@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - 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

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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

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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

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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

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - 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

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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

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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

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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

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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

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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

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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

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293

REVISION No.: 01 - Jun 12/13 Page: 8

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - 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

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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

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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

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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

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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

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(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

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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

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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

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(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

Condition Action Compliance Time

Threshold Grace Period

Config. 001 First application 5 months after AD

effective date

None

Table 2: Additional Work

Condition Action Compliance Time

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.

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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)

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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 prior

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

SEDOR4, AIRBUS

Customer Services Technical Data

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

E-mail: sb.reporting@airbus.com

SB Reporting service is accessible on-line through 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.

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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

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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.

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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

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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.

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(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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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 platform

Manpower

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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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

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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

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SERVICE BULLETIN

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 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

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293

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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

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SERVICE BULLETIN

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 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

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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

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(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

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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

and

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

or

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 Bulk cargo-compartment door 823, refer to AMM Task 52-30-00-410-803.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293

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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

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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 Platform

Manpower

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

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(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

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(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

NOTES

Non Aqueous CleanerGeneral08BAA9 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.

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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

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(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 02 with:

Release AgentLiquid Wax14DBB1 As required

and

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

or

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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

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SERVICE BULLETIN

**CONF ALL

BEFORE

FR19

FR18

3FP1

A

(7 POS) (1) (7 POS) (1)

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

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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

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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

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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

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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

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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

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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

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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

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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

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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

0 5

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

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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

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jan 31/13 SERVICE BULLETIN No.: A330-34-3293

REVISION No.: 01 - Jun 12/13 Page: 1

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