@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 FUSELAGE SKIN PANELS

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Following changes in the Apr01/13 revision of the Structural Repair Manual (SRM) for A330 aircraft,

and with regards to previously embodied SRM repairs, AIRBUS now requires operators to apply specific

actions listed in this Service Bulletin.

This Service Bulletin is issued to instruct operators to examine their records and take the applicable

corrective action when necessary.

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

skin panels.

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.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

REVISION No.: 00 - Dec 08/14 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

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 GFA GIA GRL

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

MAS MAU MEA MON MSR OHY OMA PAL QAF QFA QTR RJA RSF

RSY SAA SAI SAS SIA 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 YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 533234-832-848-001: Inspection

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

**CONF 002

Task 533234-832-848-001: Inspection

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

APPENDICES

**CONF ALL

None

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

REVISION No.: 00 - Dec 08/14 Page: 2

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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 FUSELAGE SKIN PANELS

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

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

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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@A330

SERVICE BULLETIN

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 1443-1444

(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

AAW 0999 1043

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

ARA 0891 0927

ARG 0290 0300 0358 0364

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@A330

SERVICE BULLETIN

OPERATOR MSN

ASY 0747 0951 0969 1036 1183

AVA 0948 0967 1009 1016 1073 1208 1224 1279 1342 1400

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

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

CEB 1420

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

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

1438

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

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

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

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

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

1167 1205 1226 1245

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

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@A330

SERVICE BULLETIN

OPERATOR MSN

FWI 0253 0758 0965 1021 1265

GFA 0276 0281 0286 0287 0334 0340

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

1261 1288 1364 1410

GRL 0230

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

1422

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

0479 0512 0581 0669 0673

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

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

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

1287 1294 1300 1381

LAA 1412 1424

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

1388 1395 1431

MAU 0883 1057

MEA 0926 0984 0995 0998

MON 0261 0265

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

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 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

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

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

SVA 1108 1127 1137 1141 1147 1153 1189 1192

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

TNA 1357 1378

TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419

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

VIR 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352

VKG 0309 0349 0356 0357

VOZ 1293 1306 1319 1407

WRC 0296

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

1075 1126 1131 1165 1411 1423 1433

XLF 0501 0635 1360

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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 0525 0526 0527

0529 0530 0532 0535 0536 0539 0548 0550 0551 0565 0567

0568 0581 0584 0597 0627 0635 0657

001

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@A330

SERVICE BULLETIN

MSN CONFIGURATION

0524 0533 0542 0549 0552 0553 0555 0558 0564 0570 0571

0573 0574 0576 0578 0579 0587 0588 0591 0593 0595 0600

0602 0603 0605 0607 0609 0610 0612 0614 0616 0618 0620

0621 0623 0625 0629 0631 0632 0633 0634 0636 0637 0638

0640 0641 0642 0644 0645 0647 0648 0649 0650 0652 0653

0654 0655 0656 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 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

002

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@A330

SERVICE BULLETIN

MSN CONFIGURATION

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

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft in the effectivity of this Service Bulletin that have not

embodied Modification No. 49144S16279.

**CONF 002

Config. 002 is valid for aircraft in the effectivity of this Service Bulletin that have

embodied Modification No. 49144S16279.

(6) Material Effectivity

No Material Set

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Following changes in the Apr01/13 revision of the Structural Repair Manual (SRM) for

A330 aircraft, and with regards to previously embodied SRM repairs, AIRBUS now

requires operators to apply specific actions listed in this Service Bulletin.

(2) Objective/Action

This Service Bulletin is issued to instruct operators to examine their records and take the

applicable corrective action when necessary.

(3) Advantages

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

of fuselage skin panels.

