtask 343215-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 343215-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 30-31-00-720-801

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

12-34-24-860-802.

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

(c) Open the Avionics Access Door 811.

(d) Open the passenger/crew door(s).

(e) Do the preparation procedure as specified in the functional test of the heating of the

AOA sensor, refer to AMM Task 30-31-00-720-801.

C. PROCEDURE

(1) Subtask 343215-832-001-001 - Do a Detailed Inspection of the Three AOA Sensors

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

Manpower Resources

Manhours 1.75

Minimum number of person 1

Subtask elapsed time 1.75

Skills NON SPECIFIC

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 30-31-00-720-801

Fig. A-FBAAA

Areas to be Inspected

Sheet 01

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) Do a check of the part number of the three AOA sensors (FINs 3FP1, 3FP2 and

3FP3).

Refer to figure Fig. A-FBAAA Sheet 01

1 If the affected PN C16291AA is found installed on any of the three positions:

a Do the functional test of the heating of the AOA sensors PN C16291AA

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

Refer to AMM Task 30-31-00-720-801

Refer to Figure Fig. A-FBBAA Sheet 01

NOTE: Refer to AMM Task 30-31-00-720-801 which requests to

perform three times the record of the maximum current

(Imax).

<1> If the maximun current (Imax) found is equal or less than 1.2A:

<a> Before next flight, replace the affected AOA sensor in

accordance with the SUBTASK 343215-960-001-001 Replace

the Affected AOA sensor(s) and

<b> Send the Inspection Report to Airbus and

<c> Repeat the Task 343215-832-801-001 at the interval given in

PLANNING INFORMATION paragraph 1.E.(2)

OR

<d> Do the SUBTASK 343215-960-002-001 Replace the Affected

AOA Sensors by Another PN as Terminating Action and

<e> Send the Inspection Report to Airbus

[1] If all AOA Sensors found upgraded to PN C16291AB

[a] No further action.

[2] If all AOA Sensors are not found upgraded to PN

C16291AB on the three positions (3FP1, 3FP2 and 3FP3):

[a] Repeat the Task 343215-832-801-001 at the interval

given in PLANING INFORMATION paragraph 1.E.(2)

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<2> If the maximun current (Imax) found is more than 1.2A:

<a> Send the Inspection Report to Airbus and

<b> Repeat the Task 343215-832-801-001 at the interval given in

PLANING INFORMATION paragraph 1.E.(2)

OR

<c> Do the SUBTASK 343215-960-002-001 Replace the Affected

AOA Sensors by Another PN as Terminating Action and

[1] Send the Inspection Report to Airbus and

[a] No further action.

[2] If all AOA Sensors are not found upgraded to PN

C16291AB on the three positions (3FP1, 3FP2 and 3FP3):

[a] Repeat the Task 343215-832-801-001 at the interval

given in PLANING INFORMATION paragraph 1.E.(2)

2 If the PN C16291AA is not found installed on the three positions (3FP1, 3FP2

and 3FP3)

a No further action

D. TEST

(1) Subtask 343215-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 30-31-00-720-801

(a) Job set-up :

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

after the functional test of heating of the AOA sensors (Refer to AMM Task

30-31-00-720-801).

(b) Procedure :

1 Do the operational test of the probe ice protection (Refer to AMM Task

30-31-00-720-801).

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

E. CLOSE-UP

(1) Subtask 343215-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 30-31-00-720-801

(a) Do the close-up procedure after the functional test of the heating of the AOA

sensor (Refer to AMM Task 30-31-00-720-801).

(b) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(c) Close the passenger/crew door(s).

(d) Close the Avionics Access Door 811 .

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

(f) Remove the access platform(s).

(g) Put the aircraft back to its initial configuration.

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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This Page Intentionally Left Blank

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SERVICE BULLETIN

Task 343215-833-801-001 - Repair

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 THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

A. GENERAL

(1) Subtask 343215-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 343215-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 34-11-19-400-801

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(a) Do the preparation procedure as specified in the removal of the AOA sensors (FINs

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

C. PROCEDURE

NOTE: To accomplish the repair of the affected AOA sensor(s) you have two

possibilities :

- either you replace them as per AMM Task 34-11-19-000-801 and AMM

Task 34-11-19-400-801 in accordance with SUBTASK 343215-960-001

001 OPTION 1 - Replace the Affected AOA Sensor(s) ,

- or you replace them as per Service Bulletin in accordance with SUBTASK

343215-960-002 001 OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action .

(1) Subtask 343215-960-001-001 - OPTION 1 - Replace the Affected AOA Sensor(s)

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C16291AA 3 SENSOR

NOTE: The components listed above are only necessary if found affected AOA

sensors. The quantity of these items are to be ordered as required.

References

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

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) Depending on the result of the inspection, replace the affected AOA sensor(s).

