@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - AOA - INSTALL AOA PROBES IN MIXED

CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND

UTAS ON STANDBY

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 204937S33428

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The aim of this modification is to allow the airlines to fly in a mixed Angle of Attack (AOA) configuration.

This Service Bulletin requires the replacement of two UTAS AoA probes (FINs 3FP1 and 3FP2) PN

0861ED (installed by Mod. No. 46921S14694 or Service Bulletin No. A330-34-3087) or PN 0861ED2

(installed by Mod. No. 204294S33100 or Service Bulletin No. A330-34-3311) by two THALES AoA

probes PN C16291AB.

The accomplishment of this Service Bulletin will allow the airlines to fly in mixed AoA configurations.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

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SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB AOA Probes

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA02 1 See SB AOA Probes

EFFECTIVITY

**CONF ALL

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

AFL AIB ARG ASY AVA AZU BER CAL CCA CEB CES CHH CPA

CRK CSC CSN DLH EIN ETD EVA FIN FJI GAP GIA HDA HVN

JAI JST LAA MAS MEA MNB OBS OHY OMA ONE PAL QFA QTR

RSF SAA SAS SIA SKY SVA TAM TAX THA THY TNA TPA TSC

UAF VIR VOZ XAX XLF

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin:

Service Bulletin No. A330-34-3087

NOTE: Service Bulletin No. A330-34-3087 (NAVIGATION - ANGLE OF ATTACK INDICATION

- INSTALL ANGLE OF ATTACK SENSORS ROSEMOUNT) applies Modification No.

46921S14694.

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER Operator Information Transmission (OIT) No. 999.0017/15

NATURE OF THE WORK

AIRCRAFT NO

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SERVICE BULLETIN

SUMMARY

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 343315-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 3.50

**CONF 002

Task 343315-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 3.50

APPENDICES

**CONF ALL

Appendix 01 - Elapsed Time Assumptions

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SERVICE BULLETIN

SUMMARY

**CONF ALL

FR1

FR20

Z120

A

FR19

FR18

A

3FP2

3FP1

A

TYPICAL INSTALLATION

G_SB_343315_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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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 - AOA - INSTALL AOA PROBES IN MIXED

CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND

UTAS ON STANDBY

MODIFICATION No.: 204937S33428

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 Service Bulletin is only applicable to aircraft equipped with UTAS AOA

PN 0861ED or PN 0861ED2.