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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@A330

SERVICE BULLETIN

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 533234-832-848-001: Inspection

(1) Do a check of the Aircraft Records

**CONF 002

Task 533234-832-848-001: Inspection

(1) Do a check of the Aircraft Records

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

(2) Accomplishment Timescale

Table 01, Config. 001 - A330-200 and A330-300 SRM Update of the Fuselage Skin Repairs

Compliance time (Whichever occurs

Condition first/later)

Action

Threshold Grace period

Repetitive

interval

All Aircraft Check the Aircraft records

and identify all the skin

repairs performed as per the

Structural Repair Manual in

the following areas:

Nose forward fuselage

(Section 11/12):

- lower shell panels below

stringers 31 LH thru 31 RH

- lateral and upper panels

between Frame (FR) 10

and 18, except panel

junction at stringer 9

between FR 10 and 13

- skin panels between FR 18

and 19, below stringers 43

LH/RH

Center fuselage (Section

15):

- skin panels between FR 38

and 53.3

- skin panels between FR

53.3 and 54 below

stringers 31 LH/RH

Forward and Rear fuselage

(Sections 13, 14, 14A, 15A,

and 16 thru 18):

- skin panels between FR 18

and 19 above stringer 43

LH/RH

- skin panels between FR 19

and 38

- skin panels between FR

53.3 and 54 above stringer

31 LH/RH

- skin panels between FR 54

and 80

24 months from

September 2014.

See Note (*)

None None

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

Table 01, Config. 001 - A330-200 and A330-300 SRM Update of the Fuselage Skin Repairs

Compliance time (Whichever occurs

Condition first/later)

Action

Threshold Grace period

Repetitive

interval

Existing repairs

covered by a

SRM version prior

to April 2013

revision and

located on the

Nose Forward

fuselage or center

fuselage

Update the recorded

inspection threshold and

interval in line with the value

given in the April 2013 or

subsequent SRM revisions.

As soon as possible

before September

2016 See Note (***)

None None

Existing repairs

covered by a

SRM version prior

to April 2013

revision , located

on the Forward

and Rear

fuselage but no

longer covered in

the current SRM

(i,e : SRM Figure

inactivated or the

repair in an

excluded area)

Contact AIRBUS with a

detailed repair report for

specific assessment.

As soon as possible

before September

2016 See note (**)

None None

Existing repairs

covered by a

SRM version prior

to April 2013

revision, located

on the Forward

and Rear

fuselage and still

covered in the

current SRM (i,e :

SRM Figure not

inactive and the

repair is not in an

excluded area)

Check if the structure

underneath the skin (frames

or stringers) has been

repaired

As soon as possible

before September

2016 See note (***)

None None

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

Table 01, Config. 001 - A330-200 and A330-300 SRM Update of the Fuselage Skin Repairs

Compliance time (Whichever occurs

Condition first/later)

Action

Threshold Grace period

Repetitive

interval

Existing repairs

covered by a

SRM version prior

to April 2013

revision, located

on the Forward

and Rear

fuselage, still

covered in the

current SRM (i.e:

SRM Figure not

inactive and the

repair not in an

excluded area)

and without any

structural repair

underneath the

skin

Update the recorded

inspection threshold and

interval in line with the

values given in the April

2013 or subsequent SRM

revisions

As soon as possible

before September

2016 See note (***)

None None

Existing repairs

covered by a

SRM version prior

to April 2013

revision, located

on the Forward

and Rear

fuselage, still

covered in the

current SRM (i.e :

SRM Figure not

inactive and the

repair not in an

excluded area)

and with a

structural repair

underneath the

skin.

Contact AIRBUS with a

detailed repair report for

specific assessment

As soon as possible

before September

2016 See note (**)

None None

No existing repair

covered by a

SRM version prior

to April 2013

revision

No further action necessary

within this Service Bulletin

None None None

NOTE: (*): It is recommended to check records within 6 months after SB issue

date.

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

compliance time.

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

NOTE: (***): Any new Repair inspection instruction following this update can be

achieved at the customers convenience:

- at anytime within the SB compliance time but no later than any

existing repair inspection already scheduled before update

- as per the new inspection instruction updated following this SB

Only the schedule of the updated inspection instruction is required to

close the SB, not the inspection itself.

