# Airbus Service Bulletin A330-92-3132

Copy: Revision 01 ("A330-92-3132 R01"), 39 pages: PDF https://openairdocs.org/files/sha256/34/4f/344f118f07fcf99da6649b3b38fdabeb0ddfdf659043f22da6cde05369727f29; text https://openairdocs.org/service-documents/airbus/a330-92-3132/file/344f118f07fc.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-3988; AD 2016-11-19 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: A330-92-3132
- Latest revision known: A330-92-3132, Revision 01, dated May 21, 2015 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/airbus/a330-92-3132

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

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

- [AD 2016-11-19](https://openairdocs.org/ad/2016-11-19.md), effective Jul 22, 2016: Revision 01

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-92-3132/proposed.md).

## Text (39 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-3988; AD 2016-11-19 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
REVISION TRANSMITTAL SHEET
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: 92
TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION-CABLE LOOM
INSTALLATION DRAWINGS-IMP ROVEMENT OF FEEDER ROUTING
ATTACHMENT IN WING/PYLON
MODIFICATION No.: 203672D50692
This page transmits Revision No.01 of Service Bulletin No.A330-92-3132
ADDITIONAL WORK
**CONF ALL
No additional work is required by this revision for aircraft modified by any previous issue.
REASON
Revision No. 01 issued to:
- replace the consumable material 08ADB1 with consumable 08BPA1
- add the correct ESPM references
- add work steps in Para 3.C. to rework the holes in bracket, Item 3, if necessary
- correct Figure A-GBAAA
- add Appendix 02
- update the Service Bulletin effectivity.
CHANGES
SUMMARY
REASON/DESCRIPTION/OPERATIONAL
CONSEQUENCES
REASON UPDATED
 R
MATERIAL PRICE INFORMATION
 MATERIAL PRICE INFORMATION TABLE
UPDATED
R
EFFECTIVITY
 OPERATOR LIST UPDATED
 R
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
REFERENCES / REPERCUSSIONS
 REFERENCES/REPERCUSSIONS TABLE
UPDATED
R
APPENDICES
 APPENDICES UPDATED
 R
PLANNING INFORMATION
EFFECTIVITY
 EFFECTIVITY RELATED INFORMATION
UPDATED
R
Configuration definition
CONF 001
 CONFIGURATION DEFINITION UPDATED
 R
Material Effectivity
 MATERIAL EFFECTIVITY UPDATED
MATERIAL SET UPDATED
MATERIAL SET QUANTITY UPDATED
R
REASON
Objective/Action
 OBJECTIVE/ACTION UPDATED
 R
REFERENCES
 REFERENCED DOCUMENTATION UPDATED
 R
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY
Procurement Addresses
 PROCUREMENT ADDRESSES UPDATED
MATERIAL SET UPDATED
R
Price and Availability
 PRICE AND AVAILABILITY UPDATED
MATERIAL SET UPDATED
R
LIST OF COMPONENTS
Kit 923132D01R03
 PART MATERIAL SET UPDATED
MATERIAL SET LABEL UPDATED
QUANTITY UPDATED
NOTE UPDATED
R
LIST OF MATERIALS - OPERATOR
SUPPLIED
Consumable Materials
Consumable CMLD01
 CONSUMABLE MATERIAL SET UPDATED
CONSUMABLE UPDATED
R
ACCOMPLISHMENT INSTRUCTIONS
TASK 923132- 831-848-001-Modification
Subtask 923132-910-201-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 923132-831-201-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
NOTE UPDATED
CONSUMABLE UPDATED
REFERENCED DOCUMENTATION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
R
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 923132-831-202-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
NOTE UPDATED
CONSUMABLE UPDATED
REFERENCED DOCUMENTATION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
R
Subtask 923132-942-201-001
 SUBTASK SOLUTION UPDATED
 R
Fig. A-GBAAA
 FIGURE SOLUTION UPDATED
 R
Fig. A-GBAAA Sheet 01
 SHEET UPDATED
 R
Fig. A-GBAAA Sheet 02
 SHEET ADDED
 N
Appendix 02 - Post SB Installation Details
APPENDIX CONTENT
 APPENDIX CONTENT ADDED
 N
Fig. A-GABAA
 FIGURE SOLUTION ADDED
 N
Fig. A-GABAA Sheet 01
 SHEET ADDED
 N
Fig. A-GABAA Sheet 02
 SHEET ADDED
 N
FILLING INSTRUCTIONS
This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS
No previous revision
REVISION SEQUENCE
ORIGINAL: Jun 19/14
REVISION No. : 01 - May 21/15
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
This Page Intentionally Left Blank
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 4
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@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: 92
TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION-CABLE LOOM
INSTALLATION DRAWINGS-IMP ROVEMENT OF FEEDER ROUTING
ATTACHMENT IN WING/PYLON
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 203672D50692
MINOR
 None
NOTE
: As per EASA IR 21, a minor change is one that has no appreciable effect on the
mass, balance, structural strength, reliability, operational characteristics affecting the
airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
The G-route wiring looms 7701VB and 7702VB are fixed with plastic brackets and metallic clamps at
the first attachment point in the wing after each pylon in the LH and RH wings. Due to vibration, cracks
have been found to occur in the bracket and the metallic strap has been found to be missing. This can
cause chafing of the wiring loom on the aircraft structure.
This modification installs a new metallic bracket with electrical bonding, reinforced clamp and grommet
to replace the existing parts at the first attachment point in the wing after each inboard pylon in the LH
and RH wings.
Accomplishment of this Service Bulletin will improve the wiring installation in the wing/pylon area to
prevent chafing, possible short circuits and damage to systems. This will prevent potential system
misbehavior, improve reliability and avoid unscheduled maintenance action.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 MANDATORY (1)
 CANCELS INSPECTION SB
 NO
POTENTIAL AD
 YES
 A/C OPERATION AFFECTED
 NO
RELIABILITY AFFECTED
 YES
 PAX COMFORT AFFECTED
 NO
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A330
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
COST SAVING
 NO
 ETOPS AFFECTED
 NO
STRUCTURAL LIFE EXTN
 NO
 VENDOR SB INVOLVED
 NO
NOTE
 (1)
: Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit
 923132D01R03
 1
 892.00
 Grommets, Brackets and Attaching Parts
EFFECTIVITY
This Service Bulletin is applicable to this (these) operator(s) :
18P
 34Z
 38W 43P
 44W
 83V
 99Y AAR AAW ABD ACA ACI AEA
AFL AFR AIB 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 G8E
 GAP
GFA GIA GRL HAL HDA HFY HVN I2L IAW IBE JAI JST KAL
KLM LAA MAS MAU MEA MNB MON MSR NMB OBS
 OHY OMA ONE
PAL QAF QFA QTR RJA RSF RSY SAA SAI SAS SIA SVA SWR
TAE TAM TAP TCX THA THY TNA TOW TPA TSC UAE UAF USA
VIR VKG VOZ WRC XAX XLF
CONCURRENT REQUIREMENTS
None
REFERENCES / REPERCUSSIONS
TFU
 None
OEB
 None
AOT
 None
SIL
 None
ISI
 None
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 None
NATURE OF THE WORK
AIRCRAFT
 YES
EQUIPMENT
 NO
HARD
 NO
SOFT
 NO
OBRM
 NO
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@A330
SERVICE BULLETIN
SUMMARY
MANPOWER
Task 923132-831-848-001: Modification
TOTAL MANHOURS
 8.00
ELAPSED TIME (HOURS)
 4.00
APPENDICES
Appendix 01 - Elapsed Time Assumption
Appendix 02 - Post SB Installation Details
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
A
LH SHOWN
RH SIMILAR
B
RIB11A
B
NOTE:
AREA OF MODIFICATION
A
A
,  Z452 Z522
,  Z462 Z622
G_SB_923132_6_SAAA_01_00
Figure A-GSAAA - Sheet 01
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 4
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@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: 92
TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION-CABLE LOOM
INSTALLATION DRAWINGS-IMP ROVEMENT OF FEEDER ROUTING
ATTACHMENT IN WING/PYLON
MODIFICATION No.: 203672D50692
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
330-202 330-203 330-223 330-223F 330-243 330-243F 330-301 330-302
330-303 330-321 330-322 330-323 330-341 330-342 330-343
(2) Effectivity by MSN
0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0065
 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
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A330
SERVICE BULLETIN
0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522
0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558
0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588
0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618
0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650
0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688
0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718
0720-0722 0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747
0749-0752 0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782
0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811
0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863
0865-0869 0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901
0903-0909 0911 0913-0916 0918-0920 0922-0923 0925-0928 0930-0932 0934-0937
0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-0998
1000-1004
 1006-1016 1018-1023 1025-1026 1028-1029 1031-1039 1041-1049
1051-1055 1057-1063 1065-1067 1069-1078 1080-1082 1084-1090 1092-1101
1103-1108 1110 1112 1114-1116 1118 1120 1123-1124 1126-1127 1129-1133
1135-1138 1141 1143 1145-1151 1153 1155-1157 1159-1161 1163-1165 1167-1175
1177-1178 1180-1181 1183-1184 1186-1193 1195-1196 1198-1206 1208-1241
1243-1252 1254-1256 1258-1272 1274-1498
 1500-1504
 1506-1522
 1524-1532
(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
18P
 1321
34Z
 1483
 1491
38W
 0401
43P
 1053
44W
 0970
83V
 0353
 0362
99Y
 1439
AAR
 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340
1435 1464 1518
AAW
 1043 1472
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
 0345
 0437
 0451
 0871
ALK
 0303 0306 0311 0313 0404 0456 0627
ARA
 0891 0927
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A330
SERVICE BULLETIN
OPERATOR
 MSN
ARG
 0290 0300 0358 0364
ASY
 0747 0951 0969 1036 1183
AVA
 0948 0967 1009 1016 1073 1208 1224 1279 1342 1400 1492
 1508
AZA
 0272 0339 1123 1135 1218 1225 1252 1283 1308 1313 1327 1354
AZU
 0365
 0372
 0462
 0494
 0527
 0529
 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
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
CEB
 1420 1445 1495 1527
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
CHH
 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255 1325 1369
1438 1532
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
CRK
 1031 1034 1039 1042 1051 1054 1059 1062 1115 1175 1277 1286
1320 1322 1358 1384 1398
CRL
 0285 0320 1359 1376
CSA
 0425
CSC
 1082 1138 1241 1397 1432 1528
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
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 0330
 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 1032 1070
1071 1081 1167 1205 1226 1245 1414 1486 1521 1524
EVA
 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 1254
1268 1274
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A330
SERVICE BULLETIN
OPERATOR
 MSN
EVE
 0833
FIN
 0994 1007 1013 1023 1067 1078 1088 1173
FJI
 1394 1416 1465
FWI
 0253 0758 0965 1021 1265
G8E
 0184
 0189
 0191
GAP
 1463
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
GRL
 0230
HAL
 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404
1422 1469 1488 1496 1511 1530
HDA
 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405
0479 0512 0581 0669 0673 1457
HFY
 0096 0127 0211 0262 1008
HVN
 0275 0294 0299 0366 0943 0946 0962 1019 1256 1266
I2L
 0625
 0632
IAW
 1339
IBE
 1377 1385 1405 1426 1437 1490 1507 1515
JAI
 0923 0947 0956 1351 1361 1370 1391
JST
 0842 0853 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
 0116 1136 1148 1164 1180 1209 1219 1229 1234 1243 1281 1318
1336 1337 1347 1388 1395 1431 1470 1489
MAU
 0883 1057
MEA
 0926 0984 0995 0998
MNB
 1332
MON
 0261 0265
MSR
 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246
NMB
 1451 1466
OBS
 0802
OHY
 0072 0087 0098 0143
OMA
 1038 1044 1049 1063 1093 1120 1227
ONE
 1506
PAL
 0183 0188 0198 0200 0203 1449 1456
 1460 1467 1475 1482 1504
1510 1531
QAF
 0487 0605
QFA
 0506
 0508 0513
 0522
 0553 0558 0564 0574 0593 0595 0603 0695
0705 0712 0887 0892 0898 0940
 0976 1061 1094 1169 1174 1198
1251
 1258 1365
QTR
 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 1350 1386 1406
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 4
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 13