(1) Models

330-202 330-203 330-223 330-223F 330-243 330-243F 330-302 330-303

330-321 330-322 330-323 330-342 330-343

(2) Effectivity by MSN

0012 0017 0050 0060 0062 0064-0066 0071 0083 0098-0099 0102 0106 0109

0112-0113 0118 0121-0122 0132 0155 0177 0209 0224 0231 0234 0244 0346 0358

0364 0386 0389 0393 0405 0407 0418 0420-0421 0423 0432 0439 0444 0454 0469

0476 0479 0493 0496-0497 0506 0508 0512-0513 0515 0522 0527 0529-0530 0532

0535 0539 0548 0553 0555 0558 0564-0565 0568 0573-0574 0581 0587 0593 0595

0602-0603 0607 0634 0641 0649 0652 0654-0656 0661-0662 0664-0665 0669 0671

0673 0675 0678-0679 0691-0693 0695 0697 0699 0704-0705 0707 0712-0714 0716

0720 0725 0728 0732 0735 0739 0741-0742 0747 0750 0752 0754-0756 0759 0769

0773-0774 0776-0777 0780-0782 0785-0786 0791 0797 0802 0805 0810 0815 0818

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SERVICE BULLETIN

0821-0823 0825 0828 0830-0831 0836 0838-0842 0847 0850-0851 0853 0855

0860-0862 0866-0867 0871 0873 0875 0879 0881-0882 0884-0885 0887-0890 0892

0895 0898 0901 0903 0906 0908-0909 0911 0915-0916 0919-0920 0923 0926 0928

0930 0932 0935-0937 0940-0942 0944-0945 0947-0949 0951 0954 0956-0959 0961

0964 0967-0969 0976-0978 0980 0982-0986 0988 0990 0994-0998 1003-1004

1006-1007 1009-1010 1012-1013 1015-1016 1020 1023 1025 1028 1035-1038 1044

1049 1051-1052 1060-1063 1067 1073-1074 1078 1080 1085-1088 1090 1092-1094

1096 1098-1099 1105-1108 1110 1112 1115-1116 1118 1120 1124 1127 1129-1130

1132 1136-1137 1141 1146-1150 1153 1156-1157 1159-1160 1163-1164 1168-1170

1172-1175 1177-1178 1180 1183-1184 1186-1187 1189-1192 1195-1196 1198-1199

1201-1202 1204 1206 1208-1210 1212-1216 1219-1224 1227-1229 1231-1237

1239-1240 1243-1244 1247 1249-1251 1254-1256 1258 1260-1263 1266-1272 1274

1277-1282 1284-1286 1288-1289 1291-1293 1296-1299 1301 1303-1307 1309 1311

1314-1315 1317-1320 1322-1325 1328-1333 1335-1338 1341-1353 1356-1358

1360-1362 1364-1375 1378-1380 1382-1384 1386-1388 1391-1392 1394-1398

1400-1402 1406-1410 1412-1413 1416 1418 1420-1421 1424-1425 1427-1432 1434

1436 1438 1440 1442-1450 1452-1454 1456-1463 1465 1467-1468 1470-1471

1473-1479 1482-1485 1487 1489 1491-1495 1497 1500-1501 1503-1506 1508-1510

1513-1514 1516-1517 1519-1520 1522-1523 1525 1527-1529 1531-1532 1534

1536-1548 1550-1554 1557-1563 1566-1575 1577 1579 1582 1585-1588 1591-1593

1595 1597-1599 1602-1603 1605 1607-1609 1614 1616-1618 1620-1625 1629

1632-1636 1639-1640 1642 1644-1645

(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

AFL 1232 1247 1270 1284 1299 1301 1323 1328 1345 1356 1371

AIB 0871

ARG 0358 0364 1605 1623

ASY 0747 0951 0969 1036 1183

AVA 0948 0967 1009 1016 1073 1208 1224 1279 1342 1400 1508

AZU 0527 0532

BER 0432 0444 0454 0469 0476 0493 0665 0739 0822 0828 0911

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450 1539

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 1373 1383 1396

1413 1434 1444 1459 1471 1493 1509 1525 1538 1541 1563 1570

1587

CEB 1420 1445 1495 1527 1552 1602

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 1372 1375 1402 1421 1429 1440 1461 1468 1479

1484 1500 1520 1537 1547 1551 1569 1588 1595 1603 1617 1632

1639

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SERVICE BULLETIN

OPERATOR MSN

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255 1325 1369

1438 1532 1558 1573 1591 1614 1634

CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539

0548 0565 0679 0776 0850 0855 0895 0915 0959 1163 1196 1222

1239 1285 1317 1343 1349 1362 1366 1387 1409 1436 1443 1503

1523 1545 1557 1567 1598 1618 1621

CRK 1051 1062 1115 1175 1277 1286 1320 1322 1358 1384 1398

CSC 1397 1432 1528 1579

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

1392 1425 1430 1494 1519 1536 1575 1593 1625 1636 1645

DLH 1292 1305 1314 1497

EIN 0841 0847 0985 1025 1106

ETD 0825 0831 0885 0888

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 1254

1268 1274

FIN 0994 1007 1013 1023 1067 1078 1088 1173

FJI 1394 1416 1465

GAP 1456 1463

GIA 0988 1020 1028 1052 1184 1214 1261 1288 1364 1410 1446 1474

1548 1560 1577 1585

HDA 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405

0479 0512 0581 0669 0673 1457

HVN 1256 1266

JAI 0923 0947 0956 1351 1361 1370 1391

JST 0842 0853 0945

LAA 1412 1424 1505 1543

MAS 1136 1148 1164 1180 1209 1219 1229 1234 1243 1281 1318 1336

1337 1347 1388 1395 1431 1470 1489

MEA 0926 0984 0995 0998

MNB 1332

OBS 0802

OHY 0098

OMA 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599

ONE 1492 1506 1540 1586 1608

PAL 1449 1460 1467 1475 1482 1504 1510 1531 1546 1553 1559 1566

1568

QFA 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695

0705 0712 0887 0892 0898 0940 0976 1061 1094 1169 1174 1198

1251 1258 1365

QTR 1350 1386 1406

RSF 0980 0996 1235 1379 1478 1516

SAA 1191 1210 1223 1236 1249 1271

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 1382 1401 1427 1447 1453

1477 1485 1517 1544 1562 1597 1609 1633

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SERVICE BULLETIN

OPERATOR MSN

SKY 1483 1491 1542 1554 1574 1592 1607 1624 1635

SVA 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513

TAM 0968 1112 1118 1213 1221

TAX 0692

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 1374 1408

THY 0529 0697 0704 0742 0754 0774 0882 0901 0932 0949 0961 0977

1004 1092 1150 1160 1170 1172 1204 1212 1228 1240 1298 1307

1311 1344 1418 1442 1458 1476 1487 1501 1514 1522 1529 1550

1571 1616 1620 1622 1629 1640 1642 1644

TNA 1357 1378

TPA 1368 1380 1428 1448 1534

TSC 0132 0177 0407

UAF 1080 1186 1250

VIR 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352

VOZ 1293 1306 1319 1407 1452 1561

XAX 0654 0662 0716 0741 0786

XLF 1360

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0050 0060 0062 0064 0065 0066 0071 0083 0098