Table 01, Config. 002 - A330-200 and A330-300 SRM Update of the Fuselage Skin Repairs

Compliance time (Whichever

Condition occurs first/later)

Action

Threshold Grace period

Repetitive

interval

All Aircraft Check the Aircraft records

and identify all the skin

repairs performed as per the

Structural Repair Manual

(SRM) in the following areas:

Nose forward fuselage

(Section 11/12):

- lower shell panels below

stringers 31 LH thru 31RH

- lateral and upper panels

between frames 10 and 18,

except panel junction at

stringer 9 between frames

10 and 13

- skin panels between frames

18 and 19, below stringers

43 LH/RH

Center fuselage (Section 15):

- skin panels between frames

38 and 53.3

- skin panels between frames

53.3 and 54 below stringers

31 LH/RH

24 months from

September 2014.

See Note (*)

None None

Existing repairs

covered by a

SRM version prior

to April 2013

revision and

located on the

Nose Forward

fuselage or center

fuselage

Update the recorded

inspection threshold and

interval in line with the value

given in the April 2013 or

subsequent SRM revisions.

As soon as possible

before September

2016 See Note (**)

None None

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

Table 01, Config. 002 - A330-200 and A330-300 SRM Update of the Fuselage Skin Repairs

Compliance time (Whichever

Condition occurs first/later)

Action

Threshold Grace period

Repetitive

interval

No existing repair

covered by a

SRM version prior

to April 2013

revision

No further action necessary

within this Service Bulletin

None None None

NOTE: (*): It is recommended to check records within 6 months after SB issue

date.

NOTE: (**): Any new Repair inspection instruction following this update can be

achieved at the customers convenience:

- at anytime within the SB compliance time but no later than any

existing repair inspection already scheduled before update

- as per the new inspection instruction updated following this SB

Only the schedule of the updated inspection instruction is required to

close the SB, not the inspection itself.

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 and

date given 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

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.

**CONF 001

Task 533234-832-848-001: Inspection

On Aircraft

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

Task 533234-832-848-001: Inspection

Do a check of the Aircraft Records 1.00

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

**CONF 002

Task 533234-832-848-001: Inspection

On Aircraft

Do a check of the Aircraft Records 1.00

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Structural Repair Manual (SRM) 53-00-11 53-11-11 53-31-11

**CONF 002

Structural Repair Manual (SRM) 53-11-11 53-31-11

**CONF ALL

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

No Material Set

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this 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: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 533234-832-848-001 - Inspection

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: 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.

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.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

**CONF 002

Manpower

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 533234-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

**CONF 002

(1) Subtask 533234-839-201-001 - 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

None

**CONF 002

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 533234-839-202-001 - Do a check of the Aircraft Records

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Structural Repair Manual (SRM) 53-00-11

53-11-11

53-31-11

Fig. A-GBAAA

Identification of Nose forward fuselage

and Center fuselage areas

Sheet 01

Fig. A-GFAAB

Flow Chart

Sheet 01

Fig. A-GBBAB

Identification of Forward and Rear

fuselage areas

Sheet 01

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SERVICE BULLETIN

(a) Do a check of the aircraft records for SRM repairs in the given areas, refer to Fig.

A-GBAAA Sheet 01, Fig. A-GBBAB Sheet 01, Fig. A-GFAAB Sheet 01 and the

table below.

FUSELAGE SECTION LOCATION SRM REPAIR REFERENCES

Forward Fuselage and Rear

Fuselage

Fuselage Skin panels in sections

13 and 14/14A:

- panels between FR 18 and FR

19 above stringer 43 LH and

RH

- panels between FR19 and FR

38

Fuselage Skin panels in sections

15A and 16 thru 18:

- panels between FR 53.3 and

FR 54 above stringer 31 LH

and RH

- panels between FR 54 and 80

SRM 53-00-11 Figures:

- 202 thru 210

- 213 thru 216

- 223 thru 237

Nose Forward Fuselage Fuselage Skin panels in sections

11/12:

- Lower shell panels below

stringers 31 LH-31 RH

- Lateral and Upper panels

between FR 10 and FR

18, except panel junction at

stringer 9 between FR 10 and

FR 13

- Panels between FR 18 and

FR 19 and below stringers 43

LH/RH

SRM 53-11-11 Figures:

- 201 thru 203

- 206 thru 208

- 211 thru 213

Center Fuselage Fuselage skin panels in sections

15:

- Panels between FR 38 and FR

53.3

- Panels between FR 53.3 and

FR 54 and below stringer 31

LH/RH

SRM 53-31-11 Figures:

- 209 thru 212

If the repair(s) is/are NOT covered by SRM revision prior to April-13, no further

action is required in accordance with this Service Bulletin.

