@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: 53

TITLE: FUSELAGE - INSPECTION OF SKIN DOUBLER REPAIR AT STRINGER

9 JUNCTION BETWEEN FR 10 AND FR13

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A330-53-3235

ADDITIONAL WORK

**CONF ALL

Additional work is required by this revision for aircraft modified by the original issue of this Service

Bulletin.

REASON

Revision No. 01 issued to take into account SRM Temporary Revision 53-001.

CHANGES

The main changes of this revision are:

- SRM Temporary Revision 53-001 (dated Nov 28/14) added.

- Effectivity extended up to MSN 1600.

- ADDITIONAL WORK added for aircraft on which Service Bulletin No. A330-53-3235 Revision No.

00 has already been embodied.

FRONT MATTER

FUSELAGE - INSPECTION OF SKIN

DOUBLER REPAIR AT STRINGER 9

JUNCTION BETWEEN FR 10 AND FR13

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED R

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

Advantages ADVANTAGES UPDATED R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 533235- 832-801-001-Inspection

Subtask 533235-839-001-001 SUBTASK SOLUTION UPDATED

MANPOWER RESSOURCE UPDATED

R

Subtask 533235-832-001-001 SUBTASK SOLUTION UPDATED R

TASK 533235- 832-803-001-ADDITIONAL

WORK for Aircraft on which Service

Bulletin No. A330-53-3235 Revision No.

00 has already been embodied

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Subtask 533235-839-003-001 SUBTASK SOLUTION ADDED N

Subtask 533235-832-003-002 SUBTASK SOLUTION ADDED N

Fig. A-FFAAA

Fig. A-FFAAA Sheet 01 SHEET UPDATED R

FILING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Sep 26/14

REVISION No. : 01 - Jan 14/15

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - INSPECTION OF SKIN DOUBLER REPAIR AT STRINGER

9 JUNCTION BETWEEN FR 10 AND FR13

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Following changes in Apr-2013 revision and Temporary Revision 53-001 (dated Nov 28/14) of SRM

A330, and with regards to previously embodied SRM repairs, Airbus is requiring the operators to apply

specific actions defined in this Service Bulletin.

This Service Bulletin requires the operators to identify records of SRM skin doubler repairs at stringer 9

longitudinal panel junction between Frame 10 and Frame 13.

- In case of an existing SRM repair, recorded prior to SRM Temporary Revision 53-001 (dated Nov

28/14), is located in excluded area of SRM Temporary Revision 53-001 (dated Nov 28/14) or

subsequent SRM revision, please contact AIRBUS Repair Support (SEOE) for further instructions.

- In case of an existing SRM repair, recorded prior to SRM Temporary Revision 53-001 (dated Nov

28/14), is not located in an excluded area of SRM Temporary Revision 53-001 (dated Nov 28/14)

or subsequent SRM revision, please update recorded inspection instructions in line with the current

SRM requirements.

Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of skin doubler

repairs of the longitudinal panel junction at stringer 9 between Frame 10 and Frame 13.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

38W 39V 43P 62S 99Y AAR AAW ABD ACA ACI AEA AFL AFR

AIB AIC ALK ARA ARG ASY AVA AZA AZU BEC BEL BER BGH

CAL CCA CEB CES CHH CPA CRK CRL CSA CSC CSN DAH DAL

DGA DLH EDW EIN ETD EVA EVE FIN FJI FWI GAP GFA GIA

GRL HAL HDA HFY HVN IAW IBE ISS IYE JAI JST KAL KLM

LAA MAS MAU MEA MON MSR NMB OHY OMA ONE PAL QAF QFA

QTR RJA RSF RSY SAA SAI SAS SIA SKY SVA SWR SYA TAE

TAM TAP TCX THA THY TNA TOW TSC UAE UAF USA VIR VKG

VOZ WRC XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 533235-832-801-001: Inspection

TOTAL MANHOURS 2.00

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

Task 533235-832-803-001: ADDITIONAL WORK for Aircraft on which Service Bulletin No.