0099 0102 0106 0109 0112 0113 0118 0121 0122 0132 0155

0177 0209 0224 0231 0234 0244 0346 0358 0364 0386 0389

0393 0405 0407 0418 0420 0421 0423 0432 0439 0444 0454

0469 0476 0479 0493 0496 0497 0506 0508 0512 0513 0515

0522 0527 0529 0530 0532 0535 0539 0548 0553 0555 0558

0564 0565 0568 0573 0574 0581 0587 0593 0595 0602 0603

0607 0634 0641 0649 0652 0654 0655 0656 0661 0662 0664

0665 0669 0671 0673 0675 0678 0679 0691 0692 0693 0695

0697 0699 0704 0705 0707 0712 0713 0714 0716 0720 0725

0728 0732 0735 0739 0741 0742 0747 0750 0752 0754 0755

0756 0759 0769 0773 0774 0776 0777 0780 0781 0782 0785

0786 0791 0797 0802 0805 0810 0815 0818 0821 0822 0823

0825 0828 0830 0831 0836 0838 0839 0840 0841 0842 0847

0850 0851 0853 0855 0860 0861 0862 0866 0867 0871 0873

0875 0879 0881 0882 0884 0885 0887 0888 0889 0890 0892

0895 0898 0901 0903 0906 0908 0909 0911 0915 0916 0919

0920 0923 0926 0928 0930 0932 0935 0936 0937 0940 0941

0942 0944 0945 0947 0948 0949 0951 0954 0956 0957 0958

0959 0961 0964 0967 0968 0969 0976 0977 0978 0980 0982

0983 0984 0985 0986 0988 0990 0994 0995 0996 0997 0998

1003 1004 1006 1007 1009 1010 1012 1013 1015 1016 1020

1023 1025 1028 1035 1036 1037 1038 1044 1049 1051 1052

1060 1061 1062 1063 1067 1073 1074 1078 1080 1085 1086

1087 1088 1090 1092 1093 1094 1096 1098 1099 1105 1106

1107 1108 1110 1112 1115 1116 1118 1120 1124 1127 1129

1130 1132 1136 1137 1141 1146 1147 1148 1149 1150 1153

1156 1157 1159 1160 1163 1164 1168 1169 1170 1172 1173

1174 1175 1177 1178 1180 1183 1184 1186 1187 1189 1190

1191 1192 1195 1196 1198 1199 1201 1202 1204 1206 1208

1209 1210 1212 1213 1214 1215 1216 1219 1220 1221 1222

1223 1224 1227 1228 1229 1231 1232 1233 1234 1235 1236

1237 1239 1240 1243 1244 1247 1249 1250 1251 1254 1255

1256 1258 1260 1261 1262 1263 1266 1267 1268 1269 1270

1271 1272 1274 1277 1278 1279 1280 1281 1282 1284 1285

1286 1288 1289 1291 1292 1293 1296 1297 1298 1299 1301

1303 1304 1305 1306 1307 1309 1311 1314 1315 1317 1318

1319 1320 1322 1323 1324 1325 1328 1329 1330 1331 1332

1333 1335 1336 1337 1338 1341 1342 1343 1344 1345 1346

1347 1348 1349 1350 1351 1352 1353 1356 1357 1358 1360

1361 1362 1364 1365 1366 1367 1368 1369 1370 1371 1372

1373 1374 1375 1378 1379 1380 1382 1383 1384 1386 1387

1388 1391 1392 1394 1395 1396 1397 1398 1400 1401 1402

1406 1407 1408 1409 1410 1412 1413 1416 1418 1420 1421

1424 1425 1427 1428 1429 1430 1431 1432 1434 1436 1438

1440 1442 1443 1444 1445 1446 1447 1448 1449 1450 1452

1453 1454 1456 1457 1458 1459 1461 1462 1463 1465 1467

1468 1470 1471 1473 1474 1475 1476 1477 1478 1479 1482

1483 1484 1485 1487 1489 1491 1492 1493 1494 1495 1497

001 002

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SERVICE BULLETIN

MSN CONFIGURATION

1500 1501 1503 1504 1505 1506 1508 1509 1510 1513 1514

1516 1517 1519 1520 1522 1523 1525 1527 1528 1529 1531

1532 1534 1536 1537 1538 1539 1540 1541 1542 1543 1544

1545 1546 1547 1548 1550 1551 1552 1553 1554 1557 1558

1559 1560 1561 1562 1563 1566 1567 1568 1569 1570 1602

001 002

1460 1571 1572 1573 1574 1575 1577 1579 1582 1585 1586

1587 1588 1591 1592 1593 1595 1597 1598 1599 1603 1605

1607 1608 1609 1614 1616 1617 1618 1620 1621 1622 1623

1624 1625 1629 1632 1633 1634 1635 1636 1639 1640 1642

1644 1645

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Mod. No. 204294S33100 (Service Bulletin No.

A330-34-3311) is not embodied.

**CONF 002

Config. 002 is valid for aircraft on which Mod. No. 204294S33100 (Service Bulletin No.

A330-34-3311) is embodied.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA02 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin:

Service Bulletin No. A330-34-3087

NOTE: Service Bulletin No. A330-34-3087 (NAVIGATION - ANGLE OF ATTACK

INDICATION - INSTALL ANGLE OF ATTACK SENSORS ROSEMOUNT)

applies Modification No. 46921S14694.

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SERVICE BULLETIN

