# Airbus Service Bulletin A330-28-3130

Copy: No revision named ("SB A330-28-3130 R00"), 46 pages: PDF https://openairdocs.org/files/sha256/22/ec/22ecce12424e549433ee0f2a8f763b68a945804ea19e029e83327d2d7afa34cf; text https://openairdocs.org/service-documents/airbus/a330-28-3130/file/22ecce12424e.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0270; AD 2018-14-04 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: A330-28-3130
- Page: https://openairdocs.org/service-documents/airbus/a330-28-3130

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

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

- [AD 2018-14-04](https://openairdocs.org/ad/2018-14-04.md), effective Aug 13, 2018: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-28-3130/proposed.md).

## Text (46 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0270; AD 2018-14-04 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: 28
TITLE: FUEL - TANKS - INSPECTION OF TRIM TANK OVERFLOW
**CONF ALL
MODIFICATIONS
None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
While performing an assessment of Long Range (LR) family aircraft Ground Test Requirements (GTR),
it has been determined that the ’Production Test to Verify Tank Pressures during Refuel Overflow’ is not
performed on the trim tank.
The aim of this Inspection Service Bulletin (ISB) is to perform a trim tank overflow ground test and to
check that trim tank pressure values and trim surge tank pressure values are not exceeded.
Accomplishment of this Service Bulletin will ensure that there is no blockage of the vent pipes.
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
DE-FUELLING/VENTILATION
 YES
 VALIDATION ON AIRCRAFT
 YES
BOOKLET AVAILABLE
 YES
NOTE
 (1)
: Service Bulletin must be accomplished.
NOTE
: This Service Bulletin has been accomplished before delivery on aircraft with
Manufacturer Serial Number (MSN) 1176 to validate its content.
NOTE
: A booklet including photographs taken during the validation of this Service Bulletin is
available on AIRBUS|World - Maintenance and Engineering - AirN@v engineering (in
the concerned SB file).
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A330
SERVICE BULLETIN
SUMMARY
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit tool 283130T01R00
 1
 See SB
 Overflow pipe tool and pressure
transducer tool
EFFECTIVITY
This Service Bulletin is applicable to this (these) operator(s) :
18P 34N 38W 41N 43P 56O 78U 83V 96U 98W AAL AAR AAW
ACA ACI AEA AFL AFR AIB ALD ALK ARA ARG ASL ASY AVA
AZA AZU BEC BEL BER BGH CAL CBJ CCA CEB CES CHH CPA
CRK CRL CSA CSC CSN DAH DAL DGA DLH EDW EIN ETD EVA
EVE F2I FIN FJI FWI GCR GFA GIA GRL HAL HDA HFY HKC
HVN IAW IBE IRA JAI JAV KAC KAL KLM LAA LNI MAS MAU
MEA MLM MNB MOV MSR NMB OBS OHY OMA ONE PAL PLM QAF
QFA QTR RJA RSF RSY RZO SAA SAF SAI SAS SEY SIA SVA
SWR SXD TAE TAM TAP TAR TCX THA THY TNA TOW TPA TSC
U6A UAE UAF VIR VKG VOZ WOW WRC XAX XLF
CONCURRENT REQUIREMENTS
None
REFERENCES / REPERCUSSIONS
TFU
 28.12.00.008
OEB
 None
AOT
 None
SIL
 None
ISI
 00.00.00198
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 None
NATURE OF THE WORK
AIRCRAFT
 YES
EQUIPMENT
 NO
HARD
 NO
SOFT
 NO
OBRM
 NO
MANPOWER
Task 283130-832-895-001: Special Detailed Inspection of the Trim Tank Overflow
TOTAL MANHOURS
 17.50
ELAPSED TIME (HOURS)
 5.25
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
SUMMARY
APPENDICES
Appendix 01 - Manpower Gantt Chart
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
B
A
VIEW LOOKING UP
FWD
VENT SYSTEM
TO BE INSPECTED
Z343
Z333
Z319
A
RIB3
LH INNER
VENT VALVE 
RH INNER
VENT VALVE 
RH OUTER
VENT VALVE 
MAIN VENT
PIPE OUTLET
RIB2
RIB3
B
705QN
LOCATION OF THE INLET
VALVE ACTUATOR
RIB3
MAIN VENT PIPE
SECONDARY VENT PIPE
VENT PIPE OUTLET
SURGE
SECONDARY
TANK
LH OUTER
VENT VALVE 
MAIN VENT
PIPE INLETS
G_SB_283130_7_SAAA_01_02
Figure A-USAAA - Sheet 01
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 4
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
FR40 FR47
FR46
FR47
Z140A
A
B
B
700QN2
700QN1
701QN
THE VALVE ACTUATORS
LOCATION OF
G_SB_283130_7_SBAA_01_01
Figure A-USBAA - Sheet 01
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 5
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A330
SERVICE BULLETIN
SUMMARY
This Page Intentionally Left Blank
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 6
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@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: 28
TITLE: FUEL - TANKS - INSPECTION OF TRIM TANK OVERFLOW
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
330-202 330-203 330-223 330-223F 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 0042 0045 0050 0054-0055 0060 0062 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 0195 0200 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 0295-0296 0300-0301
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 0591 0593 0595 0597 0600 0602-0603 0605 0607
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A330
SERVICE BULLETIN
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 1274-1521
1523-1651 1653-1660 1662-1681 1684-1701 1703-1704 1706 1708-1711
(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
34N
 0518 0536
38W
 0401
41N
 1676
43P
 1053
