# Airbus Service Bulletin A330-25-3743

Copy: No revision named ("A330-25-3743 R00"), 64 pages: PDF https://openairdocs.org/files/sha256/5b/8a/5b8ad3e21637a94edb5f88a6f6e6c6393508667b0c33ed85defa2e9b6e985803; text https://openairdocs.org/service-documents/airbus/a330-25-3743/file/5b8ad3e21637.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2020-0673, the docket of AD 2021-02-12. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-25-3743
- Page: https://openairdocs.org/service-documents/airbus/a330-25-3743

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

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

- [AD 2021-02-12](https://openairdocs.org/ad/2021-02-12.md), effective Mar 30, 2021: No revision named

## Text (64 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2020-0673, the docket of AD 2021-02-12. 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
REV 00 Sep 23/19 A330-25-3743
Page 1
CONF ALL
AIRBUS
2, ROND POINT EMILE DEWOITINE
31700 BLAGNAC
FRANCE
 
The content of this document is the property of Airbus.
It is supplied in confidence and commercial security on its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may information
contained in it be disclosed to unauthorized persons.
It must not be reproduced in whole or in part without permission in writing from the owners of the
copyright. Requests for reproduction of any data in this document and the media authorized for it must
be addressed to Airbus.
MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - CARGO LINING REPAIRS - INSPECT FOR
CORRECT REPAIR MATERIAL
MODIFICATION No.:
None

### Page 2

A330
SERVICE BULLETIN
SUMMARY
REV 00 Sep 23/19 A330-25-3743
Page 2
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - CARGO LINING REPAIRS - INSPECT FOR
CORRECT REPAIR MATERIAL
SUMMARY
This summary is for information only and is not approved for modification of the aircraft.
A. MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR None
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.
B. REASON
(1) History
Most of the cargo compartment linings are composite sandwich panels made of a
honeycomb core bonded with a front and rear prepreg layer. They have a role in
the fire protection. The related repair procedure in the AMM advise to use material
according to CML 13XBD4. For this application code, two materials are proposed:
Gillpatch III and Speedpatch AF800. T ests revealed that only Gillpatch III is passing the
flame penetration tests (and not Speedpatch AF800).
(2) Objective/Action
An inspection is requested to identify if any repair has been performed using Ref.
AMM T ask 25-50-00-340-803 Speed Patches (on Both Sides) Repair Method (Damage
Through) - All Cargo Compartment Linings with Honeycomb Core”, in combination with
Speedpatch AF800.
(3) Advantages
This Service Bulletin will ensure the correct fire protection function of the cargo
compartment linings.
(4) Operational/Maintenance Consequences
None
C. GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY COST SAVING NO
A/C OPERATION
AFFECTED
NO VENDOR SB NO
CANCELS INSPECTION SB NO ETOPS AFFECTED NO
PAX COMFORT AFFECTED NO POTENTIAL AD YES
RELIABILITY AFFECTED NO STRUCTURAL LIFE EXTENSION NO
LIFE LIMIT NO LINE MAINTENANCE AFFECTED NO
NOTE: Service Bulletin must be accomplished.