C. REASON

(1) History

The aim of this modification is to allow the airlines to fly in a mixed Angle of Attack

(AOA) configuration.

(2) Objective/Action

This Service Bulletin requires the replacement of two UTAS AoA probes (FINs 3FP1

and 3FP2) PN 0861ED (installed by Mod. No. 46921S14694 or Service Bulletin No.

A330-34-3087) or PN 0861ED2 (installed by Mod. No. 204294S33100 or Service Bulletin

No. A330-34-3311) by two THALES AoA probes PN C16291AB.

(3) Advantages

The accomplishment of this Service Bulletin will allow the airlines to fly in mixed AoA

configurations.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 343315-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

(1) Replace the AOA Probe 1 (FIN 3FP1)

(2) Replace the AOA Probe 2 (FIN 3FP2)

**CONF 002

Task 343315-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

(1) Replace the AOA Probe 1 (FIN 3FP1)

(2) Replace the AOA Probe 2 (FIN 3FP2)

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

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SERVICE BULLETIN

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that this Service Bulletin must be done

before Mar 31/17, the AD will confirm it but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organization Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

**CONF 001

Task 343315-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

Get Access 1.00

On Aircraft

Replace the AOA Probe 1 (FIN 3FP1) 1.00

Replace the AOA Probe 2 (FIN 3FP2) 1.00

Tests 0.50

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 3.50

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumptions .

**CONF 002

Task 343315-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

Get Access 1.00

On Aircraft

Replace the AOA Probe 1 (FIN 3FP1) 1.00

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SERVICE BULLETIN

Task 343315-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

Replace the AOA Probe 2 (FIN 3FP2) 1.00

Tests 0.50

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 3.50

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumptions .

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 34-11-19

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-34-3087

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 34-11-19

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-34-3087

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

Illustrated Parts Catalog (IPC) 34-11-01 34-11-19

L. INTERCHANGEABILITY/MIXABILITY

The interchangeability/mixability possibilities are for new or modified parts introduced by the

accomplishment of this Service Bulletin.

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

AOA Probe 0861ED C16291AB 03 NO (1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): When AOA PN 0861ED is removed, it may be replaced:

- with the AOA PN 0861ED,

- with the AOA PN C16291AB only if both AOA probes (FINs 3FP1 and

3FP2) are replaced simultaneously.

When the new PN is removed, it must be replaced by the new PN.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

AOA Probe 0861ED2 C16291AB 03 NO (1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): When AOA PN 0861ED2 is removed, it may be replaced:

- with the AOA PN 0861ED2,

- with the AOA PN C16291AB only if both AOA probes (FINs 3FP1 and

3FP2) are replaced simultaneously.

When the new PN is removed, it must be replaced by the new PN.

**CONF ALL

M. SPARES

AOA Probe 0861ED

AOA Probe 0861ED2

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Vendor parts are to be procured from:

Equipment BFEA01

Equipment BFEA02

THALES AVIONICS S.A.S.

105, avenue du General Eisenhower

BP 63647

TOULOUSE CEDEX 1

FRANCE

Attn: Retrofit Manager

Tel: +33 5 61 19 76 95

Fax: +33 5 61 19 68 20

e-mail: retrofit@fr.thalesgroup.com

(2) Price and Availability

From Equipment BFEA01 to Equipment BFEA02

No AIRBUS kit will be provided.

