# @A330 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. ATA SYSTEM: 34 

### TITLE: NAVIGATION - SENSORS POWER SUPPLY AND SWITCHING - INSTALL THALES ANGLE OF ATTACK SENSORS PN C16291AB **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 49228S16346 58555S30640 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES The design of the heater of THALES Angle Of Attack (AOA) sensor PN C16291AA suffers from an ageing issue, which affects the heating efficiency of the vane The loss of AOA heating efficiency appears over a number of flight hours which depends on the operational life of the AOA sensors, especially the number of flight cycles (vibration modes), power ON/OFF sequences, handling, etc... accumulated by the vane. At system level , consequences are a possible loss of windshear and/or alpha protection and/or spurious reversion into Alternate law. Airbus recommends operators to perform a recurrent functional test of the AOA heating on affected AOA sensor PN C16291AA, as per Inspection Service Bulletin No. A330-34-3215 (refer to OIT ref. SE999.0036/08/BB dated on 2nd May 2008). In order to increase the reliability of AOA sensors and to reduce the probability of vane heating failures, the vane of THALES AOA probe PN C16291AA has been redesigned. This Service Bulletin is published to inform all operators of A330 aircraft of the issue of THALES AVIONICS Service Bulletin No. C16291A-34-009. This Service Bulletin proposes replacement of the three Thales AOA sensors PN 45150320 or PNC16291AA by three new THALES AOA sensors PN C16291AB.

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 1 5

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# @A330 SERVICE BULLETIN SUMMARY Accomplishment of this Service Bulletin improves the reliability of AOA sensors and cancels the inspection requirements of Service Bulletins No. A330-34-3215. The consequences on schedule maintenance activities of the embodiment of this Service Bulletin are that the Maintenance Planning Document 341300-02-1 will be no more required after the accomplishment of this Service Bulletin. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED CANCELS INSPECTION SB YES POTENTIAL AD NO 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 MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA01 1 See SB Sensor **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA01 1 See SB Sensor EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

51W 78V 97X AAR AAW ACA ACI ADH AEA AFL AFR ALK BEL BMA BTV CRL CYP DAH DGA DLH EDW EIN ETD FWI GFA GIA GRL HFY HVN I2L IAC IWD IYE JAI KAL KFR KLM LTU LVG MAS MAU MLM MON MPD MSR MXA NWA OBS PAL QAF QTR STZ SWR TAM TAP TCX THY TSC UAE USA VKG VLK XAX XLF CONCURRENT REQUIREMENTS **CONF 001 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification : Service Bulletin No. A330-34-3103 Mod. No. 49228S16346
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# @A330 SERVICE BULLETIN SUMMARY **CONF 002 None REFERENCES / REPERCUSSIONS **CONF ALL TFU 34.10.00.038 OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER OIT SE999.0036/08/BB NATURE OF THE WORK AIRCRAFT NO EQUIPMENT YES HARD YES SOFT NO OBRM NO MANPOWER **CONF 001 Task 343228-831-801-001: Modification TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 Additional manhours related to Vendor SB; refer to: Modify the AOA sensors 3FP1, 3FP2 and 3FP3 THALES AVIONICS Service Bulletin No. C16291A-34-009 **CONF 002 Task 343228-831-801-001: Modification TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 APPENDICES **CONF ALL None

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 3 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF ALL

FR19 FR18 

### A

3FP1 3FP2 3FP3 

### A **A**

TYPICAL INSTALLATION 

## A

G_SB_343228_5_SUAA_01_00 Figure A-FSUAA - Sheet 01

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 4 5

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# @A330 SERVICE BULLETIN

AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 ATA SYSTEM: 34 

### TITLE: NAVIGATION - SENSORS POWER SUPPLY AND SWITCHING - INSTALL THALES ANGLE OF ATTACK SENSORS PN C16291AB MODIFICATION No.: 49228S16346 58555S30640 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE: This modification is embodied before delivery on aircraft MSN 1069 , 1071 , 1075 and subsequent. (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 0059 0067 0069-0070 0072-0073 0077 0082 0086-0087 0095-0096 0100 0107 0110-0111 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 DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 1 5

