# @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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 34 

### TITLE: NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY AOA PROBE FLAT PLATE MODIFICATION No.: 203295S32646 This page transmits Revision No.01 of Service Bulletin No.A330-34-3293 ADDITIONAL WORK **CONF ALL Additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 issued to modify the installation of the two AOA cover plates on RH side in order to ensure that both plates are flush with the fuselage (Refer to SBIT No. 13-0017), and to apply minor changes. CHANGES FRONT MATTER NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY AOA PROBE FLAT PLATE CONFIGURATION UPDATED R
SUMMARY MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE UPDATED R MANPOWER MANPOWER UPDATED R Fig. A-FSAAA FIGURE SOLUTION UPDATED R Fig. A-FSAAA Sheet 01 SHEET UPDATED R Fig. A-FSAAA Sheet 02 SHEET UPDATED R Fig. A-FSAAA Sheet 03 SHEET ADDED N

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 1 5

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# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONF 001 CONFIGURATION DEFINITION UPDATED R Material Effectivity MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED MATERIAL SET UPDATED R
COMPLIANCE Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R MANPOWER MANPOWER 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 CMLA01 CONSUMABLE MATERIAL SET UPDATED CONSUMABLE UPDATED R Components COMPONENTS UPDATED R Component COMPA02 PART MATERIAL SET UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

Component COMPA03 PART MATERIAL SET ADDED N ACCOMPLISHMENT INSTRUCTIONS TASK 343293- 831-801-001-Modification of the AOA sensor plates Subtask 343293-831-001-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 2 5

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# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 343293-831-002-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED FIGURE REFERENCE UPDATED CONFIGURATION UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED NOTE UPDATED R

Subtask 343293-700-001-001 SUBTASK SOLUTION UPDATED NOTE UPDATED REFERENCED DOCUMENTATION UPDATED R
Subtask 343293-942-001-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED QUANTITY UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

TASK 343293- 831-802-001-Additional Work TASK SOLUTION ADDED N Task associated data - 001 TASK ASSOCIATED DATA ADDED N Subtask 343293-910-002-001 SUBTASK SOLUTION ADDED N Subtask 343293-839-002-001 SUBTASK SOLUTION ADDED N Subtask 343293-941-002-001 SUBTASK SOLUTION ADDED N Subtask 343293-831-004-001 SUBTASK SOLUTION ADDED N Subtask 343293-700-002-001 SUBTASK SOLUTION ADDED N Subtask 343293-942-002-001 SUBTASK SOLUTION ADDED N Fig. A-FBAAA FIGURE SOLUTION UPDATED R Fig. A-FBAAA Sheet 01 SHEET UPDATED R Fig. A-FBAAA Sheet 02 SHEET UPDATED R Fig. A-FBCAA FIGURE SOLUTION ADDED N Fig. A-FBCAA Sheet 01 SHEET ADDED N Fig. A-FBCAA Sheet 02 SHEET ADDED N Fig. A-FBDAA FIGURE SOLUTION ADDED N Fig. A-FBDAA Sheet 01 SHEET ADDED N Fig. A-FBDAA Sheet 02 SHEET ADDED N 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.
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 3 5

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# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET HISTORY OF PREVIOUS REVISIONS No previous revision REVISION SEQUENCE ORIGINAL: Jan 31/13 REVISION No. : 01 - Jun 12/13

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 4 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. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 34 

### TITLE: NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY AOA PROBE FLAT PLATE **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 203295S32646 MINOR None NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following a recent in-service event, as a precautionary measure, Airbus requires to suspend the installation of the AOA (Angle Of Attack) conic plates as per Operator Information Transmission (OIT) No. 999.0086/12, currently performed through an Airbus monitored campaign with Service Bulletin No. A330-34-3255. This modification requires the removal of the conic plates PN F3411060200000 and PN F3411060900000, and the installation of flat plates PN F3411007920200 (LH) / PN F3411007920300 (RH). Also, it requires to change the 3 AOA Sensor Protection Covers (FINs 7955ME, 7956ME and 7957ME) stored in Flight Kit No 2 (FIN 7500NW). Refer to OIT No. 999.0086/12 and FOT No. 999.0089/12 for further explanations. For aircraft already fitted with the AOA conic plates through retrofit or from production, Airbus released associated operational recommendations in an FOT No. 999.0089/12, the Operations Engineering Bulletin (OEB) 45 and Flight Manual (FM) Temporary Revision 293. This Service Bulletin modifies the Ground System Equipment (the AOA Protection Covers) needed for parking, mooring or storing the aircraft.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 1 5

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# @A330 SERVICE BULLETIN SUMMARY Accomplishment of this Service Bulletin cancels OEB 45 and FM TR293. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this cancellation. The operational consequence of this Service Bulletin is the modification of the Flight Manual (FM) and Flight Crew Operating Manual (FCOM) by removing temporary operational measures introduced by OEB 45, FOT No. 999.0089/12 and FM TR293. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED YES RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED 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 Component COMPA01 1 See SB Flat Plates, Covers Component COMPA02 1 See SB Screws Component COMPA03 1 See SB Screws EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

11S 38W 46W 62S AAR AAW ACA ACI AEA AFL AFR ALK ARA ASY AVA AZA BEC BEL BER BMA C9G CAL CCA CES CHH CPA CRK CRL CSC CSN DAH DAL DGA DLH EDW EIN ETD EVA FIN FWI GFA GIA GRL HAL HDA HFY HVN I2L IAC IAW ISS IYE JAI JAV JST KAL KFR KLM MAS MAU MEA MNB MON MSR OBS OHY OMA PAL QAF QFA QTR RJA RSF RSY RYN SAA SAI SAS SIA SVA SWR TAE TAI TAM TAP TCX THA THY TNA TOW TSC UAE UAF USA VIR VKG VOZ XAX XLF YZR CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB 45 AOT None SIL None LINE MAINTENANCE AFFECTED No DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 2 5