@A330
SERVICE BULLETIN
OPERATOR
 MSN
RJA
 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
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
TAE
 0348
TAM
 0232 0238 0247 0259 0361 0466 0472 0700 0968 1112 1118 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 0112 0122 0209 0224 0231 0346 0990
1003 1035 1037 1060 1074 1086 1090 1263 1269 1289 1338 1348
1374 1408
THY
 0463 0504 0697 0704 0742 0754 0774 0869 0874
 0876
 0882 0901
0932 0939
 0949
 0961
 0977
 1004 1092 1150 1160 1170 1172 1204
1212 1213
 1228 1240 1298 1307 1311 1344 1418 1442 1458 1476
1487 1501 1514 1522 1529
TNA
 1357 1378
TOW
 1033 1046 1248 1275 1312 1334 1363 1390 1419
 1498
TPA
 1368 1380 1428 1448
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
WRC
 0296
XAX
 0054 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066 1075
1126 1131 1165 1411 1423 1433 1481
XLF
 0501 0635 1360
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 5
6
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SERVICE BULLETIN
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064
0065 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
 0936
 0937
001
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 6
6
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SERVICE BULLETIN
MSN
 CONFIGURATION
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 1000 1001
1002 1003 1004 1006 1007 1008 1009 1010 1011 1012 1013
1014 1015 1016 1018 1019 1020 1021 1022 1023 1025 1026
1028 1029 1031 1032 1033 1034 1035 1036 1037 1038 1039
1041 1042 1043 1044 1045 1046 1047 1048 1049 1051 1052
1053 1054 1055 1057 1058 1059 1060 1061 1062 1063 1065
1066 1067 1069 1070 1071 1072 1073 1074 1075 1076 1077
1078 1080 1081 1082 1084 1085 1086 1087 1088 1089 1090
1092 1093 1094 1095 1096 1097 1098 1099 1100 1101 1103
1104 1105 1106 1107 1108 1110 1112 1114 1115 1116 1118
1120 1123 1124 1126 1127 1129 1130 1131 1132 1133 1135
1136 1137 1138 1141 1143 1145 1146 1147 1148 1149 1150
1151 1153 1155 1156 1157 1159 1160 1161 1163 1164 1165
1167 1168 1169 1170 1171 1172 1173 1174 1175 1177 1178
1180 1181 1183 1184 1186 1187 1188 1189 1190 1191 1192
1193 1195 1196 1198 1199 1200 1201 1202 1203 1204 1205
1206 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217
1218 1219 1220 1221 1222 1223 1224 1225 1226 1227 1228
1229 1230 1231 1232 1233 1234 1235 1236 1237 1238 1239
1240 1241 1243 1244 1245 1246 1247 1248 1249 1250 1251
1252 1254 1255 1256 1258 1259 1260 1261 1262 1263 1264
1265 1266 1267 1268 1269 1270 1271 1272 1274 1275 1276
1277 1278 1279 1280 1281 1282 1283 1284 1285 1286 1287
1288 1289 1290 1291 1292 1293 1294 1295 1296 1297 1298
1299 1300 1301 1302 1303 1304 1305 1306 1307 1308 1309
1310 1311 1312 1313 1314 1315 1316 1317 1318 1319 1320
1321 1322 1323 1324 1325 1326 1327 1328 1329 1330 1331
1332 1333 1334 1335 1336 1337 1338 1339 1340 1341 1342
1343 1344 1345 1346 1347 1348 1349 1350 1351 1352 1353
1354 1355 1356 1357 1358 1359 1360 1361 1362 1363 1364
1365 1366 1367 1368 1369 1370 1371 1372 1373 1374 1375
1376 1377 1378 1379 1380 1381 1382 1383 1384 1385 1386
1387 1388 1389 1390 1391 1392 1393 1394 1395 1396 1397
1398 1399 1400 1401 1402 1403 1404 1405 1406 1407 1408
1409 1410 1411 1412 1413 1414 1415 1416 1417 1418 1419
1420 1421 1422 1423 1424 1425 1426 1427 1428 1429 1430
1431 1432 1433 1434 1435 1436 1437 1438 1439 1440 1441
1442 1443 1444 1445 1446 1447 1448 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 1500 1501 1502 1503 1504 1506 1507 1508 1509
1510 1511 1512 1513 1514 1515 1516 1517 1518 1519 1520
1521 1522 1524 1525 1526 1527 1528 1529 1530 1531 1532
001
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 7
6
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SERVICE BULLETIN
(5) Configuration definition
**CONF 001
Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a
standard configuration.
(6) Material Effectivity
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit
 923132D01R03
 1
Consumable CMLD01
 1
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
The G-route wiring looms 7701VB and 7702VB are fixed with plastic brackets and
metallic clamps at the first attachment point in the wing after each pylon in the LH and
RH wings. Due to vibration, cracks have been found to occur in the bracket and the
metallic strap has been found to be missing. This can cause chafing of the wiring loom
on the aircraft structure.
(2) Objective/Action
This modification installs a new metallic bracket with electrical bonding, reinforced clamp
and grommet to replace the existing parts at the first attachment point in the wing after
each inboard pylon in the LH and RH wings.
(3) Advantages
Accomplishment of this Service Bulletin will improve the wiring installation in the
wing/pylon area to prevent chafing, possible short circuits and damage to systems. This
will prevent potential system mis behavior, improve reliab ility and avoid unscheduled
maintenance action.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
Task 923132-831-848-001: Modification
(1) Modify the Cable Loom Support Bracket of the G-route 7701VB LH
(2) Modify the Cable Loom Support Bracket of the G-route 7702VB RH
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 8
6
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SERVICE BULLETIN
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
This Service Bulletin must be accomplished before Oct 31/16.
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 date given
above 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.
Task 923132-831-848-001: Modification
Get Access
 2.00
On Aircraft
Modify the Cable Loom Support Bracket of the G-route
7701VB LH
2.00
Modify the Cable Loom Support Bracket of the G-route
7702VB RH
2.00
Close-Up
 2.00
TOTAL MANHOURS
 8.00
ELAPSED TIME (HOURS)
 4.00
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-GAAAA
 given in Appendix 01 - Elapsed Time Assumption .
H. WEIGHT AND BALANCE
Not Changed
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 9
6
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SERVICE BULLETIN
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
Aircraft Maintenance Manual (AMM)
 06-20-00 06-31-53 06-41-53
11-00-00 12-34-24 20-21-11
20-28-00 54-52-11 57-41-37
57-42-37
Elec. Std. Practices Manual (ESPM)
 20-33-00 20-33-11 20-33-30
20-33-41 20-51-20 20-51-22
20-55-00
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-21-00
 51-23-11
 51-40-00
51-42-00 51-44-00
K. PUBLICATION AFFECTED
Elec. Std. Practices Manual (ESPM)
 20-33-11 20-33-41
Illustrated Parts Catalog (IPC)
 57-26-05
L. INTERCHANGEABILITY/MIXABILITY
Not Applicable
M. SPARES
None
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 10
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SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Customers with aircraft shown in the effectivity of this Service Bulletin should send a
purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:
Kit
 923132D01R03
 AIRBUS Material, Logistics and Suppliers
Weg beim Jaeger 150
D-22335 HAMBURG
GERMANY
For ordering by internet:
http://spares.airbus.com
For ordering by fax: +49 40 50 76 2590
For ordering by E-mail; airbus.kit@airbus.com
(2) Price and Availability
Kit
 923132D01R03
Cost
 892.00 USD
Availability
 90 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
B. INDUSTRY SUPPORT INFORMATION
AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at
no charge for orders placed before Dec 31/17.
For aircraft under warranty at Jan 01/13, AIRBUS will credit the manhours indicated in this
Service Bulletin at the agreed in-house warranty labor rate for claims received not later than
90 days after completion of the last affected aircraft of your fleet.
C. LIST OF COMPONENTS
Kit 923132D01R03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
1
 MS21042L3
 4
 NUT
2
 NAS1149D0363H
 8
 WASHER
3
 F9249296220000
 2
 BRACKET
4
 ASNA0032-060
 2
 CLAMP
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 11
6
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SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
5
 NAS1801-3-12
 4
 SCREW
6
 ABS0678B02
 2
 SUPPORT
8
 NSA939510CN
 0.578
 STRIP
9
 F9239026810000
 PLCRDSET
 (1
)
11
 NSA935401-03
 2
 TIE
NOTE
: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
NOTE
 (1)
: This set contains Service Bulletin accomplishment placards for both LH and
RH wings.
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
Consumable CMLD01
ITEM
 DESCRIPTION
 REFERENCE TO CML
MAT. No.
QTY PER A/C
 SEE
NOTES
Varnish-- Electrical Bonding
Structure
04TMB2
 As required
Coating Sealant-Fuel Tank
Brushable
06HAA1
 As required
Non Aqueous Cleaner - Non
Structural Use
08BPA1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
(2) Components
None
(3) Equipment
None
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
None
F. TOOLING
None
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 12
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SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 923132-831-848-001 - Modification
WARNING
: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION
: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP
ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY
AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE
WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,
COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO
THIS:
- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS
NECESSARY ON WIRING AND COMPONENTS.
- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND
OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION
AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
"refer to" are used and the operator has a procedure accepted by the local
authority he belongs to, the accepted alternative procedure can be used. When the
words "in accordance with" are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. Other paragraphs are recommended and may be deviated
from, done as part of other actions or done with accepted methods different from
those given in the Service Bulletin, as long as the RC paragraphs can be done and
the aircraft can be put back into a serviceable condition.
Task Associated Data
Zone
452 462 522 622
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 13
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SERVICE BULLETIN
Manpower
TOTAL MANHOURS
 8.00
ELAPSED TIME (HOURS)
 4.00
A. GENERAL
(1) Subtask 923132-910-201-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
11-00-00, Page Block 201
Task 20-21-11-911-801
Task 20-28-00-912-802
Elec. Std. Practices Manual (ESPM)
 20-33-00
20-51-20
Structural Repair Manual (SRM)
 51-21-00
51-23-11
51-40-00
51-42-00
51-44-00
(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.
(d) Remove and install fasteners in accordance with SRM 51-42-00.
(e) To torque tighten the standard threaded fasteners, refer to AMM Task
20-21-11-911-801.
(f) If alternative and substitute fasteners have to be used, you must make sure that the
associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’
column.
(g) If the length of any fastener specified in this Service Bulletin does not meet
installation standards given in SRM Chapter 51, then a fastener of the same
specification, or an approved substitute, with a length which meets the installation
standards given in SRM Chapter 51 may be used. In addition, washers may be
installed for fastener grip length in accordance with SRM Chapter 51.
(h) For the general installation of elec trical harnesses, refer to ESPM 20-33-00.
(i) For the electrical bonding, re fer to ESPM 20-51-20 and AMM Task
20-28-00-912-802.
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 14
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SERVICE BULLETIN
(j) For the installation of placards, refer to AMM 11-00-00, Page Block 201.
(k) Apply protective treatment in accordance with SRM 51-21-00.
(l) Apply paint coatings in accordance with SRM 51-23-11.
(m) Obtain fastener hole diameters and drill and de-burr data in accordance with SRM
51-44-00.
(2) Subtask 923132-839-201-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
B. PREPARATION
(1) Subtask 923132-941-201-001 - Job Set-up
Work Zones and Access Panels
Zone
 Access/Work location
452
462
522
622
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 54-52-11-000-809
Task 57-41-37-000-801
Task 57-42-37-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 15
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SERVICE BULLETIN
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) To get access for the LH Wing:
1
 Remove the fixed leading edge access panels 522AB and 522BB, refer to
AMM Task 57-41-37-000-801 and AMM Task 57-42-37-000-801.
2
 Remove the pylon access panels 452CL and 452CR, refer to AMM Task
54-52-11-000-809.
(c) To get access for the RH Wing:
1
 Remove the fixed leading edge access panels 622AB and 622BB, refer to
AMM Task 57-41-37-000-801 and AMM Task 57-42-37-000-801.
2
 Remove the pylon access panels 462CL and 462CR, refer to AMM Task
54-52-11-000-809.
C. PROCEDURE
(1) Subtask 923132-831-201- 001 - Modify the Cable Loom Support Bracket of the G-
route 7701VB LH
Work Zones and Access Panels
Zone
 Access/Work location
452
462
522
622
Manpower Resources
Manhours
 2.00
Minimum number of person
 1
Subtask elapsed time
 2.00
Skills
 AIRFRAME
Material necessary to do the job
Kit 923132D01R03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
1
 MS21042L3
 2
 NUT
2
 NAS1149D0363H
 4
 WASHER
3
 F9249296220000
 1
 BRACKET
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 16
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 25