56O
 0116 0127
78U
 0314 0455
83V
 0171
96U
 0396
98W
 0054
AAL
 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041
1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526
AAR
 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340
1435 1464 1518
AAW
 1043 1472 1535
ACA
 0277 0279 0284 0344 0400 0408 0412 0419
ACI
 0507 0510
AEA
 0461 0505 0526 0551 0597 0733 0745 0749 0814 0931 0950 0992
1097 1574
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
 0042 0871
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A330
SERVICE BULLETIN
OPERATOR
 MSN
ALD
 0326 0328 0392
ALK
 0303 0306 0311 0313 0456 0627 1008 1564 1583 1604 1650 1669
1687 1689
ARA
 0891 0927
ARG
 0290 0300 0358 0364 0587 0634 1605 1623
ASL
 0885
ASY
 0747 0892 0898 0951 0969 1036 1183
AVA
 1009 1016 1073 1208 1224 1279 1342 1400 1492
AZA
 0272 0339 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313
1327 1354
AZU
 0462 0494 0527 0529 0532
BEC
 0863
BEL
 0030 0037 0045 0082 0095 0229 0249 0291 0324 1085
BER
 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 0739 0802
0822 0828 0911 0968 1112
BGH
 0255
CAL
 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769
0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450 1539
CBJ
 0988 1020 1028 1052
CCA
 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873
0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187
1199 1216 1237 1260 1282 1304 1330 1333 1353 1373 1383 1396
1413 1434 1444 1459 1471 1493 1509 1525 1538 1541 1563 1570
1587 1658 1673 1685 1695
CEB
 1420 1445 1495 1527 1552 1602
CES
 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830
0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291
1303 1324 1331 1372 1375 1402 1421 1429 1440 1461 1468 1479
1484 1500 1520 1537 1547 1551 1569 1588 1595 1603 1617 1632
1639 1655 1664
CHH
 0875 0881 0906 0982 1159 1168 1178 1190 1255 1325 1438 1532
1558 1573 1591 1614 1634 1656 1663 1677 1686 1703
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 1567
1618 1621
CRK
 1031 1034 1039 1042 1051 1054 1059 1062 1099 1105 1107 1115
1124 1146 1157 1175 1277 1286 1322 1358 1369 1384 1398 1668
CRL
 0285 0320 1359 1376
CSA
 0425
CSC
 1082 1138 1241 1397 1432 1528 1579 1662
CSN
 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954
0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 1335
1392 1425 1430 1494 1519 1536 1575 1593 1625 1636 1645 1699
DAH
 0644 0647 0650 0653 0667 1613 1630 1649
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A330
SERVICE BULLETIN
OPERATOR
 MSN
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 1627 1628 1637 1679
1701
DGA
 0240
DLH
 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905
0913 0922 0989 1292 1305 1314 1497
EDW
 1193 1711
EIN
 0269 0330 0397 0841 0847 0985 1025 1106
ETD
 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852
0854 0868 0975 0991 1032 1070 1071 1081 1167 1205 1226 1245
1414 1486 1521 1524
EVA
 0661 0678 0693 0755 1254 1268 1274 1684 1690
EVE
 0670 1691
F2I
 0070 0072 0087 0200
FIN
 0994 1007 1013 1023 1067 1078 1088 1173
FJI
 1394 1416 1465 1692
FWI
 0253 0343 0758 0965 1021 1265
GCR
 0919
GFA
 0276 0281 0286 0287 0334 0340
GIA
 0138 0140 0144 0148 0153 0165 1184 1214 1261 1288 1364 1410
1446 1474 1548 1560 1577 1585 1654 1671 1698 1709
GRL
 0230
HAL
 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404
1422 1469 1488 1496 1511 1530 1565 1606 1615 1672
HDA
 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405
0479 0512 0581 0669 0673 1457 1503 1523 1545 1557 1598
HFY
 0211 0262
HKC
 1320
HVN
 0275 0366 0943 0946 0962 1019 1256 1266
IAW
 1339
IBE
 1377 1385 1405 1426 1437 1490 1507 1515 1694 1700 1710
IRA
 1540 1586
JAI
 0888 0923 0947 0956 1351 1361 1370 1391
JAV
 0409
KAC
 1626 1643 1653 1678 1681
KAL
 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350
0351 0368 0428 0484 0490 0550 1133 1155 1200 1203 1393 1556
1576 1590 1611 1638 1647
KLM
 0682 0686 0703 0738 0770 0801 0925 1161 1287 1294 1300 1381
1580
LAA
 1412 1424 1505 1543
LNI
 1675 1680 1693
MAS
 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
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 4
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A330
SERVICE BULLETIN
OPERATOR
 MSN
MLM
 0451
MNB
 1332
MOV
 0535 0655
MSR
 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246
NMB
 1451 1466
OBS
 0833
OHY
 0098 0143 0316 0345 0353 0362 0404 0437 0625 0632
OMA
 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599
ONE
 1506 1508 1608 1657
PAL
 1449 1456 1460 1463 1467 1475 1482 1504 1510 1531 1546 1553
1559 1566 1568
PLM
 0261 0265
QAF
 0487 0605
QFA
 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695
0705 0712 0842 0853 0887 0940 0945 0976 1061 1094 1169 1174
1198 1251 1258 1365
QTR
 0441 0473 0489 0511 0521 0571 0623 0637 0638 0659 0680 0711
0721 0734 0743 0746 0760 0789 0792 0813 0820 0826 0849 0893
0907 0918 1350 1386 1406 1578 1584 1594 1688 1708
RJA
 0979 1002
RSF
 0980 0996 1235 1379 1478 1516
RSY
 0096 0120 0283 0295
RZO
 0970
SAA
 1191 1210 1223 1236 1249 1271
SAF
 1667
SAI
 0055 0086 0811 0819 0834 0900
SAS
 0496 0497 0515 0568 1660 1665 1697
SEY
 0751 0807
SIA
 0978 0983 0986 1010 1012 1015 1132 1149 1156 1382 1401 1427
1447 1453 1477 1485 1517 1544 1562 1597 1609 1633 1648 1666