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# @A330 SERVICE BULLETIN SUMMARY
LIFE LIMIT None OTHER OIT No. 999.0086/12 OTHER FOT No. 999.0089/12 OTHERS SBIT No. 13-0017 NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 343293-831-801-001: Modification of the AOA sensor plates TOTAL MANHOURS 6.25 ELAPSED TIME (HOURS) 4.25 Task 343293-831-802-001: Additional Work TOTAL MANHOURS 4.25 ELAPSED TIME (HOURS) 4.25 APPENDICES APPENDIX 01: Elapsed Time Assumption

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 3 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF ALL

**NOTE:** TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS. 

## BEFORE FR19 FR18 3FP1 3FP2 3FP3 

### A

**A**



## A 

## OR

**THALES GOODRICH** 



### C

**C A**  **B**

G_SB_343293_5_SAAA_01_02 Figure A-FSAAA - Sheet 01

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 4 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF ALL

TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS. 

## AFTER

**CAUTION:** NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND SHALL REMAIN AS DELIVERED. **NOTE:** DEPENDS ON AIRCRAFT CONFIGURATION. ONLY ONE CONFIGURATION LH SIDE SHOWN, AOA SENSOR 

## B
**FWD**

G_SB_343293_5_SAAA_02_02 Figure A-FSAAA - Sheet 02

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 5 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF ALL

TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS. 

## AFTER

**CAUTION:** NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND SHALL REMAIN AS DELIVERED. 

## C **NOTE:** DEPENDS ON AIRCRAFT CONFIGURATION. ONLY ONE CONFIGURATION RH SIDE SHOWN, AOA SENSOR**FWD**

G_SB_343293_5_SAAA_03_00 Figure A-FSAAA - Sheet 03

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 6 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF ALL



### B FR69 FR73



## A

**B A**  Z160

7500NW

FLIGHT KIT No 2 **NOTE:** ARE STORED IN FLIGHT KIT No 2 FIN (7500NW) AOA PROTECTION COVERS FINs (7955ME, 7956ME AND 7957ME) G_SB_343293_5_SBAA_01_01 Figure A-FSBAA - Sheet 01

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 7 5

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# @A330 SERVICE BULLETIN SUMMARY

This Page Intentionally Left Blank

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# @A330 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 34 

### TITLE: NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY AOA PROBE FLAT PLATE MODIFICATION No.: 203295S32646 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 applicable by Service Bulletin only. NOTE: This Service Bulletin is only applicable to aircraft listed below on which Mod. No. 201609S31691 (INSTALL A NEW CONIC PLATE FOR NEW AOA (ANGLE OF ATTACK SENSOR) THALES) or Mod. No. 201610S31887 (INSTALL A NEW CONIC PLATE FOR AOA (ANGLE OF ATTACK SENSOR) GOODRICH AND OLD AOA THALES) are embodied or on which Service Bulletin No. A330-34-3255 is accomplished. (1) Models 330-202 330-203 330-223 330-223F 330-243 330-243F 330-301 330-302 330-303 330-321 330-322 330-323 330-341 330-342 330-343 (2) Effectivity by MSN 0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0066 0070-0072 0077 0082-0083 0086-0087 0095-0096 0098-0099 0102 0106-0107 0109 0111-0113 0116 0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 1 5

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# @A330 SERVICE BULLETIN

0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782 0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863 0865-0869 0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922-0923 0926-0928 0930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-1004 1006-1016 1018-1023 1025-1026 1028-1029 1031-1039 1041-1049 1051-1055 1057-1063 1065-1067 1069-1078 1080-1082 1084-1090 1092-1101 1103-1108 1110 1112 1114-1116 1118 1120 1123-1124 1126-1127 1129-1133 1135-1138 1141 1143 1145-1151 1153 1155-1157 1159-1161 1163-1165 1167-1175 1177-1178 1180-1181 1183-1184 1186-1193 1195-1196 1198-1206 1208-1241 1243-1252 1254-1256 1258-1272 1274-1349 1352-1360 1362-1365 (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 46W 0871 62S 1321 AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340 AAW 0999 1043 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0505 0526 0551 0597 0670 0733 0745 0749 0814 0931 0950 1097 AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247 1264 1270 1284 1299 1301 1323 1328 1345 1356 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 ALK 0303 0306 0311 0313 0404 0456 0627 ARA 0891 0927
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 2 5

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# @A330 SERVICE BULLETIN

OPERATOR MSN ASY 0747 0951 0969 1036 1183 AVA 0948 0967 1009 1016 1073 1208 1224 1342 AZA 0272 0339 1123 1135 1218 1225 1252 1283 1308 1313 1327 1354 BEC 0863 BEL 0030 0037 0045 0082 0095 0229 0249 0324 BER 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 0739 0822 0828 0911 BMA 0398 C9G 0461 CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769 0805 0823 0838 0861 0920 1177 1272 1278 1346 CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873 0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187 1199 1216 1237 1260 1282 1304 1330 1333 1353 CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830 0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291 1303 1324 1331 CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255 1325 CPA 0102 0113 0118 0121 0155 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 0776 0850 0855 0895 0915 0959 1163 1196 1222 1239 1285 1317 1343 1349 1362 CRK 1031 1034 1039 1042 1051 1054 1059 1062 1115 1277 1286 1320 1322 1358 CRL 0285 0320 1359 CSC 0462 1082 1138 1241 CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954 0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 1335 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 1292 1305 1314 EDW 0291 1193 EIN 0269 0397 0841 0847 0985 1025 1106 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 EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 1254 1268 1274 FIN 0994 1007 1013 1023 1067 1078 1088 1173 FWI 0253 0758 0965 1021 1265 GFA 0276 0281 0286 0287 0334 0340 0532 0992 GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052 1184 1214 1261 1288 1364 GRL 0230 HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 3 5