A330-53-3235 Revision No. 00 has already been embodied

TOTAL MANHOURS 2.00

APPENDICES

None

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 3

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 4

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - INSPECTION OF SKIN DOUBLER REPAIR AT STRINGER

9 JUNCTION BETWEEN FR 10 AND FR13

MODIFICATION No.: None

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321

330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0070-0072

0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116 0118

0120-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0206 0209 0211 0219

0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256

0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288

0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320

0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 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

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

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 0925-0928 0930-0932 0934-0937

0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-1003

1006-1016 1018-1023 1025-1026 1028-1029 1031 1033-1039 1041-1049 1052-1055

1057-1061 1063 1065-1067 1069 1071-1078 1080-1082 1084-1090 1093-1101

1103-1108 1110 1112 1114 1116 1118 1120 1123-1124 1126-1127 1129-1133 1135

1137-1138 1141 1143 1145-1147 1149-1151 1153 1155-1157 1159-1161 1163 1165

1167-1174 1177-1178 1181 1183-1184 1186-1193 1195-1196 1198-1206 1208-1241

1243-1252 1254-1256 1258-1272 1274-1319 1321-1331 1333-1343 1345-1349

1351-1367 1369-1379 1381-1385 1387-1405 1407-1413 1415-1417 1419-1427

1429-1441 1443-1447 1449-1505 1507-1523 1525-1533 1535-1549 1551-1577

1579-1583 1585-1593 1595-1600

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

38W 0401

39V 0874 0939

43P 1053

62S 1321

99Y 1439

AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340

1435 1464 1518

AAW 0999 1043 1472 1499 1535

ABD 0343

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597 0670 0733 0745 0749 0814 0931 0950

0992 1097

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247

1264 1270 1284 1299 1301 1323 1328 1345 1356 1371

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

0567 0584 0657

AIB 0871

AIC 0353 0362

ALK 0303 0306 0311 0313 0404 0456 0627 1564 1583

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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@A330