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
SXD
 0530 0555 0573 0612 0616 0684
TAE
 0348
TAM
 0232 0238 0247 0259 0361 0466 0472 0700
TAP
 0181 0195 0223 0305 0308 0312 0317 0365 0372 0477 0486 0877
0899 0904 0914 0934 0997 1006
TAR
 1631 1641
TCX
 0254 0266 0301 0398 0948 0967
THA
 0050 0060 0062 0112 0122 0209 0231 0346 0990 1003 1035 1037
1060 1074 1086 1090 1263 1269 1289 1338 1348 1374 1408
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 5
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A330
SERVICE BULLETIN
OPERATOR
 MSN
THY
 0463 0504 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901
0932 0939 0949 0961 0977 1004 1092 1118 1150 1160 1170 1172
1204 1212 1213 1221 1228 1240 1298 1307 1311 1344 1418 1442
1458 1476 1483 1487 1491 1499 1501 1514 1529 1542 1550 1554
1571 1592 1616 1620 1622 1629 1635 1640 1642 1644 1651 1696
1704 1706
TNA
 1357 1378
TOW
 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498 1555
1601 1610
TPA
 1368 1380 1428 1448 1534
TSC
 0111 0132 0177 0248 0250 0251 0271 0369 0407 0427 0480 0795
0966 0971
U6A
 0065 0224
UAE
 0293 0382 0384 0452 0491 0509 0525
UAF
 1080 1186 1250
VIR
 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352
VKG
 0309 0349 0356 0357
VOZ
 1293 1306 1319 1407 1452 1561
WOW
 1098 1607 1624
WRC
 0296
XAX
 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066 1075 1126
1131 1165 1411 1423 1433 1481 1533 1549 1581 1589 1596 1600
1612 1619 1646 1659 1670 1674
XLF
 0501 0635 1360
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 6
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 13

@A330
SERVICE BULLETIN
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0042 0045 0050 0054 0055 0060 0062
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 0195 0200 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 0295 0296 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 0939 0940 0941 0942 0943 0944 0945 0946 0947
001
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 7
7
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SERVICE BULLETIN
MSN
 CONFIGURATION
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 1499 1500 1501 1502 1503 1504 1505
1506 1507 1508 1509 1510 1511 1512 1513 1514 1515 1516
1517 1518 1519 1520 1521 1523 1524 1525 1526 1527 1528
1529 1530 1531 1532 1533 1534 1535 1536 1537 1538 1539
1540 1541 1542 1543 1544 1545 1546 1547 1548 1549 1550
1551 1552 1553 1554 1555 1556 1557 1558 1559 1560 1561
001
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 8
7
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SERVICE BULLETIN
MSN
 CONFIGURATION
1562 1563 1564 1565 1566 1567 1568 1569 1570 1571 1572
1573 1574 1575 1576 1577 1578 1579 1580 1581 1582 1583
1584 1585 1586 1587 1588 1589 1590 1591 1592 1593 1594
1595 1596 1597 1598 1599 1600 1601 1602 1603 1604 1605
1606 1607 1608 1609 1610 1611 1612 1613 1614 1615 1616
1617 1618 1619 1620 1621 1622 1623 1624 1625 1626 1627
1628 1629 1630 1631 1632 1633 1634 1635 1636 1637 1638
1639 1640 1641 1642 1643 1644 1645 1646 1647 1648 1649
1650 1651 1653 1654 1655 1656 1657 1658 1659 1660 1662
1663 1664 1665 1666 1667 1668 1669 1670 1671 1672 1673
1674 1675 1676 1677 1678 1679 1680 1681 1684 1685 1686
1687 1688 1689 1690 1691 1692 1693 1694 1695 1696 1697
1698 1699 1700 1701 1703 1704 1706 1708 1709 1710 1711
001
(5) Configuration definition
**CONF 001
Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a
standard configuration.
(6) Material Effectivity
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit tool 283130T01R00
 1
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
While performing an assessment of Long Range (LR) family aircraft Ground Test
Requirements (GTR), it has been determined that the ’Production Test to Verify Tank
Pressures during Refuel Overflow’ is not performed on the trim tank.
(2) Objective/Action
The aim of this Inspection Service Bulletin (ISB) is to perform a trim tank overflow
ground test and to check that trim tank pressure values and trim surge tank pressure
values are not exceeded.
(3) Advantages
Accomplishment of this Service Bulletin will ensure that there is no blockage of the vent
pipes.
(4) Operational/Maintenance Consequences
None
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 9
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SERVICE BULLETIN
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
Task 283130-832-895-001: Special Detailed Inspection of the Trim Tank Overflow
(1) Install the Overflow Pipe Tool and the Pressure Transducer Tool for the Trim Surge
Tank
(2) Install the Pressure Transducer Tool for the Trim Tank
(3) Do the Trim Tank Overflow Ground Test
(4) Depending on the Inspection Results, do a Detailed Inspection of the NACA Duct
(5) Remove the Overflow Pipe Tool and the Pressure Transducer Tool for the Trim
Surge Tank
(6) Remove the Pressure Transducer Tool for the Trim Tank
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness
Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued
to confirm this classification. It is anticipated that the AD will confirm the thresholds
given but reference should be made to the AD for confirmation of the mandated
accomplishment timescale.