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# @A330 SERVICE BULLETIN

OPERATOR MSN HDA 0012 0017 0071 0083 0099 0106 0109 0234 0244 0405 0479 0512 0581 0654 0662 0692 0716 0741 0786 HFY 0096 0127 0211 0262 1008 HVN 0275 0294 0299 0366 0943 0962 1019 1256 1266 I2L 0205 0330 0358 0364 0527 0529 IAC 0353 0362 IAW 1339 ISS 0802 IYE 0625 0632 JAI 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956 JAV 0255 JST 0506 0508 0513 0522 0842 0853 0940 0945 1198 1251 1258 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0425 0428 0484 0490 0550 1133 1155 1200 1203 KFR 0874 0939 0946 KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 1161 1287 1294 1300 MAS 0077 0107 0116 0119 0290 0296 0300 1136 1148 1164 1180 1209 1219 1229 1234 1243 1281 1318 1336 1337 1347 MAU 0883 1057 MEA 0926 0984 0995 0998 MNB 1332 MON 0261 0265 MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246 OBS 0833 OHY 0072 0087 0098 0143 OMA 1038 1044 1049 1063 1093 1120 1227 PAL 0183 0184 0188 0189 0191 0198 0200 0203 QAF 0487 0605 QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887 0892 0898 0976 1061 1094 1169 1174 1365 QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659 0680 0684 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820 0826 0849 0893 0907 0918 RJA 0970 0979 1002 RSF 0980 0996 1235 RSY 0120 0171 RYN 0343 SAA 1191 1210 1223 1236 1249 1271 SAI 0055 0070 0086 SAS 0496 0497 0515 0568 SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099 1105 1107 1124 1132 1146 1149 1156 1157 SVA 1108 1127 1137 1141 1147 1153 1189 1192 SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290 1355 TAE 0348 DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 4 5

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# @A330 SERVICE BULLETIN

OPERATOR MSN TAI 1279 TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0869 0876 0949 0961 0968 0977 1112 1118 1213 1221 TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934 TCX 0254 0266 0301 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 0990 1003 1035 1037 1060 1074 1086 1090 1263 1269 1289 1338 1348 THY 0463 0504 0697 0704 0742 0754 0774 1004 1092 1150 1160 1170 1172 1204 1212 1228 1240 1298 1307 1311 1344 TNA 1357 TOW 1033 1046 1248 1275 1312 1334 1363 TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 0795 0966 0971 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0382 0384 0392 0396 0409 0437 0451 0452 0455 0491 0494 0509 0518 0525 0536 UAF 1080 1186 1250 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041 1069 1076 1095 1100 VIR 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352 VKG 0309 0349 0356 0357 VOZ 0365 0372 1293 1306 1319 XAX 0054 0952 0974 1048 1066 1075 1126 1131 1165 XLF 0501 0635 1360 YZR 1175

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 5 5

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# @A330 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064 0065 0066 0070 0071 0072 0077 0082 0083 0086 0087 0095 0096 0098 0099 0102 0106 0107 0109 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177 0181 0183 0184 0188 0189 0191 0195 0198 0200 0203 0205 0206 0209 0211 0219 0222 0223 0224 0226 0229 0230 0231 0232 0234 0238 0240 0241 0244 0247 0248 0249 0250 0251 0253 0254 0255 0256 0258 0259 0261 0262 0265 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281 0283 0284 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328 0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345 0346 0348 0349 0350 0351 0353 0356 0357 0358 0361 0362 0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403 0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422 0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487 0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513 0515 0516 0518 0519 0521 0522 0524 0525 0526 0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549 0550 0551 0552 0553 0555 0558 0564 0565 0567 0568 0570 0571 0573 0574 0576 0578 0579 0581 0584 0587 0588 0591 0593 0595 0597 0600 0602 0603 0605 0607 0609 0610 0612 0614 0616 0618 0620 0621 0623 0625 0627 0629 0631 0632 0633 0634 0635 0636 0637 0638 0640 0641 0642 0644 0645 0647 0648 0649 0650 0652 0653 0654 0655 0656 0657 0658 0659 0661 0662 0663 0664 0665 0666 0667 0669 0670 0671 0673 0674 0675 0676 0678 0679 0680 0682 0683 0684 0686 0687 0688 0690 0691 0692 0693 0695 0696 0697 0699 0700 0701 0703 0704 0705 0707 0708 0709 0711 0712 0713 0714 0716 0717 0718 0720 0721 0722 0724 0725 0726 0728 0729 0730 0732 0733 0734 0735 0737 0738 0739 0741 0742 0743 0745 0746 0747 0749 0750 0751 0752 0754 0755 0756 0758 0759 0760 0769 0770 0772 0773 0774 0776 0777 0778 0780 0781 0782 0784 0785 0786 0788 0789 0791 0792 0795 0796 0797 0799 0801 0802 0803 0805 0806 0807 0809 0810 0811 0813 0814 0815 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0830 0831 0832 0833 0834 0836 0838 0839 0840 0841 0842 0843 0845 0847 0849 0850 0851 0852 0853 0854 0855 0857 0858 0859 0860 0861 0862 0863 0865 0866 0867 0868 0869 0871 0873 0874 0875 0876 0877 0879 0881 0882 0883 0884 0885 0887 0888 0889 0890 0891 0892 0893 0895 0896 0898 0899 0900 0901 0903 0904 0905 0906 0907 0908 0909 0911 0913 0914 0915 0916 0918 0919 0920 0922 0923 0926 0927 0928 0930 0931 0932 001