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

Refer to Figure Fig. A-FBBAA

1 Remove :

FIN 3FP1

1 AOA Sensor C16291AA

and/or

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FIN 3FP2

1 AOA Sensor C16291AA

and/or

FIN 3FP3

1 AOA Sensor C16291AA

2 Install :

FIN 3FP1

1 AOA Sensor C16291AA

and/or

FIN 3FP2

1 AOA Sensor C16291AA

and/or

FIN 3FP3

1 AOA Sensor C16291AA

(2) Subtask 343215-960-002-001 - OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action

Manpower Resources

Manhours 0.00

Minimum number of person 0

Subtask elapsed time 0.00

Skills NON SPECIFIC

References

Service Bulletin (SB) A330-34-3228

(a) Do the replacement of the three THALES AOA sensors PN C16291AA by PN

C16291AB as per Service Bulletin No. A330-34-3228.

D. TEST

(1) Subtask 343215-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

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

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(a) Job set-up :

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

after the installation of the AOA sensors (FINs 3FP1, 3FP2 and 3FP3) (Refer

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

(b) Procedure :

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

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

E. CLOSE-UP

(1) Subtask 343215-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Do the close-up procedure after the installation of the AOA sensors (FINs 3FP1,

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

(b) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(c) Close the passenger/crew door(s).

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

(e) Remove the access platform(s).

(f) Put the aircraft back to its initial configuration.

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

**CONF ALL

FR19

FR18

A

A

A

3FP2

3FP3

A

3FP1

AREA TO BE INSPECTED

G_SB_343215_5_BAAA_01_02

Figure A-FBAAA - Sheet 01

Areas to be Inspected

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SERVICE BULLETIN

**CONF ALL

YES

OR

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

NO FURTHER ACTION

DO THE FUNCTIONAL TEST OF THE HEATING OF THE

AOA SENSOR(S) AT THE THRESHOLD GIVEN IN THE

PLANNING INFORMATION PARAGRAPH 1.E.(2) AS PER

SUBTASK 343215−832−001 001

I MAX CURRENT 1.2 A

DO A DETAILED VISUAL INSPECTION OF THE

THREE AOA SENSORS (FINS 3FP1, 3FP2 AND 3FP3).

DO A CHECK OF THE PART NUMBER

C16291AA OF THE THREE AOA SENSORS

YES PN C16291AA

INSTALLED

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

NO FURTHER ACTION

NO

OR

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

REPEAT THE FUNCTIONAL

TEST AT INTERVAL GIVEN IN

THE PLANNING INFORMATION

PARAGRAPH 1.E.(2).

NO

REPLACE AFFECTED THALES

AOA SENSOR(S) PN C16291AA

BY THE NEW SAME PN AS PER

SUBTASK 343215−960−001 001

REPLACE THALES AOA

SENSOR(S) PN C16291AA BY

ANOTHER PN AS PER

SUBTASK 343215−960−002 001

NO AOA SENSORS NO UPGRADED TO

PN C16291AB

YES

THE FUNCTIONAL TEST

 AT INTERVAL GIVEN IN THE

PLANNING INFORMATION

PARAGRAPH 1.E.(2).

REPEAT

ALL

G_SB_343215_5_BBAA_01_02

Figure A-FBBAA - Sheet 01

Flow Chart

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SERVICE BULLETIN

Appendix 1 : Inspection Report

**CONF ALL

The results of the inspection, including no findings, replacement or actions to be done, must be

forwarded to AIRBUS, on the attached inspection report sheet.

DATE: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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SERVICE BULLETIN

Appendix 1 : Inspection Report

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A330−34−3215

DATE OF INSPECTION :

INSPECTION METHOD : DETAILED

INSPECTION

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING

AFS/NAV/COM SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: inspection.results@airbus.com

FAX +33 (0)5 61 93 44 25

I MAX CURRENT > 1.2A

3FP1 3FP2

REPLACEMENT OF AOA

FIN 3FP3

SENSOR

YES NO YES NO YES NO

YES NO YES NO YES NO

I MAX RECORDED

C16291AA

C16291AB AS PER

C16291AA C16291AA

SERVICE BULLETIN 

NEW AOA SENSOR PN

INSTALLED

No. A330−34−3228

C16291AB AS PER C16291AB AS PER

SERVICE BULLETIN 

No. A330−34−3228

SERVICE BULLETIN 

No. A330−34−3228

G_SB_343215_5_AAAA_01_05

Figure A-FAAAA - Sheet 01

Inspection Report

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SERVICE BULLETIN

REPORTING SHEET

TITLE: NAVIGATION - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

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: May 28/08 SERVICE BULLETIN No.: A330-34-3215

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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: May 28/08 SERVICE BULLETIN No.: A330-34-3215

REVISION No.: 03 - Jul 23/15 Page: 1

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