Table 1, Config. 001 - Do a Special Detailed Inspection of the Trim Tank Overflow
Condition
 Action
 Compliance time
 Repetitive interval
All aircraft
 Do a special detailed
inspection of the trim
tank overflow in
accordance with TASK
283130-832-895 001
42 months from ISB
issuance date
None
Trim tank pressure
values exceeded
Contact AIRBUS and
follow their instructions
Before next flight
 None
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 10
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SERVICE BULLETIN
Table 1, Config. 001 - Do a Special Detailed Inspection of the Trim Tank Overflow
Condition
 Action
 Compliance time
 Repetitive interval
Remove the overflow
pipe tool and the
pressure transducer
tools, in accordance
with SUBTASK
283130-080-401 001 for
the trim tank and
SUBTASK
283130-080-402 001 for
the trim surge tank
Before next flight
 None
AND
Trim tank pressure
values not exceeded,
and trim surge tank
pressure values not
exceeded
No further action
 None
 None
Remove the overflow
pipe tool and the
pressure transducer
tool, in accordance with
SUBTASK
283130-080-402 001 for
the trim surge tank
Before next flight
 None
AND
Trim tank pressure
values not exceeded,
and trim surge tank
pressure values
exceeded
Do a detailed inspection
of the NACA duct in
accordance with
SUBTASK
283130-832-404 001
Before next flight
 None
Remove the blockage or
do the applicable repair
procedure in
accordance with
SUBTASK
283130-832-404 001
Before next flight
 None
AND
Install the overflow pipe
tool and the pressure
transducer tool in
accordance with
SUBTASK
283130-480-401 001 for
the trim surge tank
Before next flight
 None
AND
NACA duct found
blocked or damaged
Repeat the trim tank
overflow ground test in
accordance with
SUBTASK
283130-832-402 001
Before next flight
 None
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 11
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SERVICE BULLETIN
Table 1, Config. 001 - Do a Special Detailed Inspection of the Trim Tank Overflow
Condition
 Action
 Compliance time
 Repetitive interval
Install the overflow pipe
tool and the pressure
transducer tool in
accordance with
SUBTASK
283130-480-401 001 for
the trim surge tank
Before next flight
 None
AND
NACA duct not found
blocked or damaged
Repeat the trim tank
overflow ground test in
accordance with
SUBTASK
283130-832-402 001
Before next flight
 None
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 283130-832-895-001: Special Detailed Inspection of the Trim Tank Overflow
Get Access
 2.00
On Aircraft
Install the Overflow Pipe Tool and the Pressure
Transducer Tool for the Trim Surge Tank
2.00
Install the Pressure Transducer Tool for the Trim Tank
 1.00
Do the Trim Tank Overflow Ground Test
 6.00
Depending on the Inspection Results, do a Detailed
Inspection of the NACA Duct
2.00
Remove the Overflow Pipe Tool and the Pressure
Transducer Tool for the Trim Surge Tank
2.00
Remove the Pressure Transducer Tool for the Trim
Tank
1.00
Tests
 0.50
Close-Up
 1.00
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 12
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SERVICE BULLETIN
Task 283130-832-895-001: Special Detailed Inspection of the Trim Tank Overflow
TOTAL MANHOURS
 17.50
ELAPSED TIME (HOURS)
 5.25
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-UAAAA
 given in Appendix 01.
NOTE
: The minimum manhours necessary to accomplish this Service Bulletin are
those for the Inspection. Depending on the inspection result, additional
manhours can apply.
H. WEIGHT AND BALANCE
Not Changed
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
Aircraft Maintenance Manual (AMM)
 06-20-00 06-41-55 12-34-24
20-21-11 28-00-00 28-10-00
28-11-00 28-11-42 28-11-43
28-12-00 28-12-48 28-25-00
32-12-00 52-41-23
Elec. Std. Practices Manual (ESPM)
 20-55-00
Structural Repair Manual (SRM)
 51-42-00
K. PUBLICATION AFFECTED
None
L. INTERCHANGEABILITY/MIXABILITY
Not Applicable
M. SPARES
None
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 13
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SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 14
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SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
No Material Set
(2) Price and Availability
No Material Set
B. INDUSTRY SUPPORT INFORMATION
For aircraft under warranty at May 30/17 and for the accomplishment of this Service Bulletin
before Nov 30/20, 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.
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit
management department.
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
France
E-mail: monitored.retrofit@airbus.com
C. LIST OF COMPONENTS
No Kit
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
None
(2) Components
NOTE
: To accomplish this Service Bulletin it is necessary to use the expendable
parts listed in the subsequent referenced task:
- AMM Task 28-12-48-400-801
- AMM Task 28-11-42-400-802
- AMM Task 28-11-43-400-801.
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 15
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SERVICE BULLETIN
(3) Equipment
None
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
None
F. TOOLING
(1) Tooling - Price and Availability
Tooling policy will be communicated by the Retrofit Information Letter (RIL).
(2) Tools
NOTE
: To accomplish this Service Bulletin it is necessary to use the tools listed
in the subsequent re ferenced tasks:
- AMM Task 28-11-43-000-801
- AMM Task 28-11-43-400-801
- AMM Task 28-11-42-000-802
- AMM Task 28-11-42-400-802
- AMM Task 28-12-00-210-805
- AMM Task 28-12-48-000-801
- AMM Task 28-12-48-400-801.
(3) Special Tools
Kit tool 283130T01R00
ITEM
 PART N˚
 KEYWORD
 QTY
 SEE
NOTES
2
 98F28109017000
 TOOL
 1
98F28109018000
 TOOL
 1
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 16
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SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 283130-832-895-001 - Special Detailed Inspection of the Trim Tank Overflow
WARNING
: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
WARNING
: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE
IN POSITION BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND RELATED DOORS
- COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS
AND CAN CAUSE DAMAGE.
WARNING
: YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO WORK IN
OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE SAFETY PROCEDURES,
T H E R EI SAR I S KO F :
- DEATH OR INJURY TO PERSONS
- DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT.
WARNING
: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY
KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION
(CDCCL). CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A
POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN
THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A
CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
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.
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 17
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SERVICE BULLETIN
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.
NOTE
: The purpose of flowcharts is to supplement the information given in the Procedure
and Compliance paragraphs and not to serve as the primary source for tasks or
compliance times given in this Service Bulletin.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact Airbus for further
instructions and approval.
Task Associated Data
Zone
140 190 210 319 343 346
Access
Door
 312AR
Panel
 198DB
Manpower
TOTAL MANHOURS
 17.50
ELAPSED TIME (HOURS)
 5.25
A. GENERAL
(1) Subtask 283130-910-401-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 18
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SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-41-55, Page Block 001
Task 20-21-11-911-801
Structural Repair Manual (SRM)
 51-42-00
(a) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(b) For the identification of access panels, refer to AMM 06-41-55, Page Block 001.
(c) To torque tighten the standard threaded fasteners, refer to AMM Task
20-21-11-911-801.
(d) Remove and install fasteners in accordance with SRM 51-42-00.
(2) Subtask 283130-839-401-001 - 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 283130-941-401-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 28-00-00-610-801
Task 28-10-00-910-801
Task 32-12-00-010-801
Task 52-41-23-000-801
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: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 19
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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) Open the Main Landing Gear (MLG) door Left Hand (LH) side to access to the
valves 700QN1, 700QN2 and 701QN, refer to AMM Task 32-12-00-010-801.
(c) Do the job set-up procedure as specified in the removal of the maintenance door
312AR to access to the valve 705QN, refer to AMM Task 52-41-23-000-801.