@A330
SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
4
 ASNA0032-060
 1
 CLAMP
5
 NAS1801-3-12
 2
 SCREW
6
 ABS0678B02
 1
 SUPPORT
8
 NSA939510CN
 0.29
 STRIP
9
 F9239026810000
 1
 PLCRDSET
 (1
)
11
 NSA935401-03
 1
 TIE
NOTE
 (1)
: This set contains Service Bulletin accomplishment placards for both LH
and RH wings.
Consumable CMLD01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Varnish-- Electrical Bonding
Structure
04TMB2
 As required
Coating Sealant-Fuel Tank
Brushable
06HAA1
 As required
Non Aqueous Cleaner -
Non Structural Use
08BPA1
Textile-Lint Free Cotton
 14SBA1
 As required
References
Aircraft Maintenance Manual (AMM)
 11-00-00, Page Block 001
Task 20-28-00-912-802
Elec. Std. Practices Manual (ESPM)
 20-33-11
20-33-41
20-51-22
Structural Repair Manual (SRM)
 51-44-00
Fig. A-GBAAA
Modification of the Cable Loom Support
Bracket, LH and RH
Sheet 01
Sheet 02
(a) At the attachment point in the LH wing after the pylon, remove the support bracket
from the wiring loom 7701VB, Item (7), refer to Fig. A-GBAAA Sheet 01
 ,V i e wC :
2 Nut MS21042L3 Item (1) Discard
2 Screw NAS1096-3-8 Item (5) Discard
4 Washer NAS1149D0316H Item (2) Discard
1 Bracket ABS0679-01 Item (3) Discard
1 Clamp ASNA0033-060 Item (4) Discard
1 Tie-Cable NSA935401-03 Item (11) Discard
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 17
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 26