### Page 3

A330
SERVICE BULLETIN
SUMMARY
REV 00 Sep 23/19 A330-25-3743
Page 3
D. MAINTENANCE CONFIGURATION
No specific aircraft maintenance configuration required.
E. MATERIAL PRICE INFORMATION
(1) Inspection of Cargo-Compartment Linings for correct Repair Material on
Aircraft
(a) T ask set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-Compartment
Linings for correct Repair Material on Aircraft
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Components See SB See Note Blind rivets, washer
NOTE: Price information to be obtained from the given supplier.
(2) Inspection of Cargo-Compartment Linings for correct Repair Material in
Warehouse or Workshop
(a) T ask set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-Compartment
Linings for correct Repair Material in Warehouse or Workshop
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Components See SB See Note Blind rivets, washer
NOTE: Price information to be obtained from the given supplier.
F. APPLICABILITY
This Service Bulletin is applicable to this (these) operator(s):
01Q 01V 09K 12P 18P 18Q 34N 36P 38W 39N 39V 41N 46O 57L 72T 77L 78X 83V 96U 97X
98W AAF AAL AAR AAW ABR ACA ACI AEA AFL AFR AHK AIB ALK ARG ASL ASY AVA AWW AZA
AZU BCS BEC BEL BOS CAL CBJ CCA CEB CES CHH CPA CRK CRL CSA CSC CSN CSZ CXB DAH
DAL DGA DLH EDW EIN ETD EVA EVE F2I FAF FIN FJI FWI G2X G8E GCR GFA GIA GJT GRL HAL
HDA HFM HFY HKC HVN IAW IBE IRA ISS JAI JAV KAC KAL KKK KLM LAA LKE LLC LMU LNI MAS
MAU MEA MNB MSC MSR NMB NWS OBS OHY OMA P2C PAL PLM QAF QFA QTR RNA RSF RSY
RWD RZO SAA SAF SAS SIA SVA SWR SXD SZN TAI TAM TAP TAR TAX TBA TCX THA THY TLM
TOW TPA TSC U6A UAE UAF VIR VKG VOZ WOW XAX XLF
G. CONCURRENT REQUIREMENTS
None
H. NATURE OF THE WORK
(1) Inspection of Cargo-Compartment Linings for correct Repair Material on
Aircraft
(a) T ask set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-Compartment
Linings for correct Repair Material on Aircraft
AIRCRAFT YES
EQUIPMENT NO

### Page 4

A330
SERVICE BULLETIN
SUMMARY
REV 00 Sep 23/19 A330-25-3743
Page 4
(2) Inspection of Cargo-Compartment Linings for correct Repair Material in
Warehouse or Workshop
(a) T ask set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-Compartment
Linings for correct Repair Material in Warehouse or Workshop
AIRCRAFT NO
EQUIPMENT NO
I. MANPOWER
(1) Inspection of Cargo-Compartment Linings for correct Repair Material on
Aircraft
(a) T ask set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-Compartment
Linings for correct Repair Material on Aircraft
MANPOWER
TOTAL MAN-HOURS 10.00 h
ELAPSED TIME (HOURS) 6.00 h
(2) Inspection of Cargo-Compartment Linings for correct Repair Material in
Warehouse or Workshop
(a) T ask set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-Compartment
Linings for correct Repair Material in Warehouse or Workshop
MANPOWER
TOTAL MAN-HOURS 1.25 h
ELAPSED TIME (HOURS) 1.25 h

### Page 5

A330
SERVICE BULLETIN
SUMMARY
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3Y-A-001-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743General overview
Page 5
J. GENERAL OVERVIEW
CONF ALL
FR53.2
FR66
FR65
FR73
FR39.1
FR20
Z130
Z160
Z150
A
B
C
HONEYCOMB CORE LININGS
TO BE INSPECTED
HONEYCOMB CORE LININGS
TO BE INSPECTED
HONEYCOMB CORE LININGS
TO BE INSPECTED
A
B
C
ICN-A330-A-25XX3743-A-FAPE3-00J3Y-A-001-01