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 6 5

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# @A330 SERVICE BULLETIN

MSN CONFIGURATION 0934 0935 0936 0937 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948 0949 0950 0951 0952 0954 0956 0957 0958 0959 0961 0962 0963 0964 0965 0966 0967 0968 0969 0970 0971 0973 0974 0975 0976 0977 0978 0979 0980 0982 0983 0984 0985 0986 0988 0989 0990 0991 0992 0994 0995 0996 0997 0998 0999 1000 1001 1002 1003 1004 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016 1018 1019 1020 1021 1022 1023 1025 1026 1028 1029 1031 1032 1033 1034 1035 1036 1037 1038 1039 1041 1042 1043 1044 1045 1046 1047 1048 1049 1051 1052 1053 1054 1055 1057 1058 1059 1060 1061 1062 1063 1065 1066 1067 1069 1070 1071 1072 1073 1074 1075 1076 1077 1078 1080 1081 1082 1084 1085 1086 1087 1088 1089 1090 1092 1093 1094 1095 1096 1097 1098 1099 1100 1101 1103 1104 1105 1106 1107 1108 1110 1112 1114 1115 1116 1118 1120 1123 1124 1126 1127 1129 1130 1131 1132 1133 1135 1136 1137 1138 1141 1143 1145 1146 1147 1148 1149 1150 1151 1153 1155 1156 1157 1159 1160 1161 1163 1164 1165 1167 1168 1169 1170 1171 1172 1173 1174 1175 1177 1178 1180 1181 1183 1184 1186 1187 1188 1189 1190 1191 1192 1193 1195 1196 1198 1199 1200 1201 1202 1203 1204 1205 1206 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217 1218 1219 1220 1221 1222 1223 1224 1225 1226 1227 1228 1229 1230 1231 1232 1233 1234 1235 1236 1237 1238 1239 1240 1241 1243 1244 1245 1246 1247 1248 1249 1250 1251 1252 1254 1255 1256 1258 1259 1260 1261 1262 1263 1264 1265 1266 1267 1268 1269 1270 1271 1272 1274 1275 1276 1277 1278 1279 1280 1281 1282 1283 1284 1285 1286 1287 1288 1289 1290 1291 1292 1293 1294 1295 1296 1297 1298 1299 1300 1301 1302 1303 1304 1305 1306 1307 1308 1309 1310 1311 1312 1313 1314 1315 1316 1317 1318 1319 1320 1321 1322 1323 1324 1325 1326 1327 1328 1329 1330 1331 1332 1333 1334 1335 1336 1337 1338 1339 1340 1341 1342 1343 1344 1345 1346 1347 1348 1349 1352 1353 1354 1355 1356 1357 1358 1359 1360 1362 1363 1364 1365 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. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Consumable CMLA01 1 Component COMPA01 1 Component COMPA02 1 Component COMPA03 1

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 7 5

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# @A330 SERVICE BULLETIN
B. CONCURRENT REQUIREMENTS None C. REASON (1) History Following a recent in-service event, as a precautionary measure, Airbus requires to suspend the installation of the AOA (Angle Of Attack) conic plates as per Operator Information Transmission (OIT) No. 999.0086/12, currently performed through an Airbus monitored campaign with Service Bulletin No. A330-34-3255. (2) Objective/Action This modification requires the removal of the conic plates PN F3411060200000 and PN F3411060900000, and the installation of flat plates PN F3411007920200 (LH) / PN F3411007920300 (RH). Also, it requires to change the 3 AOA Sensor Protection Covers (FINs 7955ME, 7956ME and 7957ME) stored in Flight Kit No 2 (FIN 7500NW). (3) Advantages Refer to OIT No. 999.0086/12 and FOT No. 999.0089/12 for further explanations. (4) Operational/Maintenance Consequences For aircraft already fitted with the AOA conic plates through retrofit or from production, Airbus released associated operational recommendations in an FOT No. 999.0089/12, the Operations Engineering Bulletin (OEB) 45 and Flight Manual (FM) Temporary Revision 293. This Service Bulletin modifies the Ground System Equipment (the AOA Protection Covers) needed for parking, mooring or storing the aircraft. Accomplishment of this Service Bulletin cancels OEB 45 and FM TR293. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this cancellation. The operational consequence of this Service Bulletin is the modification of the Flight Manual (FM) and Flight Crew Operating Manual (FCOM) by removing temporary operational measures introduced by OEB 45, FOT No. 999.0089/12 and FM TR293. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 343293-831-801-001: Modification of the AOA sensor plates (1) Replace the Conic Plate of the AOA Sensor FIN 3FP1, on the LH Side (2) Replace the Conic Plates of the AOA Sensors FINs 3FP2 and 3FP3, on the RH side
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 8 5

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# @A330 SERVICE BULLETIN (3) Replace the AOA protection Covers in the Flight Kit No 2 (FIN 7500NW) Task 343293-831-802-001: Additional Work (1) Modify the flat Plates position at level of the AOA Sensors FINs 3FP2 and 3FP3, on the RH side. 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. Table 1: Modification of the AOA sensor plates Compliance Time Condition Action Threshold Grace Period Config. 001 First application 5 months after AD effective date None
Table 2: Additional Work Compliance Time Condition Action Threshold Grace Period For aircraft on which this SB at its initial issue is accomplished Accomplishment of Additional Work At next C-check at the latest None

F. APPROVAL The technical content of this document is approved under the authority of 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. 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.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 9 5

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# @A330 SERVICE BULLETIN
Task 343293-831-801-001: Modification of the AOA sensor plates Get Access 0.50 On Aircraft Replace the Conic Plate of the AOA Sensor FIN 3FP1, on the LH Side 1.50 Replace the Conic Plates of the AOA Sensors FINs 3FP2 and 3FP3, on the RH side 3.00 Replace the AOA protection Covers in the Flight Kit No 2 (FIN 7500NW) 0.50 Tests 0.25 Close-Up 0.50 TOTAL MANHOURS 6.25 ELAPSED TIME (HOURS) 4.25 NOTE: For detail concerning the elapsed time assumption, refer to APPENDIX 01: Elapsed Time Assumption . Task 343293-831-802-001: Additional Work Get Access 0.50 On Aircraft Modify the flat Plates position at level of the AOA Sensors FINs 3FP2 and 3FP3, on the RH side. 3.00 Tests 0.25 Close-Up 0.50 TOTAL MANHOURS 4.25 ELAPSED TIME (HOURS) 4.25 H. WEIGHT AND BALANCE The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight -0.549 KG (-1.2103 LB) Effect on Balance -7.502 KGM (-54.262 LB.FT ) I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-21-11 20-28-00 52-30-00 52-41-00 Consumable Material List (CML) ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-51-20 20-55-00 Flight Crew Operating Manual (FCOM)
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 10 5