(d) Open the access panel 198DB to access to the refuel/defuel control panel 990VU.
(e) Obey the fuel safety procedures when you do work on the f uel syst em, refer to
AMM Task 28-00-00-610-801 and AMM Task 28-10-00-910-801.
(f) Put an access platforms in position at zones 343 and 346.
C. PROCEDURE
(1) Subtask 283130-480-401-001 - Install th e Overflow Pipe Tool and the Pressure
Transducer Tool for the Trim Surge Tank
Work Zones and Access Panels
Zone
 Access/Work location
346
 Work location
 from Rib 18 to Rib 19
Manpower Resources
Manhours
 2.00
Minimum number of person
 2
Subtask elapsed time
 1.00
Skills
 AIRFRAME
Material necessary to do the job
Kit tool 283130T01R00
ITEM
 PART N˚
 KEYWORD
 QTY
 SEE
NOTES
2
 98F28109017000
 TOOL
 1
98F28109018000
 TOOL
 1
References
Aircraft Maintenance Manual (AMM)
 Task 20-21-11-911-801
Task 28-11-43-000-801
Task 28-12-48-000-801
Structural Repair Manual (SRM)
 51-42-00
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 20
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References
Fig. A-UBAAA
Installation of the Overflow Pipe Tool to
the NACA Vent Intake Panel
Sheet 01
Fig. A-UBCAA
Removal/Installation of the Trim Surge
Tank Water Drain Valve
Sheet 01
(a) Install the overflow pipe to the NACA vent intake panel on the lower skin of the trim
surge tank:
In accordance with SRM 51-42-00
Refer to Fig. A-UBAAA
1
 Remove the screws and washers from the NACA vent intake panel, refer to
AMM Task 28-12-48-000-801.
8 Screw Item (1) Retain
8 Washer Item (5) Retain
2
 Attach the overflow pipe tool to the NACA vent intake panel using the screws
provided:
Item 2 98F28109017000 Overflow Pipe Tool 1
NOTE
: Ensure you that the pipe hangs as vertically as possible.
3
 Place the open end of the hose into a standard 1000 liter container positioned
on the ground.
(b) Install the pressure transducer tool into the trim surge tank water drain valve
(5106QS):
Refer to AMM Task 20-21-11-911-801
In accordance with SRM 51-42-00
Refer to Fig. A-UBCAA
1
 Remove the trim tank outer drain valve, item (4).
Refer to AMM Task 28-11-43-000-801
Remove:
1 Trim Surge Tank Water
Drain Valve
Item (4) Retain
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 21
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SERVICE BULLETIN
2
 Install the pressure transducer tool:
98F28109018000 Pressure
Transducer Tool
1
a
 Carefully screw by hand and tighten to 0.34 m.daN (30.09 lbf.in.).
b
 In case of leaks, increase the torque to a maximum value of 0.564 m.daN
(49.92 lbf.in.).
CAUTION
: DO NOT OVER TIGHTEN AS THIS CAN DAMAGE THE
WATER DRAIN VALVE.
(2) Subtask 283130-480-402-001 - Ins tall the Pressure Transducer Tool for the Trim
Tank
Work Zones and Access Panels
Zone
 Access/Work location
343
 Work location
 from Rib 3 to Rib 4
Manpower Resources
Manhours
 1.00
Minimum number of person
 2
Subtask elapsed time
 0.50
Skills
 AIRFRAME
Material necessary to do the job
Kit tool 283130T01R00
ITEM
 PART N˚
 KEYWORD
 QTY
 SEE
NOTES
98F28109018000
 TOOL
 1
References
Aircraft Maintenance Manual (AMM)
 Task 20-21-11-911-801
Task 28-11-42-000-802
Structural Repair Manual (SRM)
 51-42-00
Fig. A-UBBAA
Removal/Installation of the Trim Tank
Water Drain Valve
Sheet 01
(a) Install the pressure transducer in the trim tank water drain valve (5105QS2):
Refer to AMM Task 20-21-11-911-801
In accordance with SRM 51-42-00
Refer to Fig. A-UBBAA
1
 Remove the trim tank outer drain valve, item (6).
Refer to AMM Task 28-11-42-000-802
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 22
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SERVICE BULLETIN
1 Trim Tank outer Drain
Valve
Item (6) Retain
2
 Install the pressure transducer tool:
98F28109018000 Pressure
Transducer Tool
1
a
 Carefully screw by hand and tighten to 0.34 m.daN (30.09 lbf.in.).
b
 In case of leaks, increase the torque to a maximum value of 0.564 m.daN
(49.92 lbf.in.).
CAUTION
: DO NOT OVER TIGHTEN AS THIS CAN DAMAGE THE
WATER DRAIN VALVE.
(3) Subtask 283130-832-402-001 - Do the Tr im Tank Overflow Ground Test
Work Zones and Access Panels
Zone
 Access/Work location
343
 Work location
 from Rib 3 to Rib 4
346
 Work location
 from Rib 18 to Rib 19
210
 Work location
 Door 831
Door 841
140
319
 Access
 Door 312AR
190
 Access
 Panel 198DB
Manpower Resources
Manhours
 6.00
Minimum number of person
 4
Subtask elapsed time
 1.50
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 28-25-00-650-801
Fig. A-UFAAA
Flowchart
Sheet 01
Fig. A-UBDAA
Location of the Valves Actuators
700QN1, 700QN2 and 701QN
Sheet 01
Fig. A-UBEAA
Location of the Inlet Valve Actuator
705QN
Sheet 01
CAUTION
: IF AT ANY POINT DURING THE TEST, EITHER THE TRIM TANK OR
THE TRIM SURGE TANK PRESSURES ARE EXCEEDED (I.E. TEST
FAIL) STOP THE TRANSFER IMMEDIATELY.
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 23
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SERVICE BULLETIN
(a) At the threshold given in the PLANNING INFORMATION paragraph E.(2):
Do the trim tank overflow ground test.
Refer to Fig. A-UFAAA
Refer to Fig. A-UBDAA
Refer to Fig. A-UBEAA
NOTE
: If at any time the tank pressures are exceeded then the test is
considered failed.