SERVICE BULLETIN

OPERATOR MSN

ARA 0891 0927

ARG 0290 0300 0358 0364

ASY 0747 0951 0969 1036 1183

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

AZA 0272 0339 1123 1135 1218 1225 1252 1283 1308 1313 1327 1354

AZU 0365 0372 0462 0494 0527 0532

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

BGH 0255

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

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

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

1438 1532 1558 1573 1591

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

CRK 1031 1034 1039 1042 1054 1059 1277 1286 1322 1358 1384 1398

CRL 0285 0320 1359 1376

CSA 0425

CSC 1082 1138 1241 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

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 1497

EDW 0291 1193

EIN 0269 0397 0841 0847 0985 1025 1106

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

0825 0831 0832 0852 0854 0868 0885 0888 0975 0991 1071 1081

1167 1205 1226 1245 1486 1521

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

1268 1274

EVE 0833

FIN 0994 1007 1013 1023 1067 1078 1088 1173

FJI 1394 1416 1465

FWI 0253 0758 0965 1021 1265

GAP 1456 1546

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052 1184 1214

1261 1288 1364 1410 1446 1474 1548 1560 1577 1585

GRL 0230

HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404

1422 1469 1488 1496 1511 1530 1565

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

0479 0512 0581 0669 0673 1457

HFY 0096 0127 0211 0262 0437 0451 1008

HVN 0275 0294 0299 0366 0943 0946 0962 1019 1256 1266

IAW 1339

IBE 1377 1385 1405 1426 1437 1490 1507 1515

ISS 0802

IYE 0625 0632

JAI 0923 0947 0956 1351 1361 1370 1391

JST 0842 0853 0940 0945

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

0351 0368 0428 0484 0490 0550 1133 1155 1200 1203 1393 1556

1576 1590

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 0925 1161

1287 1294 1300 1381 1580

LAA 1412 1424 1505 1543

MAS 0067 0116 1209 1219 1229 1234 1243 1281 1318 1336 1337 1347

1388 1395 1431 1470 1489

MAU 0883 1057

MEA 0926 0984 0995 0998

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246

NMB 1451 1466

OHY 0072 0087 0098 0143

OMA 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599

ONE 1492 1540 1586

PAL 0183 0184 0188 0189 0191 0198 0200 0203 1449 1460 1463 1467

1475 1482 1504 1510 1531 1553 1559 1566 1568

QAF 0487 0605

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

0705 0712 0887 0892 0898 0976 1061 1094 1169 1174 1198 1251

1258 1365

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SERVICE BULLETIN

OPERATOR MSN

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 1379 1478 1516

RSY 0120 0171

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 1382 1401 1427 1447 1453

1477 1485 1517 1544 1562 1597

SKY 1483 1491 1542 1554 1574 1592

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

SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290

1355 1403

SYA 0345

TAE 0348

TAM 0232 0238 0247 0259 0361 0466 0472 0700 0968 1112 1118 1213

1221

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

0914 0934

TCX 0254 0266 0301 0398

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 0463 0504 0529 0697 0704 0742 0754 0774 0869 0876 0882 0901

0932 0949 0961 0977 1150 1160 1170 1172 1204 1212 1228 1240

1298 1307 1311 1458 1476 1487 1501 1514 1522 1529 1571

TNA 1357 1378

TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419 1498 1555

TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 0795 0966 0971

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0382 0384 0392

0396 0409 0452 0455 0491 0509 0518 0525 0536

UAF 1080 1186 1250

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

1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526

VIR 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352

VKG 0309 0349 0356 0357

VOZ 1293 1306 1319 1407 1452 1561

WRC 0296

XAX 0054 0330 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066

1075 1126 1131 1165 1411 1423 1433 1481 1533 1549 1581 1589

1596 1600

XLF 0501 0635 1360

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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@A330

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064

0065 0066 0067 0070 0071 0072 0082 0083 0086 0087 0095

0096 0098 0099 0102 0106 0109 0111 0112 0113 0116 0118

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 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 0925 0926 0927 0928 0930 0931 0932 0934 0935

001

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

MSN CONFIGURATION

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 1006 1007 1008 1009 1010 1011

1012 1013 1014 1015 1016 1018 1019 1020 1021 1022 1023

1025 1026 1028 1029 1031 1033 1034 1035 1036 1037 1038

1039 1041 1042 1043 1044 1045 1046 1047 1048 1049 1052

1053 1054 1055 1057 1058 1059 1060 1061 1063 1065 1066

1067 1069 1071 1072 1073 1074 1075 1076 1077 1078 1080

1081 1082 1084 1085 1086 1087 1088 1089 1090 1093 1094

1095 1096 1097 1098 1099 1100 1101 1103 1104 1105 1106

1107 1108 1110 1112 1114 1116 1118 1120 1123 1124 1126

1127 1129 1130 1131 1132 1133 1135 1137 1138 1141 1143

1145 1146 1147 1149 1150 1151 1153 1155 1156 1157 1159

1160 1161 1163 1165 1167 1168 1169 1170 1171 1172 1173

1174 1177 1178 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 1321 1322 1323 1324 1325 1326 1327 1328 1329 1330