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# @A330 SERVICE BULLETIN
Flight Manual (FM) Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-42-00 51-43-00 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 10-11-00 12-21-11 34-11-19 Aircraft Wiring List (AWL) Flight Crew Operating Manual (FCOM) Flight Manual (FM) Illustrated Parts Catalog (IPC) 25-73-04 34-11-01 Tool Equipment Manual (TEM) 10-11-00 This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in advance, in case you need your operational documentation to be amended by a revision priorto Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to: SEDOR4, AIRBUS Customer Services Technical Data Fax No.: (33) 5 61 93 28 06 E-mail: sb.reporting@airbus.com SB Reporting service is accessible on-line through AIRBUSWorld from: - ’My on-line services’ section, available on all AIRBUSWorld pages - The Maintenance & Engineering Community, in: . Modify and Upgrade page - Access SB and VSB section. These amendments will be confirmed by the next normal revision of operational documentation, once your Service Bulletin accomplishment report has been sent, as usual, to our Customer Services Aircraft In-Service Data (SEDOR4). L. INTERCHANGEABILITY/MIXABILITY DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Plate F3411060200000 F3411007920200 01 NO Plate F3411060900000 F3411007920200 01 NO Plate F3411060200000 F3411007920300 01 NO Plate F3411060900000 F3411007920300 01 NO AOA Sensor Protection 98D34203003000 98F10001000000 01 NO
NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 11 5

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# @A330 SERVICE BULLETIN
NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. M. SPARES AOA Sensor Protection 98D34203003000 Plate F3411060200000 Plate F3411060900000

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 12 5

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# @A330 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign. Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: Component COMPA01 AIRBUS Material, Logistics and Suppliers IFD - In Flight Desk Weg beim Jaeger 150 D-22335 HAMBOURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 4012 For ordering by E-mail: ifd.spares@airbus.com Airbus Material, Logistics and Suppliers do not stock standard hardware as competitive multiple suppliers ensure access to minimum prices Airbus recommends Customers with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to B/E Aerospace. The address is: Component COMPA02 Component COMPA03 B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15TH Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com internet: www.beconsumables.com or, alternatively any other source on the open market. (2) Price and Availability

Component COMPA01 No AIRBUS kit will be provided.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 13 5

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# @A330 SERVICE BULLETIN Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be purchased by a spares purchase order. Component COMPA02 No AIRBUS kit will be provided. Operator supplied standard hardware parts required to accomplish this Service Bulletin are to be supplied from the Operator’s stock. Component COMPA03 No AIRBUS kit will be provided. Operator supplied standard hardware parts required to accomplish this Service Bulletin are to be supplied from the Operator’s stock. B. INDUSTRY SUPPORT INFORMATION AIRBUS will provide the AIRBUS parts (COMPA01) at no charge for orders placed before Jun 30/13. For the accomplishment of this Service Bulletin before Jun 30/13, AIRBUS will credit the manhours indicated in this Service Bulletin at the agreed in-house warranty labor rate for claims received not later than 90 days after completion of the last affected aircraft of your fleet. For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department. AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX France E-mail: monitored.retrofit@airbus.com Tel : (33) 5 67 19 06 22 Fax : (33) 5 61 93 27 45 C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Polysulfide Sealant-General Purpose Fillet 06AAB1 As required

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 14 5

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# @A330 SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Polysulfide Sealant-Fuel Tank Quick Curing 06ABF1 As required Non Aqueous Cleaner-General 08BAA9 As required Release Agent-Liquid Wax 14DBB1 As required (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 2 F3411007920200 1 PLATE (2) F3411060200000 01 (2) F3411060900000 01 2 F3411007920300 2 PLATE (2) F3411060200000 01 (2) F3411060900000 01 98F10001000000 3 AOAPRTCT 98D34203003000 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 NAS1102-3-14 21 SCREW 3 NAS1102-3-12 2 SCREW NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES NAS1102-3-12 2 SCREW NAS1102-3-14 14 SCREW NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 15 5

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# @A330 SERVICE BULLETIN (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 16 5

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# @A330 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 343293-831-801-001 - Modification of the AOA sensor plates 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 Zone 121 122 160 Modified FIN 7955ME 7956ME 7957ME 7500NW Access Door 823 Other access Access platformManpower TOTAL MANHOURS 6.25 ELAPSED TIME (HOURS) 4.25 A. GENERAL (1) Subtask 343293-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 Task 20-21-11-911-801 Task 20-28-00-912-804 Task 20-28-00-912-805
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# @A330 SERVICE BULLETIN

References Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-24-00 51-42-00 51-43-00 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer to Consumable Material List (CML). (b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (c) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (d) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (e) Remove and install of fasteners in accordance with SRM 51-42-00. (f) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00. (g) If the length of any fastener specified in this Service Bulletin does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. (h) Do the electrical bonding, refer to ESPM 20-51-20 and AMM Task 20-28-00-912-804 or AMM Task 20-28-00-912-805. (i) Apply sealant in accordance with SRM 51-24-00. (2) Subtask 343293-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 343293-941-001-001 - 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 52-30-00-010-803 52-41-00, Page Block 001
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 18 5