NOTE
: The trim tank shall be below high level. There should be sufficient
fuel in the wing tanks to ensure that the aircraft remains within
Center of Gravity (CG) limits throughout the test. In order to keep
the CG forward and have sufficient fuel for the AFT transfer, each
inner tank shall be greater than 20 T.
1
 Open the following valves using the Multipurpose Control and Display Unit
(MCDU) fuel valve test:
a
 LEFT AND RIGHT AFT TRANS FER VALVES: B and D (5700QA1 /
700QN1 and 5700QA1 / 700QN2)
b
 TRIM PIPE ISOLATION VALVE: W (5701QA / 701QN)
c
 TRIM TANK INLET VALVE: L (5705QA / 705QN).
2
 Disconnect the connectors of the following valve actuators in order to prevent
closure from the Fuel Control and Monitoring Computer (FCMC):
a
 On centre section rear spar:
<1> LEFT AND RIGHT AFT TRANSFER VALVES: B and D (700QN1
and 700QN2)
<2> TRIM PIPE ISOLATION VALVE: W (701QN).
b
 On trim tank:
<1> TRIM TANK INLET VALVE: L (705QN).
3
 On the OVERHEAD PANEL (245VU) select PUMP L1 to ON.
4
 Fill trim tank towards high level (which shall be monitored on the MCDU page
’FUEL - FCMC1 - SPECIFIC DATA - FUEL QUANTITIES’), ensuring that the
following pressures are not exceeded:
- Trim tank: 5.8 psi (400 mbar)
- Trim surge tank: 3 psi (210 mbar).
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 24
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5
 When high level is reached, continue to fill the trim tank and then start to
overflow the trim tank (as observed by test person monitoring trim surge tank
pressure gauge).
NOTE
: High level and overflow indications can also be visualised on
the refuel/defuel control panel 990VU.
6
 Ensure that the tank pressures do not exceed the following at any time during
the overflow:
- Trim tank: 10.5 psi (725 mbar)
- Trim surge tank: 3 psi (210 mbar).
7
 Once an overflow has started, on the OVERHEAD PANEL (245VU) select
PUMP R1 to ON.
8
 Once the overflow had reached a steady state, on the OVERHEAD PANEL
(245VU) select PUMP L2 to ON and PUMP R2 to ON.
9
 Once the overflow has reached steady state (approximately 30 seconds)
measure and record the tank pressures and ensure they are below the
following:
- Trim tank: 10.5 psi (725 mbar)
- Trim surge tank: 3 psi (210 mbar).
10
 On the OVERHEAD PANEL (245VU) deselect ALL PUMPS.
11
 Defuel the trim tank to at least below high level, refer to AMM Task
28-25-00-650-801.
NOTE
: High level indication has disappeared on the refuel/defuel
control panel 990VU.
12
 Reconnect all valve actuators.
13
 On the MCDU return all valves to CLOSED position.
NOTE
: When the valves are disconnected, they will be with an
indication ’FAIL UNKNOWN’. When you reconnect them, they
will be with ’FAIL OPEN’. In this state, you can return to the
CLOSED position.
a
 If trim tank pressure values is exceeded:
<1> Contact AIRBUS before next flight and follow their instructions.
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 25
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b
 If trim tank pressure values is not exceeded and trim surge tank pressure
values is not exceeded:
<1> Remove the tools in the trim surge tank in accordance with
SUBTASK 283130-080-402 001 Remove the Overflow Pipe Tool
and the Pressure Transducer Tool for the Trim Surge Tank .
<2> Remove the tool in the trim tank in accordance with SUBTASK
283130-080-401 001 Remove the Pressure Transducer Tool for the
Trim Tank .
<3> No further action.
c
 If trim tank pressure values is not exceeded and trim surge tank pressure
values is exceeded:
<1> Remove the tools in the trim surge tank in accordance with
SUBTASK 283130-080-402 001 Remove the Overflow Pipe Tool
and the Pressure Transducer Tool for the Trim Surge Tank .
<2> Do a detailed inspection of the NACA duct in accordance with
SUBTASK 283130-832-404 001 Depending on the Inspection
Results, do a Detailed Inspection of the NACA Duct .
<3> Install the tool in the trim surge tank in accordance with SUBTASK
283130-480-401 001 Install the Overflow Pipe Tool and the
Pressure Transducer Tool for the Trim Surge Tank .
<4> Repeat trim tank overflow ground test in accordance with SUBTASK
283130-832-402 001 Do the Trim Tank Overflow Ground Test .
(4) Subtask 283130-832-404-001 - Depending on the Inspection Results, do a Detailed
Inspection of the NACA Duct
Work Zones and Access Panels
Zone
 Access/Work location
346
 Work location
 from Rib 18 to Rib 19
Manpower Resources
Manhours
 2.00
Minimum number of person
 2
Subtask elapsed time
 1.00
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 28-12-00-210-803
Task 28-12-00-210-805
28-12-48, Page Block 401
Fig. A-UFAAA
Flowchart
Sheet 01
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 26
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SERVICE BULLETIN
(a) Do a general visual inspection of the aperture leading to the flame arrestors (NACA
duct), refer to AMM Task 28-12-00-210-803.
And
Do a detailed inspection of the trim tank flame arrestor, refer to AMM Task
28-12-00-210-805.
1
 If damage or a blockage is found:
a
 Remove the blockage
Or
Do the applicable repair procedure.
NOTE
: If necessary, replace the applicable NACA duct assembly,
refer to AMM 28-12-48, Page Block 401.
(5) Subtask 283130-080-402- 001 - Remove the Overflow Pipe Tool and the Pressure
Transducer Tool for the Trim Surge Tank
Work Zones and Access Panels
Zone
 Access/Work location
346
 Work location
 from Rib 18 to Rib 19
Manpower Resources
Manhours
 2.00
Minimum number of person
 2
Subtask elapsed time
 1.00
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 Task 20-21-11-911-801
Task 28-11-43-400-801
Task 28-12-48-400-801
Structural Repair Manual (SRM)
 51-42-00
Fig. A-UBAAA
Installation of the Overflow Pipe Tool to
the NACA Vent Intake Panel
Sheet 01
Fig. A-UBCAA
Removal/Installation of the Trim Surge
Tank Water Drain Valve
Sheet 01
(a) Remove the pressure transducer tool from the trim surge tank water drain valve
(5106QS):
Refer to AMM Task 20-21-11-911-801
In accordance with SRM 51-42-00
Refer to Fig. A-UBCAA
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 27
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SERVICE BULLETIN
1
 Carefully remove the pressure transducer tool.