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# @A330 SERVICE BULLETIN

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 0949-0950 0952 0961-0963 0965-0966 0968 0970-0971 0973-0975 0977 0979 0989 0991-0992 0999-1002 1008 1011 1014 1018-1019 1021-1022 1024 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 51W 1002 1019 78V 1033 1046 97X 1053 AAR 0640 0676 0708 0772 0803 0845 1001 1055 AAW 0999 1024 1043 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 ADH 0272 0339 AEA 0733 0745 0749 0814 0931 0950 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 ALK 0303 0306 0311 0313 BEL 0030 0037 0045 0082 BMA 0398 0401 0404 BTV 0330 CRL 0285 0320 CYP 0505 0526 DAH 0644 0647 0650 0653 0667 DGA 0240 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905 0913 0922 0989 EDW 0369 EIN 0055 0059 0086 0269 0397 ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852 0854 0868 0975 0991 FWI 0253 0758 0965 1021 GFA 0276 0281 0286 0287 0334 0340 0992 GIA 0138 0140 0144 0148 0153 0165

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# @A330 SERVICE BULLETIN

OPERATOR MSN GRL 0230 HFY 0096 1008 HVN 0087 0255 0262 0275 0366 I2L 0205 0211 IAC 0353 0362 IWD 0072 0670 0833 IYE 0625 0632 JAI 0751 0807 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0425 0428 0484 0490 0550 KFR 0874 0891 0927 0939 0946 KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 LTU 0120 0127 0171 0403 LVG 0551 0597 0627 MAS 0067 0069 0073 0077 0095 0100 0107 0110 0116 0119 0143 0290 0296 0300 MAU 0883 1057 MLM 0863 MON 0261 0265 MPD 0943 0962 0970 0979 1031 1034 1039 1042 1054 1059 MSR 0600 0610 0666 0683 0696 0709 0726 MXA 0966 0971 NWA 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 OBS 0461 PAL 0183 0184 0188 0189 0191 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 STZ 0324 SWR 0229 0249 0288 0291 0294 0299 0322 0343 1000 1018 1026 1029 TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0869 0876 0949 0961 0968 0977 TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934 TCX 0254 0266 0301 0309 0357 0427 0456 0795 THY 0463 0504 TSC 0111 0250 0271 0480 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0365 0372 0382 0384 0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509 0518 0525 0536 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041 VKG 0349 0356 VLK 0070 XAX 0054 0952 0974 1048 1066

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# @A330 SERVICE BULLETIN

OPERATOR MSN XLF 0501 0635 (4) Configuration by MSN MSN CONFIGURATION 0030 0037 0045 0054 0055 0059 0067 0069 0070 0072 0073 0077 0082 0086 0087 0095 0096 0100 0107 0110 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 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 0949 0950 0952 0961 0962 0963 0965 0966 0968 0970 0971 0973 0974 0975 0977 0979 0989 0991 0992 0999 1000 1001 1002 1008 1011 1014 1018 1019 1021 1022 1024 1026 1029 1031 1033 1034 1039 1041 1042 1043 1045 1046 1047 1048 1053 1054 1055 1057 1058 1059 1065 1066 1072 001 002

(5) Configuration definition **CONF 001 Config. 01 is valid for aircraft on which the Angle Of Attack sensor PN C16291AA is installed.

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 4 5

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# @A330 SERVICE BULLETIN

**CONF 002 Config. 02 is valid for aircraft on which the Angle Of Attack sensor PN 45150320 is installed. NOTE: Selection of config. 01 or config. 02 depends on the PN installed on aircraft. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Equipment BFEA01 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Component COMPA01 1 **CONF ALL B. CONCURRENT REQUIREMENTS **CONF 001 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification : Service Bulletin No. A330-34-3103 Mod. No. 49228S16346 **CONF 002 None **CONF ALL C. REASON (1) History The design of the heater of THALES Angle Of Attack (AOA) sensor PN C16291AA suffers from an ageing issue, which affects the heating efficiency of the vane The loss of AOA heating efficiency appears over a number of flight hours which depends on the operational life of the AOA sensors, especially the number of flight cycles (vibration modes), power ON/OFF sequences, handling, etc... accumulated by the vane. At system level , consequences are a possible loss of windshear and/or alpha protection and/or spurious reversion into Alternate law. Airbus recommends operators to perform a recurrent functional test of the AOA heating on affected AOA sensor PN C16291AA, as per Inspection Service Bulletin No. A330-34-3215 (refer to OIT ref. SE999.0036/08/BB dated on 2nd May 2008).