@A330
SERVICE BULLETIN
2 Support ABS0678B01 Item (6) Discard
NOTE
: Item (6) is removed as 2 parts.
(b) At the bracket attachment point in the LH wing after the pylon, clean the bonding
point contact surface, refer to Fig. A-GBAAA Sheet 01
 ,V i e wD ,w i t h :
Textile-Lint Free
Cotton
14SBA1 As required
and
Non Aqueous
Cleaner - Non
Structural Use
08BPA1
 As required
(c) If necessary, rework the holes in the bracket, Item 3 in accordance with SRM
51-44-00 and refer to Fig. A-GBAAA Sheet 01
 and Fig. A-GBAAA Sheet 02
 ,V i e w
D, View E and View F.
NOTE
: If holes are reworked apply protective treatment as necessary.
(d) Install the new cable loom support bracket and fasteners, refer to Fig. A-GBAAA
Sheet 01
 and Fig. A-GBAAA Sheet 02
 ,V i e wD ,V i e wEa n dV i e wF :
1 Bracket F9249296220000 Item 3
2 Screw NAS1801-3-12 Item 5
4 Washer NAS1149D0363H Item 2
2 Nut MS21042L3 Item 1
NOTE
: The bracket, Item 3, is installed inside the wing, refer to Appendix
02 - Post SB Installation Details
 .
(e) Apply a layer of:
Coating Sealant-
Fuel Tank
Brushable
06HAA1 As required
and
Varnish-- Electrical
Bonding Structure
04TMB2 As required
over the nut, Item 1, in accordance w ith ESPM 20-51- 22 and refer to AMM Task
20-28-00-912-802.
(f) Install, refer to ESPM 20-33-11
 and Fig. A-GBAAA Sheet 01
 ,V i e wD :
0.289
 Grommet NSA939510CN Item 8
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 18
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 27