1331 1333 1334 1335 1336 1337 1338 1339 1340 1341 1342

1343 1345 1346 1347 1348 1349 1351 1352 1353 1354 1355

1356 1357 1358 1359 1360 1361 1362 1363 1364 1365 1366

1367 1369 1370 1371 1372 1373 1374 1375 1376 1377 1378

1379 1381 1382 1383 1384 1385 1387 1388 1389 1390 1391

1392 1393 1394 1395 1396 1397 1398 1399 1400 1401 1402

1403 1404 1405 1407 1408 1409 1410 1411 1412 1413 1415

1416 1417 1419 1420 1421 1422 1423 1424 1425 1426 1427

1429 1430 1431 1432 1433 1434 1435 1436 1437 1438 1439

1440 1441 1443 1444 1445 1446 1447 1449 1450 1451 1452

1453 1454 1455 1456 1457 1458 1459 1460 1461 1462 1463

1464 1465 1466 1467 1468 1469 1470 1471 1472 1473 1474

1475 1476 1477 1478 1479 1480 1481 1482 1483 1484 1485

1486 1487 1488 1489 1490 1491 1492 1493 1494 1495 1496

1497 1498 1499 1500 1501 1502 1503 1504 1505 1507 1508

1509 1510 1511 1512 1513 1514 1515 1516 1517 1518 1519

1520 1521 1522 1523 1525 1526 1527 1528 1529 1530 1531

1532 1533 1535 1536 1537 1538 1539 1540 1541 1542 1543

1544 1545 1546 1547 1548 1549 1551 1552 1553 1554 1555

1556 1557 1558 1559 1560 1561 1562 1563 1564 1565 1566

1567 1568 1569 1570 1571 1572 1573 1574 1575 1576 1577

001

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SERVICE BULLETIN

MSN CONFIGURATION

1579 1580 1581 1582 1583 1585 1586 1587 1588 1589 1590

1591 1592 1593 1595 1596 1597 1598 1599 1600

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

No Material Set

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Following changes in Apr-2013 revision and Temporary Revision 53-001 (dated Nov

28/14) of SRM A330, and with regards to previously embodied SRM repairs, Airbus is

requiring the operators to apply specific actions defined in this Service Bulletin.

(2) Objective/Action

This Service Bulletin requires the operators to identify records of SRM skin doubler

repairs at stringer 9 longitudinal panel junction between Frame 10 and Frame 13.

- In case of an existing SRM repair, recorded prior to SRM Temporary Revision

53-001 (dated Nov 28/14), is located in excluded area of SRM Temporary Revision

53-001 (dated Nov 28/14) or subsequent SRM revision, please contact AIRBUS

Repair Support (SEOE) for further instructions.

- In case of an existing SRM repair, recorded prior to SRM Temporary Revision

53-001 (dated Nov 28/14), is not located in an excluded area of SRM Temporary

Revision 53-001 (dated Nov 28/14) or subsequent SRM revision, please update

recorded inspection instructions in line with the current SRM requirements.

(3) Advantages

Accomplishment of this Service Bulletin will contribute to maintain the structural integrity

of skin doubler repairs of the longitudinal panel junction at stringer 9 between Frame 10

and Frame 13.

(4) Operational/Maintenance Consequences

None

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 533235-832-801-001: Inspection

(1) Check if Skin Repairs on Longitudinal Junction at Stringer 9, between Frames 10 and

13, LH and RH Sides, have been accomplished

Task 533235-832-803-001: ADDITIONAL WORK for Aircraft on which Service Bulletin No.

A330-53-3235 Revision No. 00 has already been embodied

(1) Check if Skin Repairs on Longitudinal Junction at Stringer 9, between Frames 10 and

13, LH and RH Sides, have been accomplished

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(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 the AD will confirm the thresholds

given but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

Table 1, Config. 001 - Inspection of SRM skin repair records at stringer 9 longitudinal panel junction

between Frame 10 and Frame 13

Condition Action Compliance time

Threshold Grace period

Repetitive interval

All aircraft Check the aircraft

maintenance

program

documentation for

existing repairs, in

accordance with

the Subtask

533235-832-001-001

Before Sep-2015 None None

No existing repair

covered by a SRM

version prior to

Temporary

Revision 53-001

(Nov 28/14)

No further action

necessary within

this Service

Bulletin

None None None

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

Table 1, Config. 001 - Inspection of SRM skin repair records at stringer 9 longitudinal panel junction

between Frame 10 and Frame 13

Condition Action Compliance time

Threshold Grace period

Repetitive interval

Existing repair

covered by a SRM

version prior to

Temporary

Revision 53-001

(Nov 28/14) and

repair located in an

excluded area of

Temporary

Revision 53-001

(Nov 28/14) or

subsequent SRM

revision

Contact AIRBUS

with detailed repair

report for specific

assessment and

follow their

instructions

As soon as

possible Before

Sep-2015

See NOTE (*)

None None

Existing repair

covered by a SRM

version prior to

Temporary

Revision 53-001

(Nov 28/14) and

repair not located

in an excluded

area of Temporary

Revision 53-001

(Nov 28/14) or

subsequent SRM

revision

Update recorded

inspection

instructions in line

with the current

SRM requirements

During

accomplishment of

this Service

Bulletin

None None

NOTE (*): It is recommended to contact Airbus 6 months before the end of the

Compliance Time.