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 5 5

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# @A330 SERVICE BULLETIN (2) Objective/Action In order to increase the reliability of AOA sensors and to reduce the probability of vane heating failures, the vane of THALES AOA probe PN C16291AA has been redesigned. This Service Bulletin is published to inform all operators of A330 aircraft of the issue of THALES AVIONICS Service Bulletin No. C16291A-34-009. This Service Bulletin proposes replacement of the three Thales AOA sensors PN 45150320 or PNC16291AA by three new THALES AOA sensors PN C16291AB. (3) Advantages Accomplishment of this Service Bulletin improves the reliability of AOA sensors and cancels the inspection requirements of Service Bulletins No. A330-34-3215. (4) Operational/Maintenance Consequences The consequences on schedule maintenance activities of the embodiment of this Service Bulletin are that the Maintenance Planning Document 341300-02-1 will be no more required after the accomplishment of this Service Bulletin. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 343228-831-801-001: Modification (1) Remove the AOA sensors 3FP1, 3FP2 and 3FP3 (2) Modify the AOA sensors 3FP1, 3FP2 and 3FP3 (3) Install the AOA sensors 3FP1, 3FP2 and 3FP3 **CONF 002 Task 343228-831-801-001: Modification (1) Replace the AOA sensors 3FP1, 3FP2 and 3FP3 **CONF ALL E. COMPLIANCE (1) Classification RECOMMENDED (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 6 5

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# @A330 SERVICE BULLETIN

F. APPROVAL Approved under EASA Design Organisation Approval No. EASA21J.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 343228-831-801-001: Modification Get Access 0.50 On Aircraft Remove the AOA sensors 3FP1, 3FP2 and 3FP3 1.50 Install the AOA sensors 3FP1, 3FP2 and 3FP3 1.50 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 Additional manhours related to Vendor SB; refer to: Modify the AOA sensors 3FP1, 3FP2 and 3FP3 THALES AVIONICS Service Bulletin No. C16291A-34-009 **CONF 002 Task 343228-831-801-001: Modification Get Access 0.50 On Aircraft Replace the AOA sensors 3FP1, 3FP2 and 3FP3 3.00 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 Additional manhours related to Vendor SB; refer to:

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# @A330 SERVICE BULLETIN

**CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 12-34-24 34-11-19 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-34-3103 A330-34-3215 Vendor Service Bulletin (VSB) THALES AVIONICS Service Bulletin No. C16291A-34-009 **CONF 002 Aircraft Maintenance Manual (AMM) 12-34-24 34-11-19 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-34-3215 **CONF ALL K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL) Illustrated Parts Catalog (IPC) 34-11-01 34-11-19 Maintenance Planning Document (MPD) 34-13-00 L. INTERCHANGEABILITY/MIXABILITY **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES AOA sensor C16291AA C16291AB 01 YES (1) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved.
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# @A330 SERVICE BULLETIN

NOTE (1): Authorized without specific configuration / condition : it is possible to mix old and new PN on a same aircraft. **CONF 002 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES AOA sensor 45150320 C16291AB 01 YES (1) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. NOTE (1): Authorized without specific configuration / condition : it is possible to mix old and new PN on a same aircraft. **CONF ALL M. SPARES AOA sensor 45150320 AOA sensor C16291AA

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 9 5

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# @A330 SERVICE BULLETIN

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# @A330 SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Equipment BFEA01 Modification of removed equipment should be negotiated directly with THALES AVIONICS as per instructions given in Service Bulletin No C16291A-34-009. Vendor parts are to be purchased from : Component COMPA01 THALES AVIONICS Rue Marcel Dassault 86101 CHATELLERAULT FRANCE (2) Price and Availability

Equipment BFEA01 Refer to the vendor Service Bulletin No C1629A-34-009 for the equipment modification sales terms. Component COMPA01 Procurement terms for the equipment must be negotiated with the equipment supplier. (MATERIAL INFORMATION). B. INDUSTRY SUPPORT INFORMATION Refer to the Vendor Service Bulletin (VSB) for the industry support terms. Refer to the paragraph : ’Price and Availability’. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None

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# @A330 SERVICE BULLETIN (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES C16291AB 3 SENSOR 45150320 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. (3) Equipment Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES C16291AB 3 SENSOR C16291AA 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

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# @A330 SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 343228-831-801-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone 121 122 Modified FIN 3FP1 3FP2 3FP3 Manpower TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 Additional manhours related to Vendor SB; refer to: THALES AVIONICS Service Bulletin No. C16291A-34-009 **CONF 002 Zone 121 122 Modified FIN 3FP1 3FP2 3FP3

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# @A330 SERVICE BULLETIN
Manpower TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 4.50 Additional manhours related to Vendor SB; refer to: **CONF ALL A. GENERAL **CONF 001 (1) Subtask 343228-839-001-001 - 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 343228-839-001-001 - 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 ALL B. PREPARATION **CONF 001 (1) Subtask 343228-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 34-11-19-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802) (b) Do the preparation procedure as specified in the removal of the AOA sensors (3FP1, 3FP2 and 3FP3), (Refer to AMM Task 34-11-19-000-801).

