# Airbus Service Bulletin A330-53-3234

Copy: No revision named ("SB A330-53-3234"), 32 pages: PDF https://openairdocs.org/files/sha256/67/c2/67c2df35c836173b4ee6e9cae75a3dfa14a49af266fd2072fef88bfbe334636b; text https://openairdocs.org/service-documents/airbus/a330-53-3234/file/67c2df35c836.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-0465; AD 2016-20-13 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-53-3234
- Page: https://openairdocs.org/service-documents/airbus/a330-53-3234

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2016-20-13](https://openairdocs.org/ad/2016-20-13.md), effective Nov 25, 2016: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-53-3234/proposed.md).

## Text (32 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-0465; AD 2016-20-13 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A330
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
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
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@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
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
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
REVISION No.: 00 - Dec 08/14 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 4
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 5
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 6
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 7
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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
REVISION No.: 00 - Dec 08/14 Page: 8
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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
REVISION No.: 00 - Dec 08/14 Page: 9
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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
first/later)
Condition
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.
S e eN o t e( * )
None
 None
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 10
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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
first/later)
Condition
Action
Threshold
 Grace period
Repetitive
interval
Existing repairs
covered by a
SRM version prior
to April 2013
revision and
l o c a t e do nt h e
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
REVISION No.: 00 - Dec 08/14 Page: 11
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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
first/later)
Condition
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
REVISION No.: 00 - Dec 08/14 Page: 12
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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
occurs first/later)
Condition
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
l o c a t e do nt h e
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
REVISION No.: 00 - Dec 08/14 Page: 13
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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
occurs first/later)
Condition
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 Av iation Safety Agenc y (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 Approv al 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
REVISION No.: 00 - Dec 08/14 Page: 14
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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
REVISION No.: 00 - Dec 08/14 Page: 15
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SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 16
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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
REVISION No.: 00 - Dec 08/14 Page: 17
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SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 18
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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
REVISION No.: 00 - Dec 08/14 Page: 19
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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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 20
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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
REVISION No.: 00 - Dec 08/14 Page: 21
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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
REVISION No.: 00 - Dec 08/14 Page: 22
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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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 23
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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
REVISION No.: 00 - Dec 08/14 Page: 24
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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-G BAAA - S heet 01
Identification of Nose forward fuselage and Center fuselage areas
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 25
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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-G BBAB - S heet 01
Identification of Forward and Rear fuselage areas
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 26
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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
REVISION No.: 00 - Dec 08/14 Page: 27
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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*
NOYES
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.*
NOYES
− 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
DATE: Dec 08/14 SERVICE BULLETIN No.: A330-53-3234
REVISION No.: 00 - Dec 08/14 Page: 28
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 31

@A330
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 concer ned (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
F A X :( + 3 3 )56 19 32 80 6
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
REVISION No.: 00 - Dec 08/14 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 32

@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
F A X:( 3 3 )56 19 34 25 1
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.

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