Existing repair is covered by a SRM version prior to April-13 revision:

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

- If the repair is located on the Nose Forward fuselage or center fuselage, then

update the recorded inspection threshold and intervals in line with the values

given in the April-13 revision or subsequent SRM revision.

- If a repair is NOT located on the Nose Forward fuselage or center fuselage:

. If repair is still covered by the current SRM version (i.e :SRM Figure is not

inactive and the repair is not in an excluded area), then check if the

structure underneath the skin (frame or stringer) has been repaired.

. If there is no structural repair underneath the skin, then update the

recorded inspection threshold and intervals in line with the values given in

the April-13 or subsequent SRM revisions.

. If there is a structural repair underneath the skin, then contact AIRBUS

with a detailed repair report for specific assessment

. If the repair is no longer covered by the current SRM (SRM Figure is

inactive or the repair is now in an excluded area), then contact AIRBUS

with a detailed repair report for specific assessment

**CONF 002

(1) Subtask 533234-839-202-002 - Do a check of the Aircraft Records

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Structural Repair Manual (SRM) 53-11-11

53-31-11

Fig. A-GBAAA

Identification of Nose forward fuselage

and Center fuselage areas

Sheet 01

Fig. A-GFAAA

Flow Chart

Sheet 01

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

(a) Do a check of the aircraft records for SRM repairs in the given areas, refer to Fig.

A-GBAAA Sheet 01, Fig. A-GFAAA Sheet 01 and the table below.

FUSELAGE SECTION LOCATION SRM REPAIR REFERENCES

Nose Forward Fuselage Fuselage Skin panels in

sections 11/12:

- Lower shell panels below

stringers 31 LH thru 31 RH

- Lateral and Upper panels

between FR 10 and FR

18, except panel junction at

stringer 9 between FR 10 and

FR 13

- Panels between FR 18 and

FR 19 and below stringers 43

LH/RH

SRM 53-11-11 Figures:

- 201 thru 203

- 206 thru 208

- 211 thru 213

Center Fuselage Fuselage skin panels in

sections 15:

- Panels between FR 38 and

FR 53.3

- Panels between FR 53.3 and

FR 54 and below stringer 31

LH/RH

SRM 53-31-11 Figures:

- 209 thru 212

- If the repair(s) are NOT covered by SRM revision prior to Apr-13, no further

action is required in accordance with this Service Bulletin.

- If the repair is covered by a SRM version prior to April-13 revision, update the

recorded inspection threshold and intervals in line with the value given in the

April-13 or subsequent SRM revisions.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

None

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

**CONF ALL

A

B

NOTE:

AREA OF INSPECTION

FR19

FR10

FR18

FR0

STGR43

STGR31

FR13

FWD

FWD

A

FR38 FR53.3

FR54

B

STGR31

STGR43

STGR9

G_SB_533234_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Identification of Nose forward fuselage and Center fuselage areas

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

**CONF 001

A

NOTE:

AREA OF INSPECTION

FWD

FR38 FR53.3

FR54

FR18

FR19

FR80

A

STGR31

STGR43

G_SB_533234_6_BBAB_01_00

Figure A-GBBAB - Sheet 01

Identification of Forward and Rear fuselage areas

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

**CONF 002

NO

YES

UPDATE THE RECORDED INSPECTION

THRESHOLD AND INTERVALS IN LINE WITH 

THE VALUES GIVEN IN THE APR−13 OR

SUBSEQUENT SRM REVISIONS

NO FURTHER ACTION

AS PER THIS

SERVICE BULLETIN

02

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.