2
 Install the trim tank outer drain valve, item (4).
Refer to AMM Task 28-11-43-400-801
1 Trim Surge Tank Water
Drain Valve
Item (4) Retained at
removal
a
 Torque the outer drain valve item (4) to 0.34 m.daN (30.09 lbf.in.).
b
 In case of leaks, increase the torque to a maximum value of 0.791 m.daN
(70.00 lbf.in.).
CAUTION
: DO NOT OVER TIGHTEN AS THIS CAN DAMAGE THE
WATER DRAIN VALVE.
(b) Remove the overflow pipe tool from the NACA vent intake panel on the lower skin
of the trim surge tank:
In accordance with SRM 51-42-00
Refer to Fig. A-UBAAA
1
 Remove the captive screws of the overflow pipe tool ensuring any residual fuel
in the tool is emptied into the 1000 liter container.
2
 Install the screws and washers on the NACA vent intake panel, refer to AMM
Task 28-12-48-400-801.
Install:
8 Screw Item (1) Retained at
removal
8 Washer Item (5) Retained at
removal
(6) Subtask 283130-080-401- 001 - Remove the Pressure Transducer Tool for the Trim
Tank
Work Zones and Access Panels
Zone
 Access/Work location
343
 Work location
 from Rib 3 to Rib 4
Manpower Resources
Manhours
 1.00
Minimum number of person
 2
Subtask elapsed time
 0.50
Skills
 AIRFRAME
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 28
7
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SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 Task 20-21-11-911-801
Task 28-11-42-400-802
Structural Repair Manual (SRM)
 51-42-00
Fig. A-UBBAA
Removal/Installation of the Trim Tank
Water Drain Valve
Sheet 01
(a) Remove the pressure transducer tool from the trim tank water drain valve
(5105QS2):
Refer to AMM Task 20-21-11-911-801
In accordance with SRM 51-42-00
Refer to Fig. A-UBBAA
1
 Carefully remove the pressure transducer tool.
2
 Install the trim tank outer drain valve, item (6).
Refer to AMM Task 28-11-42-400-802
1 Trim Tank outer Drain
Valve
Item (6) Retained at
removal
a
 Torque the trim tank outer drain valve item (6) to 0.34 m.daN (30.09
lbf.in).
b
 In case of leaks, increase the torque to a maximum value of 0.791 m.daN
(70.00 lbf.in).
CAUTION
: DO NOT OVER TIGHTEN AS THIS CAN DAMAGE THE
WATER DRAIN VALVE.
D. TEST
(1) Subtask 283130-790-401-001 - Leak Test
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 28-11-00-790-823
(a) Do the leak test, refer to AMM Task 28-11-00-790-823.
E. CLOSE-UP
(1) Subtask 283130-942-403-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 29
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References
Aircraft Maintenance Manual (AMM)
 Task 32-12-00-410-801
Task 52-41-23-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Close the access panel 198DB.
(c) Do the close-up procedure as specified after the installation of the maintenance
door 312AR, refer to AMM Task 52-41-23-400-801.
(d) Close the MLG door LH side, refer to AMM Task 32-12-00-410-801.
(e) Remove the access platforms.
(f) Put the aircraft back to its initial configuration.
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 30
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**CONF ALL
2
B
RIB21
RIB18
RIB19
A
B
TRIM SURGE TANK
WATER DRAIN VALVE
NACA VENT
INTAKE PANEL
TRIM TANK
NACA OUTLET
TRIM TANK
OVERPRESSURE PROTECTOR
SPAR BOX
Z346
A
5106QS
(1)
(5) x8
x8
G_SB_283130_7_BAAA_01_03
Figure A-UBAAA - Sheet 01
Installation of the Overflow Pipe Tool to the NACA Vent Intake Panel
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 31
7
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SERVICE BULLETIN
**CONF ALL
Z343
A
B
A
B
RIB4
(6)
TRIM TANK
WATER DRAIN VALVE
RIB3
O−RING
5105QS2
G_SB_283130_7_BBAA_01_03
Figure A-UBBAA - Sheet 01
Removal/Installation of the Trim Tank Water Drain Valve
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 32
7
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@A330
SERVICE BULLETIN
**CONF ALL
(4)
B
Z346
RIB21
RIB18
RIB19
A
A
B
TRIM SURGE TANK
WATER DRAIN VALVE
O−RING
5106QS
G_SB_283130_7_BCAA_01_02
Figure A-UBCAA - Sheet 01
Removal/Installation of the Trim Surge Tank Water Drain Valve
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 33
7
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@A330
SERVICE BULLETIN
**CONF ALL
FR47
FR40 FR47
FR46 FR47
Z140A
A
B
B
C
C
C
700QN2
700QN1
701QN
C
TYPICAL VIEW
VALVE ACTUATOR
G_SB_283130_7_BDAA_01_01
Figure A-UBDAA - Sheet 01
Location of the Valves Actuators 700QN1, 700QN2 and 701QN
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 34
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SERVICE BULLETIN
**CONF ALL
A
RIB2
RIB3
B
B
A
Z319
705QN
INLET VALVE
ACTUATOR
705QN
G_SB_283130_7_BEAA_01_00
Figure A-UBEAA - Sheet 01
Location of the Inlet Valve Actuator 705QN
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 35
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SERVICE BULLETIN
**CONF ALL
DO A SPECIAL DETAILED INSPECTION OF THE TRIM TANK OVERFLOW, AT THE THRESHOLD GIVEN IN THE
PLANNING INFORMATION PARAGRAPH E.(2), IN ACCORDANCE WITH TASK 283130−832−895−001
YESNO
TRIM TANK
PRESSURE VALUES
EXCEEDED?