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 14 5

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# @A330 SERVICE BULLETIN

**CONF 002 (1) Subtask 343228-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 34-11-19-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802) (b) Do the preparation procedure as specified in the removal of the AOA sensors (3FP1, 3FP2 and 3FP3), (Refer to AMM Task 34-11-19-000-801). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 343228-900-004-001 - Remove the AOA sensors 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 (a) Remove the AOA sensors (Refer to AMM Task 34-11-19-000-801) : FIN 3FP1 1 AOA sensor C16291AA and FIN 3FP2 1 AOA sensor C16291AA and

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 15 5

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# @A330 SERVICE BULLETIN

FIN 3FP3 1 AOA sensor C16291AA

(2) Subtask 343228-831-003-001 - Modify the AOA sensors 3FP1, 3FP2 and 3FP3 References Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-009 (a) Modify the AOA sensors (3FP 1, 3FP2 and 3FP3) : Refer to THALES AVIONICS Service Bulletin No. C16291A-34-009. (3) Subtask 343228-900-003-001 - Install the AOA sensors 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 Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES C16291AB 3 SENSOR References Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801 (a) Install the AOA sensors (Refer to AMM Task 34-11-19-400-801) : FIN 3FP1 1 AOA sensor C16291AB and FIN 3FP2 1 AOA sensor C16291AB and FIN 3FP3 1 AOA sensor C16291AB

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 16 5

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# @A330 SERVICE BULLETIN

**CONF 002 (1) Subtask 343228-960-001-002 - Replace the AOA sensors 3FP1, 3FP2 and 3FP3 Work Zones and Access Panels Zone Access/Work location 121 122 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES C16291AB 3 SENSOR References Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801 Task 34-11-19-400-801 (a) Remove the AOA sensors (Refer to AMM Task 34-11-19-000-801) : FIN 3FP1 1 AOA sensor 45150320 and FIN 3FP2 1 AOA sensor 45150320 and FIN 3FP3 1 AOA sensor 45150320 (b) Install the AOA sensors (Refer to AMM Task 34-11-19-400-801) : FIN 3FP1 1 AOA sensor C16291AB and FIN 3FP2 1 AOA sensor C16291AB and DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 17 5

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# @A330 SERVICE BULLETIN

FIN 3FP3 1 AOA sensor C16291AB **CONF ALL D. TEST **CONF 001 (1) Subtask 343228-700-001-001 - 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 sensors (3FP1, 3FP2, 3FP3), (Refer to AMM Task 34-11-19-400-801). (b) Procedure : 1 Do a test procedure as specified after the installation of the AOA sensors (3FP1, 3FP2, 3FP3) (Refer to AMM Task 34-11-19-400-801). **CONF 002 (1) Subtask 343228-700-001-001 - 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 sensors (3FP1, 3FP2, 3FP3), (Refer to AMM Task 34-11-19-400-801). (b) Procedure : 1 Do a test procedure as specified after the installation of the AOA sensors (3FP1, 3FP2, 3FP3) (Refer to AMM Task 34-11-19-400-801).

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 18 5

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# @A330 SERVICE BULLETIN

**CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 343228-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in the installation of the AOA sensors (3FP1, 3FP2, 3FP3), (Refer to AMM Task 34-11-19-400-801). (c) Restore the systems and aircraft to normal operating condition. **CONF 002 (1) Subtask 343228-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in the installation of the AOA sensors (3FP1, 3FP2, 3FP3), (Refer to AMM Task 34-11-19-400-801). (c) Restore the systems and aircraft to normal operating condition.

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 19 5

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: NAVIGATION - SENSORS POWER SUPPLY AND SWITCHING - INSTALL THALES ANGLE OF ATTACK SENSORS PN C16291AB MODIFICATION No.: 49228S16346 58555S30640 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: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 1 5

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# @A330 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - Is this SB easy to understand ? Y / N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Oct 07/09 SERVICE BULLETIN No.: A330-34-3228 REVISION No.: 00 - Oct 07/09 Page: 1 5

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