@A330
SERVICE BULLETIN
(g) Install the wiring loom 7701VB, Item ( 7), refer to ESPM 20-33-11, ESPM 20-33-41
and Fig. A-GBAAA Sheet 01
 , View D, on:
1 Support ABS0678B02 Item 6
Attach the E-route cables, Item (10), to the support, Item 6, with:
1 Tie-Cable NSA935401-03 Item 11
On the new bracket, Item 3, install:
1 Clamp ASNA0032-060 Item 4
(h) Install, refer to AMM 11-00-00, Page Block 001 and Fig. A-GBAAA Sheet 01
 ,V i e w
D:
1 Placard F9239026810000 Item 9
(2) Subtask 923132-831-202- 001 - Modify the Cable Loom Support Bracket of the G-
route 7702VB RH
Work Zones and Access Panels
Zone
 Access/Work location
452
462
522
622
Manpower Resources
Manhours
 2.00
Minimum number of person
 1
Subtask elapsed time
 2.00
Skills
 AIRFRAME
Material necessary to do the job
Kit 923132D01R03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
1
 MS21042L3
 2
 NUT
2
 NAS1149D0363H
 4
 WASHER
3
 F9249296220000
 1
 BRACKET
4
 ASNA0032-060
 1
 CLAMP
5
 NAS1801-3-12
 2
 SCREW
6
 ABS0678B02
 1
 SUPPORT
8
 NSA939510CN
 0.29
 STRIP
9
 F9239026810000
 1
 PLCRDSET
 (1
)
11
 NSA935401-03
 1
 TIE
NOTE
 (1)
: This set contains Service Bulletin accomplishment placards for both LH
and RH wings.
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 19
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 28