IT IS RECOMMENDED TO CHECK RECORDS WITHIN 6 MONTHS AFTER SB ISSUE DATE

NOTE:

ANY NEW REPAIR INSPECTION INSTRUCTION FOLLOWING THIS UPDATE CAN BE ACHIEVED, AT THE CUSTOMERS CONVENIENCE

01

− AT ANY TIME WITHIN THE SB COMPLIANCE TIME BUT NOT LATER THAN ANY EXISTING REPAIR INSPECTION ALREADY SCHEDULED BEFORE UPDATE, OR

− AS PER THE NEW INSPECTION INSTRUCTION UPDATED FOLLOWING THIS SB

02

ONLY THE SCHEDULE OF THE UPDATED INSPECTION INSTRUCTION IS REQUIRED TO CLOSE THIS SB, NOT THE INSPECTION ITSELF

* REFER TO FIGURE A−GBAAA SHEET 01.

IDENTIFY RECORDS OF SRM REPAIRS.

FOR EACH RECORD, FOLLOW THE BELOW INSTRUCTIONS 01

EXISTING REPAIR

IS COVERED BY A SRM

VERSION PRIOR TO APR−13

REVISION AND LOCATED ON THE

NOSE FORWARD FUSELAGE* OR

CENTER FUSELAGE*?

G_SB_533234_6_FAAA_01_05

Figure A-GFAAA - Sheet 01

Flow Chart

DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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SERVICE BULLETIN

**CONF 001

UPDATE THE RECORDED INSPECTION

THRESHOLD AND INTERVALS IN LINE WITH 

THE VALUES GIVEN IN THE APR−13 OR

SUBSEQUENT SRM REVISIONS

CONTACT AIRBUS WITH A 

DETAILED REPAIR REPORT 

FOR SPECIFIC ASSESSMENT

NO FURTHER ACTION

AS PER THIS

SERVICE BULLETIN

02

03

SKIN UNDERNEATH

STRUCTURE (FRAME OR

STRINGER) HAS BEEN

REPAIRED

NO YES

YES NO

EXISTING REPAIR

IS LOCATED ON NOSE

FORWARD FUSELAGE* OR

CENTER FUSELAGE*

YES NO

EXISTING REPAIR IS

COVERED BY A SRM

VERSION PRIOR TO APR−13

REVISION

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.

IT IS RECOMMENDED TO CHECK RECORDS WITHIN 6 MONTHS AFTER SB ISSUE DATE

NOTE:

IT IS RECOMMENDED TO CONTACT AIRBUS 6 MONTHS BEFORE END OF THE COMPLIANCE TIME

ANY NEW REPAIR INSPECTION INSTRUCTION FOLLOWING THIS UPDATE CAN BE ACHIEVED, AT THE CUSTOMERS CONVENIENCE

01

02

− AT ANY TIME WITHIN THE SB COMPLIANCE TIME BUT NOT LATER THAN ANY EXISTING REPAIR INSPECTION ALREADY SCHEDULED BEFORE UPDATE, OR

− AS PER THE NEW INSPECTION INSTRUCTION UPDATED FOLLOWING THIS SB

03

ONLY THE SCHEDULE OF THE UPDATED INSPECTION INSTRUCTION IS REQUIRED TO CLOSE THIS SB, NOT THE INSPECTION ITSELF

* REFER TO FIGURES A−GBAAA SHEET 01 AND FIGURE A−GBBAB SHEET 01.

YES NO

− THE SRM FIGURE IS NOT INACTIVE, AND

− THE REPAIR IS NOT IN AN 

EXCLUDED AREA

EXISTING REPAIR

IS IN FORWARD OR REAR

FUSELAGE* IS THE REPAIR STILL 

COVERED IN THE CURRENT SRM VERSION: i.e. 

IDENTIFY RECORDS OF SRM REPAIRS.

FOR EACH RECORD, FOLLOW THE BELOW INSTRUCTIONS 01

G_SB_533234_6_FAAB_01_05

Figure A-GFAAB - Sheet 01

Flow Chart

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - INSPECTION OF FUSELAGE SKIN PANELS

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: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234

REVISION No.: 00 - Dec 08/14 Page: 1

6

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