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# @A330 SERVICE BULLETIN (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Put the access platforms in position at the Bulk cargo-compartment door 823 and at avionics compartment door 811 and at zone 121 to get access to the AOA sensor FIN 3FP1 and at zone 122 to get access to the AOA sensors FINs 3FP2 and 3FP3. (c) Open the Bulk cargo-compartment door 823, refer to AMM Task 52-30-00-010-803. (d) Open the avionics compartment door 811, refer to AMM 52-41-00, Page Block 001 and refer to AMM 06-41-53, Page Block 001. (e) Safety precaution 1 On the panel 225VU:
a Make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is OFF). C. PROCEDURE (1) Subtask 343293-831-001-001 - Replace the Conic Plate of the AOA Sensor FIN 3FP1, on the LH Side Work Zones and Access Panels Zone Access/Work location 121 Access Other access Access platform Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills NON SPECIFIC Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 F3411007920200 1 PLATE NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NAS1102-3-14 7 SCREW NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel.
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 19 5

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# @A330 SERVICE BULLETIN

Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTESNon Aqueous CleanerGeneral 08BAA9 As required
References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAA Modification of the LH side Plate Sheet 01 Sheet 02 NOTE: The screw item (3) must not be removed to keep the AOA sensor in position and to avoid removing it. (a) Replace the conic plate by the flat plate of the AOA sensor FIN 3FP1, on the LH side: NOTE: Make sure that the previous plate installed on the aircraft is a conic plate. Refer to aircraft maintenance records. In accordance with SRM 51-42-00 and SRM 51-43-00 Refer to AMM Task 20-21-11-911-801 1 Use a non-metallic spatula to remove the sealant and clean the areas with: Non Aqueous Cleaner-General 08BAA9 As required

2 Remove the conic plate: Refer to Fig. A-FBAAA Sheet 01 1 Plate F3411060200000 Item (2) Discard
or 1 Plate F3411060900000 Item (2) Discard attached with: 7 Screw Item (1) Discard 3 Use a non-metallic spatula to remove the sealant and clean the areas with: Non Aqueous Cleaner-General 08BAA9 As required

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# @A330 SERVICE BULLETIN

4 Install the flat plate: CAUTION: NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND SHALL REMAIN AS DELIVERED NOTE: The attaching holes of the flat plates are delivered stripped from protection at level of the surface of the bonding areas. Refer to Fig. A-FBAAA Sheet 02 1 Plate F3411007920200 Item 2 attached with: 7 Screw NAS1102-3-14 Item 1

(2) Subtask 343293-831-002-001 - Replace the Conic Plates of the AOA Sensors FINs 3FP2 and 3FP3, on the RH side Work Zones and Access Panels Zone Access/Work location 122 Access Other access Access platform 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 2 F3411007920300 2 PLATE NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NAS1102-3-14 14 SCREW 3 NAS1102-3-12 2 SCREW NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 21 5

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# @A330 SERVICE BULLETIN

Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTESNon Aqueous CleanerGeneral 08BAA9 As required
References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBCAA Modification of the RH side Plate Sheet 01 Sheet 02 NOTE: The aim of this procedure is to keep the AOA sensors in position and to avoid removing them. (a) Replace the conic plates by the flat plates of the AOA sensors FINs 3FP2 and 3FP3, on the RH side: NOTE: Make sure that the previous plate installed on the aircraft is a conic plate. Refer to aircraft maintenance records. In accordance with SRM 51-42-00 and SRM 51-43-00 Refer to AMM Task 20-21-11-911-801 1 Use a non-metallic spatula to remove the sealant and clean the areas with: Non Aqueous Cleaner-General 08BAA9 As required
2 Remove the conic plates: Refer to Fig. A-FBCAA Sheet 01

. 2 Plate F3411060200000 Item (2) Discard
or 2 Plate F3411060900000 Item (2) Discard attached with: 14 Screw Item (1) Discard 3 Install the new screw item 3 in the position shown on Fig. A-FBCAA Sheet 02: 2 Screw NAS1102-3-12 Item 3 4 Remove and discard the old screw item (3) that held the AOA sensor in position shown on Fig. A-FBCAA Sheet 01

.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 22 5

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# @A330 SERVICE BULLETIN

5 Use a non-metallic spatula to remove the sealant and clean the areas with: Non Aqueous Cleaner-General 08BAA9 As required
6 Install the flat plates: CAUTION: NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND SHALL REMAIN AS DELIVERED NOTE: The attaching holes of the flat plates are delivered stripped from protection at level of the surface of the bonding areas. Refer to Fig. A-FBCAA Sheet 02

. 2 Plate F3411007920300 Item 2 attached with: 14 Screw NAS1102-3-14 Item 1

(3) Subtask 343293-831-003-001 - Replace the AOA protection Covers in the Flight Kit No 2 (FIN 7500NW) Work Zones and Access Panels Zone Access/Work location 160 Access Door 823 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills NON SPECIFIC Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 98F10001000000 3 AOAPRTCT NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. References Fig. A-FBBAA Modification of AOA Protection Covers in the Flight Kit No 2 Sheet 01

NOTE: Depending on airline internal policy the Flight Kit No 2 may not be located in the place defined by Fig. A-FBBAA Sheet 01. Refer to airline internal policy for exact location for Flight Kit No 2, and/or its contents. DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 23 5

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# @A330 SERVICE BULLETIN (a) Remove in the Flight Kit No 2 (FIN 7500NW): Refer to Fig. A-FBBAA Sheet 01: FIN 7955ME 1 AOA Sensor Protection 98D34203003000 Discard FIN 7956ME 1 AOA Sensor Protection 98D34203003000 Discard FIN 7957ME 1 AOA Sensor Protection 98D34203003000 Discard (b) Install in the Flight Kit No 2 (FIN 7500NW): Refer to Fig. A-FBBAA Sheet 01: FIN 7955ME 1 AOA Sensor Protection 98F10001000000 FIN 7956ME 1 AOA Sensor Protection 98F10001000000 FIN 7957ME 1 AOA Sensor Protection 98F10001000000 D. TEST (1) Subtask 343293-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805 Task 20-28-00-869-801 (a) Test of electrical bonding at level of the screw item 3: 1 Make sure that the bonding contact resistance between the sensor (via screw item 3) and the fuselage structure is not higher than 5 milliohms, refer to AMM Task 20-28-00-720-805. E. CLOSE-UP (1) Subtask 343293-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 24 5