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

Task 533235-832-801-001: Inspection

On Bench

Check if Skin Repairs on Longitudinal Junction at

Stringer 9, between Frames 10 and 13, LH and RH

Sides, have been accomplished

2.00

TOTAL MANHOURS 2.00

Task 533235-832-803-001: ADDITIONAL WORK for Aircraft on which Service Bulletin No.

A330-53-3235 Revision No. 00 has already been embodied

On Bench

Check if Skin Repairs on Longitudinal Junction at

Stringer 9, between Frames 10 and 13, LH and RH

Sides, have been accomplished

2.00

TOTAL MANHOURS 2.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

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

Structural Repair Manual (SRM) 53-11-11

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

None

(2) Price and Availability

None

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of the Service Bulletin.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 533235-832-801-001 - Inspection

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

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

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

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

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

Task Associated Data

Manpower

TOTAL MANHOURS 2.00

A. GENERAL

(1) Subtask 533235-839-001-001 - 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

None

C. PROCEDURE

(1) Subtask 533235-832-001-001 - Check if Skin Repairs on Longitudinal Junction at

Stringer 9, between Frames 10 and 13, LH and RH Sides, have been accomplished

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Structural Repair Manual (SRM) 53-11-11, Page Block 201

Fig. A-FFAAA

Flow Chart

Sheet 01

NOTE: For the accomplishment timescale, refer to 1.E.(2).

(a) Check in the aircraft maintenance program documentation if skin repairs on

longitudinal junction at stringer 9, between frames 10 and 13, have been

accomplished in accordance with any of the following SRM references:

- SRM 53-11-11, Page Block 201, paragraph 5.D (Figure 204)

- SRM 53-11-11, Page Block 201, paragraph 5.E (Figure 205)

- SRM 53-11-11, Page Block 201, paragraph 5.I (Figure 209)

- SRM 53-11-11, Page Block 201, paragraph 5.J (Figure 210)

Refer to Flow Chart Fig. A-FFAAA

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SERVICE BULLETIN

1 If some repairs covered by a SRM version prior to Temporary Revision 53-001

(dated Nov 28/14) are found and if the repair is located in an excluded area of

Temporary Revision 53-001 (dated Nov 28/14) or subsequent SRM revision,

contact AIRBUS Repair Support (SEOE) with detailed repair report for specific

assessment and follow their instructions.

2 If some repairs covered by a SRM version prior to Temporary Revision 53-001

(dated Nov 28/14) are found and if the repair is not located in an excluded

area of Temporary Revision 53-001 (dated Nov 28/14) or subsequent SRM

revision, update the recorded inspection instructions in accordance with the

current SRM requirements.

NOTE: Any new repair inspection instruction following this update can

be achieved at the customer’s convenience:

- At any time within the compliance time of this Service

Bulletin, but not later than any existing repair inspection

already scheduled before update,

or:

- In accordance with the new inspection instruction updated

following this Service Bulletin.

Only the schedule of the updated inspection instruction is

required to close this Service Bulletin, not the inspection itself.

3 If no repair covered by a SRM version prior to Temporary Revision 53-001

(dated Nov 28/14) is found, no further action is required.

D. TEST

None

E. CLOSE-UP

None

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

Task 533235-832-803-001 - ADDITIONAL WORK for Aircraft on which Service Bulletin No.

A330-53-3235 Revision No. 00 has already been embodied

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: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

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

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

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

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

Task Associated Data

Manpower

TOTAL MANHOURS 2.00

A. GENERAL

(1) Subtask 533235-839-003-001 - 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

None

C. PROCEDURE

(1) Subtask 533235-832-003-002 - Check if Skin Repairs on Longitudinal Junction at

Stringer 9, between Frames 10 and 13, LH and RH Sides, have been accomplished

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Structural Repair Manual (SRM) 53-11-11, Page Block 201

Fig. A-FFAAA

Flow Chart

Sheet 01

NOTE: For the accomplishment timescale, refer to 1.E.(2).