@A330
SERVICE BULLETIN
Consumable CMLD01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Varnish-- Electrical Bonding
Structure
04TMB2
 As required
Coating Sealant-Fuel Tank
Brushable
06HAA1
 As required
Non Aqueous Cleaner -
Non Structural Use
08BPA1
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Aircraft Maintenance Manual (AMM)
 11-00-00, Page Block 001
Task 20-28-00-912-802
Elec. Std. Practices Manual (ESPM)
 20-33-11
20-33-30
20-33-41
20-51-22
Structural Repair Manual (SRM)
 51-44-00
Fig. A-GBAAA
Modification of the Cable Loom Support
Bracket, LH and RH
Sheet 01
Sheet 02
(a) At the attachment point in the RH wing after the pylon, remove the support bracket
from the wiring loom 7702VB, Item (7), refer to Fig. A-GBAAA Sheet 01
 ,V i e wC :
2 Nut MS21042L3 Item (1) Discard
2 Screw NAS1096-3-8 Item (5) Discard
4 Washer NAS1149D0316H Item (2) Discard
1 Bracket ABS0679-01 Item (3) Discard
1 Clamp ASNA0033-060 Item (4) Discard
1 Tie-Cable NSA935401-03 Item (11) Discard
2 Support ABS0678B01 Item (6) Discard
NOTE
: Item (6) is removed as 2 parts.
(b) At the bracket attachment point in the RH wing after the pylon, clean the bonding
point contact surface, refer to Fig. A-GBAAA Sheet 01
 ,V i e wD ,w i t h :
Textile-Lint Free
Cotton
14SBA1 As required
and
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 20
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 29

@A330
SERVICE BULLETIN
Non Aqueous
Cleaner - Non
Structural Use
08BPA1
 As required
(c) If necessary, rework the holes in the bracket, Item 3 in accordance with SRM
51-44-00 and refer to Fig. A-GBAAA Sheet 01
 and Fig. A-GBAAA Sheet 02
 ,V i e w
D and View E.
NOTE
: If holes are reworked apply protective treatment as necessary.
(d) Install the new cable loom support bracket and fasteners, refer to Fig. A-GBAAA
Sheet 01
 and Fig. A-GBAAA Sheet 02
 ,V i e wD ,V i e wEa n dV i e wF :
1 Bracket F9249296220000 Item 3
2 Screw NAS1801-3-12 Item 5
4 Washer NAS1149D0363H Item 2
2 Nut MS21042L3 Item 1
NOTE
: The bracket, Item 3, is installed inside the wing, refer to Appendix
02 - Post SB Installation Details
 .
(e) Apply a layer of:
Coating Sealant-
Fuel Tank
Brushable
06HAA1 As required
and
Varnish-- Electrical
Bonding Structure
04TMB2 As required
over the nut, Item 1, in accordance w ith ESPM 20-51- 22 and refer to AMM Task
20-28-00-912-802.
(f) Install, refer to ESPM 20-33-11 and
 Fig. A-GBAAA Sheet 01
 ,V i e wD :
0.289
 Grommet NSA939510CN Item 8
Refer to ESPM 20-33-30.
(g) Install the wiring loom 7702VB, Item ( 7), refer to ESPM 20-33-11, ESPM 20-33-41
and Fig. A-GBAAA Sheet 01
 , View D, on:
1 Support ABS0678B02 Item 6
Attach the E-route cables, Item (10), to the support, Item 6, with:
1 Tie-Cable NSA935401-03 Item 11
On the new bracket, Item 3, install:
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 21
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 30

@A330
SERVICE BULLETIN
1 Clamp ASNA0032-060 Item 4
(h) Install, refer to AMM 11-00-00, Page Block 001 and Fig. A-GBAAA Sheet 01
 ,V i e w
D:
1 Placard F9239026810000 Item 9
D. TEST
None
E. CLOSE-UP
(1) Subtask 923132-942-201-001 - Close-up
Work Zones and Access Panels
Zone
 Access/Work location
452
462
522
622
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 54-52-11-400-809
Task 57-41-37-400-801
Task 57-42-37-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Install the access panels for the LH wing:
1
 Install the fixed leading edge access panels 522AB and 522BB, refer to AMM
Task 57-41-37-400-801 and AMM Task 57-42-37-400-801.
2
 Install the pylon access panels 452CL and 452CR, refer to AMM Task
54-52-11-400-809.
(c) Install the access panels for the RH wing:
1
 Install the fixed leading edge access panels 622AB and 622BB, refer to AMM
Task 57-41-37-400-801 and AMM Task 57-42-37-400-801.
2
 Install the pylon access panels 462CL and 462CR, refer to AMM Task
54-52-11-400-809.
(d) Put the aircraft back to its original configuration.
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 22
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 31