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# @A330 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Polysulfide Sealant-General Purpose Fillet 06AAB1 As required Polysulfide Sealant-Fuel Tank Quick Curing 06ABF1 As required Release Agent-Liquid Wax 14DBB1 References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 20-28-00-912-802 Task 20-28-00-912-804 Task 52-30-00-410-803 52-41-00, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-24-00 Fig. A-FBAAA Modification of the LH side Plate Sheet 01 Sheet 02 Fig. A-FBCAA Modification of the RH side Plate Sheet 01 Sheet 02 (a) Protect the screws item 1 and item 3 in accordance with ESPM 20-51-20 and AMM Task 20-28-00-912-802 and/or AMM Task 20-28-00-912-804. (b) Blank off the hole located in front of the screw item (3) in accordance with SRM 51-24-00 as shown on Fig. A-FBAAA Sheet 02 and on Fig. A-FBCAA Sheet 02 with:Release AgentLiquid Wax 14DBB1 As required
andPolysulfide SealantGeneral Purpose Fillet 06AAB1 As required

orPolysulfide SealantFuel Tank Quick Curing 06ABF1 As required
(c) Make sure that the work areas are clean and clear of tools and other items of equipment. (d) Close the Bulk cargo-compartment door 823, refer to AMM Task 52-30-00-410-803.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 25 5

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# @A330 SERVICE BULLETIN (e) Close the avionics compartment door 811, refer to AMM 06-41-53, Page Block 001 and refer AMM 52-41-00, Page Block 001. (f) Remove the access platform(s). (g) Restore the systems and the aircraft to normal operating condition.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 26 5

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# @A330 SERVICE BULLETIN
Task 343293-831-802-001 - Additional Work 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 Zone 122 Access Other access Access PlatformManpower TOTAL MANHOURS 4.25 ELAPSED TIME (HOURS) 4.25 A. GENERAL (1) Subtask 343293-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 Task 20-21-11-911-801 Task 20-28-00-912-804 Task 20-28-00-912-805 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-24-00 51-42-00 51-43-00
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 27 5

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# @A330 SERVICE BULLETIN (a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer to Consumable Material List (CML). (b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (c) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (d) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (e) Remove and install of fasteners in accordance with SRM 51-42-00. (f) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00. (g) If the length of any fastener specified in this Service Bulletin does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. (h) Do the electrical bonding, refer to ESPM 20-51-20 and AMM Task 20-28-00-912-804 or AMM Task 20-28-00-912-805. (i) Apply sealant in accordance with SRM 51-24-00. (2) Subtask 343293-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 343293-941-002-001 - 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 52-41-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Put the access platforms in position at the avionics compartment door 811 and at zone 122 to get access to the AOA sensors (FINs 3FP2 and 3FP3). (c) Open the avionics compartment door 811, refer to AMM 06-41-53, Page Block 001 and AMM 52-41-00, Page Block 001. DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 28 5

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# @A330 SERVICE BULLETIN (d) Safety precaution 1 On the panel 225VU:
a Make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is OFF). C. PROCEDURE (1) Subtask 343293-831-004-001 - Modify the flat Plates position at level of the AOA Sensors FINs 3FP2 and 3FP3, on the RH side. Work Zones and Access Panels Zone Access/Work location 122 Access Other access Access Platform 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 COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES NAS1102-3-12 2 SCREW NAS1102-3-14 14 SCREW Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTESNon Aqueous CleanerGeneral 08BAA9 As required
References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBDAA Modification of the RH side Plate position (Additional Work) Sheet 01 Sheet 02 (a) If screw item (3) is located as shown on Fig. A-FBDAA Sheet 02: 1 No further action is required.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 29 5

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# @A330 SERVICE BULLETIN (b) If screw item (3) is NOT located as shown on Fig. A-FBDAA Sheet 02: NOTE: The aim of this procedure is to change the position of the screw item 3 keeping AOA sensor in the same position. In accordance with SRM 51-42-00 and SRM 51-43-00 Refer to AMM Task 20-21-11-911-801 1 Use a non-metallic spatula to remove the sealant and clean the areas with: Non Aqueous Cleaner-General 08BAA9 As required

2 Remove the flat plates: 2 Plate F3411007920300 Item (2) Retain attached with: 14 Screw Item (1) Discard 3 Install the new screw item 3 in the position shown on Fig. A-FBDAA Sheet 02: 2 Screw NAS1102-3-12 4 Remove and discard the old screw item (3) that held the AOA sensor in position shown on Fig. A-FBDAA Sheet 01

. 5 Re-install the flat plates item (2) retained at removal: CAUTION: NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND SHALL REMAIN AS DELIVERED Refer to Fig. A-FBDAA Sheet 02: 2 Plate F3411007920300 Item (2) Retained at removal attached with: 14 Screw NAS1102-3-14 D. TEST (1) Subtask 343293-700-002-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805 Task 20-28-00-869-801

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 30 5

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# @A330 SERVICE BULLETIN (a) Test of electrical bonding at level of the screw item 3: 1 Make sure that the bonding contact resistance between the sensor (via screw item 3) and the fuselage structure is not higher than 5 milliohms, refer to AMM Task 20-28-00-720-805. E. CLOSE-UP (1) Subtask 343293-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Polysulfide Sealant-General Purpose Fillet 06AAB1 As required Polysulfide Sealant-Fuel Tank Quick Curing 06ABF1 As required Release Agent-Liquid Wax 14DBB1 As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 20-28-00-912-802 Task 20-28-00-912-804 52-41-00, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-24-00 Fig. A-FBDAA Modification of the RH side Plate position (Additional Work) Sheet 01 Sheet 02 (a) Protect the screws item 1 and item 3 in accordance with ESPM 20-51-20 and AMM Task 20-28-00-912-802 and/or AMM Task 20-28-00-912-804. (b) Blank off the hole located in front of the screw item (3) in accordance with SRM 51-24-00 as shown on Fig. A-FBDAA Sheet 02with:Release AgentLiquid Wax 14DBB1 As required
andPolysulfide SealantGeneral Purpose Fillet 06AAB1 As required

or DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 31 5

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# @A330 SERVICE BULLETIN
Polysulfide SealantFuel Tank Quick Curing 06ABF1 As required
(c) Make sure that the work areas are clean and clear of tools and other items of equipment. (d) Close the avionics compartment door 811, refer to AMM 06-41-53, Page Block 001 and AMM 52-41-00, Page Block 001. (e) Remove the access platform(s). (f) Restore the systems and the aircraft to normal operating condition.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 32 5