(a) Check in the aircraft maintenance program documentation if skin repairs on

longitudinal junction at stringer 9, between frames 10 and 13, have been

accomplished in accordance with any of the following SRM references:

- SRM 53-11-11, Page Block 201, paragraph 5.D (Figure 204)

- SRM 53-11-11, Page Block 201, paragraph 5.E (Figure 205)

- SRM 53-11-11, Page Block 201, paragraph 5.I (Figure 209)

- SRM 53-11-11, Page Block 201, paragraph 5.J (Figure 210)

Refer to Flow Chart Fig. A-FFAAA

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SERVICE BULLETIN

1 If some repairs covered by a SRM version prior to Temporary Revision 53-001

(dated Nov 28/14) are found and if the repair is located in an excluded area of

Temporary Revision 53-001 (dated Nov 28/14) or subsequent SRM revision,

contact AIRBUS Repair Support (SEOE) with detailed repair report for specific

assessment and follow their instructions.

2 If some repairs covered by a SRM version prior to Temporary Revision 53-001

(dated Nov 28/14) are found and if the repair is not located in an excluded

area of Temporary Revision 53-001 (dated Nov 28/14) or subsequent SRM

revision, update the recorded inspection instructions in accordance with the

current SRM requirements.

NOTE: Any new repair inspection instruction following this update can

be achieved at the customer’s convenience:

- At any time within the compliance time of this Service

Bulletin, but not later than any existing repair inspection

already scheduled before update,

or:

- In accordance with the new inspection instruction updated

following this Service Bulletin.

Only the schedule of the updated inspection instruction is

required to close this Service Bulletin, not the inspection itself.

3 If no repair covered by a SRM version prior to Temporary Revision 53-001

(dated Nov 28/14) is found, no further action is required.

D. TEST

None

E. CLOSE-UP

None

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

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SERVICE BULLETIN

**CONF ALL

IDENTIFY THE RECORDS OF SRM SKIN REPAIRS ON LONGITUDINAL

PANEL JUNCTION AT STRINGER 9, BETWEEN FRAMES 10 AND 13,

YES COVERED BY A SRM VERSION PRIOR

IS EXISTING REPAIR

CONTACT AIRBUS

WITH DETAILED

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION

GIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND

NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR 

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN

NO FURTHER ACTION WITHIN

THIS SERVICE BULLETIN

01 FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARA 1.E.(2)

01

IN ACCORDANCE WITH SUBTASK 533235−832−001−001

TO TEMPORARY REVISION 53−001

01

REPAIR REPORT

ASSESSMENT AND

QUESTION

ACTION

FINDING

FOLLOW THEIR 

NO

YES

IN EXCLUDED AREA OF TEMPORARY

IS REPAIR LOCATED

REVISION 53−001 (DATED NOV 28/14) OR NO

SUBSEQUENT SRM REVISION?

INSTRUCTIONS

 FOR SPECIFIC

UPDATE THE RECORDED

INSPECTION THRESHOLD AND

02

INTERVALS IN LINE WHITH THE

TEMPORARY REVISION 53−001

(DATED NOV 28/14)

VALUES GIVEN IN THE

01

02 ANY NEW REPAIR INSPECTION INSTRUCTION FOLLOWING THIS UPDATE CAN 

BE ACHIEVED, AT THE CUSTOMER’S CONVENIENCE:

− AT ANY TIME WITHIN THE SB COMPLIANCE TIME BUT NOT LATER THAN ANY EXISTING REPAIR

INSPECTION ALREADY SCHEDULED BEFORE UPDATE,

OR:

− IN ACCORDANCE WITH THE NEW INSPECTION INSTRUCTION UPDATED FOLLOWING THIS

SERVICE BULLETIN. ONLY THE SCHEDULE OF THE UPDATED INSPECTION INSTRUCTION IS 

REQUIRED TO CLOSE THIS SERVICE BULLETIN, NOT THE INSPECTION ITSELF

(DATED NOV 28/14) ?

OR SUBSEQUENT SRM REVISION

G_SB_533235_5_FAAA_01_03

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 22

5

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@A330

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - INSPECTION OF SKIN DOUBLER REPAIR AT STRINGER

9 JUNCTION BETWEEN FR 10 AND FR13

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 1

5

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@A330

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Sep 26/14 SERVICE BULLETIN No.: A330-53-3235

REVISION No.: 01 - Jan 14/15 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.