@A330
SERVICE BULLETIN
**CONF ALL
A
LH SHOWN
RH SIMILAR
B
RIB11A
A
A
,  Z452 Z522
,  Z462 Z622
SB92−3132
E
(5)
(2)
(4)
(6)
(1)
(2)
(3)
C
AFTER
7701VB
9
(7)
D
4
6
1
2
3
8
5
2
(11)
11
(10)
(7702VB)
C D
B
BEFORE
(7)
(10)
VIEW FROM OUTSIDE
THE WING
VIEW FROM OUTSIDE
THE WING
VIEW FROM INSIDE
THE WING
7701VB
(7702VB)
G_SB_923132_6_BAAA_01_04
Figure A-GBAAA - Sheet 01
Modification of the Cable Loom Support Bracket, LH and RH
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 23
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 32

@A330
SERVICE BULLETIN
**CONF ALL
0101
30 mm (1.81 in) ± 0.1 mm (0.0039 in)
FOR THE INSTALLATION OF BRACKET ITEM 3, THE HOLES CAN
NOTE:
01
BE REWORKED ECCENTRICALLY TO A MAXIMUM OF 1 mm (0.039 in)
3
TO GET AN INCREASED HOLE PITCH OF 31 mm (1.220 in).
HOLES OF THE BRACKET ENLARGED TO A MAXIMUM OF 1 mm (0.039 in).02
INITIAL HOLES OF THE BRACKET BEFORE REWORK.03
HOLES ON THE WING SUPPORT.04
02 04
30 mm (1.181 in) DISTANCE BETWEEN 
THE HOLES ON THE BRACKET
UP TO 31.4 mm (1.236 in) − 31.7 mm (1.248 in) DISTANCE
BETWEEN THE HOLES ON THE WING SUPPORT
F
E
02
F
03
03
04
G_SB_923132_6_BAAA_02_03
Figure A-GBAAA - Sheet 02
Modification of the Cable Loom Support Bracket, LH and RH
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 24
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 33

@A330
SERVICE BULLETIN
Appendix 01 - Elapsed Time Assumption
**CONF ALL
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A330−92−3132 0102
MH
ET/S:
PER
MANHOURS
ELAPSED TIME PER STEP
NUMBER OF PERSONS
THIS CHART IS ONLY A PROPOSAL.
OPERATORS MAY DETERMINE THAT ANOTHER WAY
TO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
:
: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS
ARE NOT REFLECTED IN THIS GANTT CHART.
TOTAL MANHOURS
SB ELAPSED TIME
8.00
4.00
0 12 3
JOB SET−UP
MH ET/SSTEPS
2.00 1.00
MODIFY THE LH CABLE LOOM 2.00 2.00
2.00 2.00
PER
2
1
1
CLOSE−UP 2.00 1.002
SB ELAPSED TIME
(HOURS)
4
SUPPORT BRACKET OF THE
G ROUTE 7701VB LH
MODIFY THE RH CABLE LOOM
SUPPORT BRACKET OF THE
G ROUTE 7702VB RH
G_SB_923132_6_AAAA_01_04
Figure A-GAAAA - Sheet 01
Gantt Chart
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 34

@A330
SERVICE BULLETIN
Appendix 01 - Elapsed Time Assumption
This Page Intentionally Left Blank
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 35

@A330
SERVICE BULLETIN
Appendix 02 - Post SB Installation Details
**CONF ALL
(1) The following photographs illustrate the correct installation.
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 36

@A330
SERVICE BULLETIN
Appendix 02 - Post SB Installation Details
**CONF ALL
FRONT VIEW (OUTSIDE)
FRONT VIEW (OUTSIDE)
G_SB_923132_6_ABAA_01_00
Figure A-GABAA - Sheet 01
Post SB Installation Details
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 2
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 37

@A330
SERVICE BULLETIN
Appendix 02 - Post SB Installation Details
**CONF ALL
VIEW FOR THE POSITION OF THE CLAMP, ITEM 4
VIEW IN THE WING (INSIDE)
GROMMET,
ITEM 8
BRACKET,
ITEM 3
G_SB_923132_6_ABAA_02_00
Figure A-GABAA - Sheet 02
Post SB Installation Details
DATE: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 3
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 38

@A330
SERVICE BULLETIN
REPORTING SHEET
TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION-CABLE LOOM
INSTALLATION DRAWINGS-IMP ROVEMENT OF FEEDER ROUTING
ATTACHMENT IN WING/PYLON
MODIFICATION No.: 203672D50692
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: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 39

@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: Jun 19/14 SERVICE BULLETIN No.: A330-92-3132
REVISION No.: 01 - May 21/15 Page: 1
6
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

---
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