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

B. INDUSTRY SUPPORT INFORMATION

From Equipment BFEA01 to Equipment BFEA02

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

This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.

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

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

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

parts listed in the subsequent referenced AMM task:

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

(3) Equipment

Equipment BFEA01

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

NOTES

C16291AB 2 SENSOR 0861ED 03

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.

Equipment BFEA02

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

NOTES

C16291AB 2 SENSOR 0861ED2 03

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.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 343315-831-801-001 - Modification by Replacement of the two AOA Probes (FINs 3FP1

and 3FP2) on Aircraft

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.

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

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

"refer to" are used and the operator has a procedure accepted by the local

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

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

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

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

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

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

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

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

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

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

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

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2

Access

Door 811

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 3.50

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2

Access

Door 811

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 3.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 343315-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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(2) Subtask 343315-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 343315-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(2) Subtask 343315-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 343315-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 34-11-19-000-801

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

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

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position

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

12-34-24-860-802.

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

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

**CONF 002

(1) Subtask 343315-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 34-11-19-000-801

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

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

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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- All controls in NORM, AUTO or OFF position

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

12-34-24-860-802.

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

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

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 343315-831-001-001 - Replace the AOA Probe 1 (FIN 3FP1)

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 811

Work location from Frame 18 to Frame 19

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C16291AB 1 SENSOR

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

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

Task 34-11-19-400-801

(a) Remove:

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

FIN 3FP1

1 AOA Probe 0861ED

(b) Install:

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

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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FIN 3FP1

1 AOA Probe C16291AB

(2) Subtask 343315-831-002-001 - Replace the AOA Probe 2 (FIN 3FP2)

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 811

Work location from Frame 18 to Frame 19

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C16291AB 1 SENSOR

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

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

Task 34-11-19-400-801

(a) Remove:

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

FIN 3FP2

1 AOA Probe 0861ED

(b) Install:

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

FIN 3FP2

1 AOA Probe C16291AB

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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**CONF 002

(1) Subtask 343315-831-001-002 - Replace the AOA Probe 1 (FIN 3FP1)

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 811

Work location from Frame 18 to Frame 19

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C16291AB 1 SENSOR

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

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

Task 34-11-19-400-801

(a) Remove:

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

FIN 3FP1

1 AOA Probe 0861ED2

(b) Install:

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

FIN 3FP1

1 AOA Probe C16291AB

(2) Subtask 343315-831-002-002 - Replace the AOA Probe 2 (FIN 3FP2)

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 811

Work location from Frame 18 to Frame 19

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C16291AB 1 SENSOR

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

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

Task 34-11-19-400-801

(a) Remove:

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

FIN 3FP2

1 AOA Probe 0861ED2

(b) Install:

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

FIN 3FP2

1 AOA Probe C16291AB

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 343315-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

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

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(a) Job Set-up:

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

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

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

(b) Procedure:

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

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

**CONF 002

(1) Subtask 343315-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Job Set-up:

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

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

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

(b) Procedure:

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

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

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 343315-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

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

equipment.

(b) Do the Close-up procedure as specified after the installation of the AOA Probes

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

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

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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**CONF 002

(1) Subtask 343315-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

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

equipment.

(b) Do the Close-up procedure as specified after the installation of the AOA Probes

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

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

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumptions

**CONF ALL

(1) For an explanation of the manhours and elapsed time, refer to the following Gantt Chart.

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumptions

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A330−34−3315

GET ACCESS

MH ET/S

SB ELAPSED TIME

4.50

3.50

STEPS

1.00 1.00

0

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

:

:

SB ELAPSED TIME

(HOURS)

1 2 3 4

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

REPLACEMENT OF THE AOA PROBE 1.00 1.00 1

CLOSE−UP 1.00 1.00 1

TOTAL MANHOURS

1.00 1.00 1

TEST 0.50 0.50 1

FIN 3FP1

REPLACEMENT OF THE AOA PROBE

FIN 3FP2

G_SB_343315_5_AAAA_01_00

Figure A-FAAAA - Sheet 01

Gantt Chart

DATE: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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REPORTING SHEET

TITLE: NAVIGATION - AOA - INSTALL AOA PROBES IN MIXED

CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND

UTAS ON STANDBY

MODIFICATION No.: 204937S33428

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: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

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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: Mar 26/15 SERVICE BULLETIN No.: A330-34-3315

REVISION No.: 00 - Mar 26/15 Page: 1

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