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# @A330 SERVICE BULLETIN

**CONF ALL



## BEFORE FR19 FR18 3FP1



## A (1) (7 POS) (1) (7 POS)


## OR

(2) (2) (3) (3)

**NOTE:** TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS. **THALES GOODRICH**  

### A **B**

G_SB_343293_5_BAAA_01_02 Figure A-FBAAA - Sheet 01 Modification of the LH side Plate
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 33 5

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# @A330 SERVICE BULLETIN

**CONF ALL



## AFTER

1 2 (7 POS) (3)

**NOTE:** ONLY ONE CONFIGURATION SHOWN, AOA SENSOR
01 BLANK OFF THE HOLE LOCATED IN FRONT OF THE SCREW ITEM WITH: MAT. No 14DBB1 AND MAT. No 06ABF1 OR 06AAB1. (3) DEPENDS ON AIRCRAFT CONFIGURATION. 01



## B

ELECTRICAL BONDING
G_SB_343293_5_BAAA_02_04 Figure A-FBAAA - Sheet 02 Modification of the LH side Plate
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 34 5

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# @A330 SERVICE BULLETIN

**CONF ALL



## BEFORE FR19 FR18 3FP2 3FP3 

### A **B**

**A B** 



## A 

## OR

**NOTE:** TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS. **THALES GOODRICH**  (1)(7 POS)

(2) (3)

(1)(7 POS)

(2) (3)

G_SB_343293_5_BCAA_01_00 Figure A-FBCAA - Sheet 01 Modification of the RH side Plate
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 35 5

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# @A330 SERVICE BULLETIN

**CONF ALL



## AFTER

**NOTE:** ONLY ONE CONFIGURATION SHOWN, AOA SENSOR
01 BLANK OFF THE HOLE LOCATED IN FRONT OF THE SCREW ITEM WITH: MAT. No 14DBB1 AND MAT. No 06ABF1 OR 06AAB1. 3 DEPENDS ON AIRCRAFT CONFIGURATION. 

## B

ELECTRICAL BONDING 1 2 (7 POS) 3 01

G_SB_343293_5_BCAA_02_00 Figure A-FBCAA - Sheet 02 Modification of the RH side Plate
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 36 5

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# @A330 SERVICE BULLETIN

**CONF ALL



### B FR69 FR73



## A

**B A**  Z160

7500NW

FLIGHT KIT No 2 **NOTE:** ARE STORED IN FLIGHT KIT No 2 FIN (7500NW) AOA PROTECTION COVERS FINs (7955ME, 7956ME AND 7957ME) G_SB_343293_5_BBAA_01_02 Figure A-FBBAA - Sheet 01 Modification of AOA Protection Covers in the Flight Kit No 2
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 37 5

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# @A330 SERVICE BULLETIN

**CONF ALL



## BEFORE FR19 FR18 3FP2 3FP3 

### A **B**

**A B** 



## A (1) (2) (7 POS) (3) 01

**NOTE:** TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS. G_SB_343293_5_BDAA_01_00 Figure A-FBDAA - Sheet 01 Modification of the RH side Plate position (Additional Work)
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 38 5

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# @A330 SERVICE BULLETIN

**CONF ALL



## AFTER

**NOTE:** ONLY ONE CONFIGURATION SHOWN, AOA SENSOR
01 BLANK OFF THE HOLE LOCATED IN FRONT OF THE SCREW ITEM WITH: MAT. No 14DBB1 AND MAT. No 06ABF1 OR 06AAB1. 3 DEPENDS ON AIRCRAFT CONFIGURATION. 

## B

ELECTRICAL BONDING 1 2 (7 POS) 3 01

G_SB_343293_5_BDAA_02_00 Figure A-FBDAA - Sheet 02 Modification of the RH side Plate position (Additional Work)
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 39 5

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# @A330 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 40 5

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# @A330 SERVICE BULLETIN APPENDIX 01: Elapsed Time Assumption **CONF ALL (1) The following Gantt chart is only a proposal operators may determine that another way to do the work is more suitable for them.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 1 5

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# @A330 SERVICE BULLETIN APPENDIX 01: Elapsed Time Assumption

**CONF ALL

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A330−34−3293**

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 6.25 4.25 STEPS

0.50 0.50

5 0 1.50 1.50

3.00 3.00

TEST 0.25 0.25

CLOSE−UP 0.50 0.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01
02 **NOTE:** PER

1

1

1

1

1 REPLACEMENT OF AOA PROTECTION 0.50 0.50 1

: : SB ELAPSED TIME (HOURS) 1 2 3 4

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. COVERS IN THE FLIGHT KIT No 2 REPLACEMENT OF THE PLATE OF THE AOA SENSOR FIN 3FP1, RH SIDE
REPLACEMENT OF THE PLATE OF THE AOA SENSOR FINs 3FP2 AND 3FP3, LH SIDE

G_SB_343293_5_AAAA_01_01 Figure A-FAAAA - Sheet 01 Gantt Chart
DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 2 5

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY AOA PROBE FLAT PLATE MODIFICATION No.: 203295S32646 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 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 1 5

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# @A330 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

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

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293 REVISION No.: 01 - Jun 12/13 Page: 1 5

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