YES
TRIM SURGE
TANK PRESSURE VALUES
EXCEEDED?
NOTE:
NO FURTHER
THE PURPOSE OF FLOWCHARTS 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.
ACTION
YES
REMOVE THE BLOCKAGE OR DO THE  
CONTACT AIRBUS AND
FOLLOW THEIR INSTRUCTIONS
BEFORE NEXT FLIGHT
APPLICABLE REPAIR PROCEDURE 
INSTALL THE OVERFLOW PIPE TOOL AND THE PRESSURE TRANSDUCER TOOLS,  IN ACCORDANCE WITH
SUBTASK 283130−480−401−001 FOR THE TRIM SURGE TANK AND SUBTASK 283130−480−402−001 FOR THE TRIM TANK
DO THE TRIM TANK OVERFLOW GROUND TEST,
IN ACCORDANCE WITH SUBTASK 283130−832−402−001
REMOVE THE OVERFLOW PIPE TOOL AND THE PRESSURE
TRANSDUCER TOOL, IN ACCORDANCE WITH SUBTASK 
283130−080−402−001 FOR THE TRIM SURGE TANK
DO AN INSPECTION OF THE APERTURE LEADING
TO THE FLAME ARRESTORS (NACA DUCT) AND
DO A DETAILED INSPECTION OF THE FLAME ARRESTOR,
IN ACCORDANCE WITH SUBTASK 283130−832−404−001
REMOVE THE OVERFLOW PIPE TOOL AND THE PRESSURE
TRANSDUCER TOOLS, IN ACCORDANCE WITH SUBTASK
283130−080−401−001 FOR THE TRIM TANK AND
SUBTASK 283130−080−402−001 FOR THE TRIM SURGE TANK
INSTALL THE OVERFLOW PIPE TOOL AND THE PRESSURE
TRANSDUCER TOOL, IN ACCORDANCE WITH SUBTASK
283130−480−401−001 FOR THE TRIM SURGE TANK
REPEAT THE TRIM TANK OVERFLOW GROUND TEST,
IN ACCORDANCE WITH SUBTASK 283130−832−402−001
IS THE NACA
DUCT BLOCKED OR
DAMAGED?
BEFORE NEXT FLIGHT
NO
NO
G_SB_283130_7_FAAA_01_00
Figure A-UFAAA - Sheet 01
Flowchart
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 36
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SERVICE BULLETIN
Appendix 01 - Manpower Gantt Chart
**CONF ALL
For an explanation of the manhours and elapsed time, refer to the next page(s).
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 1
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Appendix 01 - Manpower Gantt Chart
**CONF ALL
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A330−28−3130
MH ET/S
TOTAL MANHOURS
SB ELAPSED TIME
15.50
5.25
STEPS
0
MH
ET/S:
PER
MANHOURS
ELAPSED TIME PER STEP
NUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.
OPERATORS MAY DETERMINE THAT ANOTHER WAY
TO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
:
:
SB ELAPSED TIME
(HOURS)
1 2 3
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS
ARE NOT REFLECTED IN THIS GANTT CHART.
4 5
GET ACCESS 2.00 1.002
INSTALL THE OVERFLOW PIPE TOOL 2.00 1.002
AND THE PRESSURE TRANSDUCER
TOOL OF THE TRIM SURGE TANK
INSTALL THE PRESSURE 1.00 0.502
TRANSDUCER TOOL OF THE
TRIM TANK
DO THE TRIM TANK OVERFLOW 6.00 1.504
GROUND TEST
REMOVE THE OVERFLOW PIPE TOOL 2.00 1.002
AND THE PRESSURE TRANSDUCER
TOOL OF THE TRIM SURGE TANK
REMOVE THE PRESSURE 1.00 0.502
TRANSDUCER TOOL OF THE
TRIM TANK
TEST 0.50 0.252
CLOSE−UP 1.00 0.502
G_SB_283130_7_AAAA_01_01
Figure A-UAAAA - Sheet 01
Gantt Chart
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 2
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SERVICE BULLETIN
Service Bulletin REPORTING
TITLE: FUEL - TANKS - INSPECTION OF TRIM TANK OVERFLOW
MODIFICATION No.: None
SB Reporting status
This Service Bulletin will only be incorporated into affected customized Maintenance and Flight
Operations Products if it is duly reported to Airbus.
General information
The SB Reporting policy is published in ISI 00.00.00135. This document provides information regarding:
the SB Reporting means and benefits, the update of customized Maintenance Products and customized
Flight Operations Products.
If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations Products" for
further information on the update of affected Flight Operations Products.
SB Reporting procedure
Standard practice to report SB is to use the online reporting application on AirbusWorld.
Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus. Question 2 "What are the standard
practices for SB reporting?"
- If this SB requires previous or simultaneous accomplishment of other SBs, Question 3 "What about
the reporting of prerequisite Service Bulletin?"
NOTE:
 ISI 00.00.00179 covers all the frequently asked questions about SB Reporting. It is revised on a
regular basis.
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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@A330
SERVICE BULLETIN
QUALITY PERCEPTION FORM
Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data
that you provide us will be used to analyse areas of difficulties and to take corrective action to further
improve the quality of our Service Bulletins.
We thank you for the time you have taken in completing this form.
(Please rate on a scale of 1 to 4, with 4 being the highest score)
- Quality rating of this SB 4321
- Quality rating of the Accomplishment Instructions 4321
- Quality rating of the Illustrations 4321
- Is this SB easy to understand ? Y/N
If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a
short description of the issue.
Planning Material Instructions
X Effectivity X Kit content X Preparation
X Reason X List of Materials Operator Supplied X Mod/Inspection
X Manpower X Industry support X Test
X References X Re-identification X Close-Up
X Publication X Tooling X Illustrations
Comments:
Operator: Date:
Name/Title:
Please return this form to:
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn : SEM4 Service Bulletins Management
F A X:( 3 3 )56 19 34 25 1
Or via your Resident Customer Support Office.
DATE: May 18/17 SERVICE BULLETIN No.: A330-28-3130
REVISION No.: 00 - May 18/17 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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