### Page 6

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 6
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - CARGO LINING REPAIRS - INSPECT FOR
CORRECT REPAIR MATERIAL
1. PLANNING INFORMATION
A. APPLICABILITY
(1) Models
ON A/C 0211, 0269, 0272, 0330, 0339, 0397, 0441, 0473, 0487, 0489, 0506-0508, 0510,
0511, 0513, 0521, 0522, 0571, 0605, 0638, 0644, 0647, 0650, 0653, 0667, 0733, 0743,
0745, 0746, 0749, 0760, 0792, 0814, 0820, 0825, 0831, 0841, 0842, 0849, 0853, 0877,
0883, 0885, 0888, 0899, 0904, 0914, 0923, 0931, 0934, 0940, 0945, 0947, 0950, 0956,
0980, 0996, 1043, 1057, 1061, 1094, 1123, 1135, 1169, 1174, 1198, 1218, 1225, 1235,
1251, 1252, 1258, 1283, 1308, 1313, 1321, 1327, 1339, 1354, 1365, 1379, 1412, 1472,
1478, 1505, 1516, 1543, 1605, 1613, 1623, 1630, 1649, 1694, 1700, 1710, 1719, 1728,
1736, 1737, 1740, 1747, 1748, 1755, 1761, 1777, 1784, 1835, 1854, 1864, 1877, 1882,
1932, 1936
330-202
ON A/C 0422, 0443, 0448, 0458, 0463, 0465, 0466, 0472, 0477, 0481, 0486, 0498, 0500,
0502-0504, 0516, 0519, 0530, 0535, 0555, 0567, 0573, 0584, 0587, 0612, 0616, 0634, 0655,
0657, 0661, 0678, 0682, 0684, 0686, 0693, 0697, 0700, 0703, 0704, 0738, 0742, 0747,
0754, 0755, 0770, 0774, 0801, 0811, 0819, 0834, 0871, 0882, 0887, 0892, 0898, 0900,
0901, 0925, 0932, 0951, 0969, 0976, 1036, 1161, 1183
330-203
ON A/C 0181, 0195, 0222, 0223, 0226, 0229, 0230, 0232, 0238, 0240, 0247, 0249, 0253,
0255, 0258, 0259, 0262, 0275, 0288, 0290, 0291, 0296, 0300, 0305, 0308, 0312, 0317,
0322, 0324, 0343, 0353, 0358, 0362, 0364, 0366, 0403, 0432, 0444, 0454, 0469, 0476,
0493, 0609, 0614, 0618, 0620, 0621, 0631, 0633, 0665, 0718, 0722, 0739, 0778, 0796,
0802, 0822, 0828, 0869, 0874, 0876, 0891, 0911, 0927, 0939, 0943, 0946, 0949, 0961,
0962, 0968, 0970, 0977, 0979, 1002, 1019, 1031, 1034, 1039, 1042, 1054, 1059, 1096,
1112, 1116, 1118, 1129, 1133, 1155, 1200, 1202, 1203, 1213, 1220, 1221, 1233, 1244,
1256, 1266, 1297, 1309, 1335, 1393
330-223
ON A/C 1136, 1148, 1164, 1180
330-223F
ON A/C 0248, 0250, 0251, 0254, 0261, 0265, 0266, 0271, 0276, 0281, 0283, 0285-0287,
0293, 0295, 0301, 0303, 0306, 0309, 0311, 0313, 0314, 0316, 0320, 0326, 0328, 0334,
0340, 0345, 0348, 0365, 0369, 0372, 0382, 0384, 0392, 0396, 0398, 0401, 0404, 0409,
0427, 0437, 0451, 0452, 0455, 0456, 0461, 0462, 0480, 0491, 0494, 0501, 0505, 0509,
0518, 0525-0527, 0529, 0532, 0536, 0551, 0597, 0600, 0610, 0625, 0627, 0632, 0635, 0649,
0652, 0656, 0658, 0664, 0666, 0683, 0688, 0696, 0709, 0717, 0724, 0726, 0728-0730, 0732,
0735, 0737, 0750, 0751, 0756, 0759, 0780, 0785, 0788, 0795, 0797, 0807, 0809, 0810,
0815, 0818, 0821, 0824, 0832, 0839, 0840, 0852, 0854, 0860, 0863, 0867, 0868, 0873,
0875, 0881, 0884, 0890, 0903, 0906, 0909, 0916, 0919, 0926, 0930, 0941, 0944, 0948,
0957, 0963, 0966, 0967, 0971, 0973, 0975, 0982, 0984, 0988, 0991, 0992, 0995, 0998,
1008, 1009, 1011, 1014, 1016, 1020, 1022, 1028, 1033, 1038, 1041, 1045-1047, 1049, 1052,
1053, 1069, 1073, 1076, 1080, 1082, 1095, 1100, 1104, 1114, 1120, 1138, 1159, 1171,
1184, 1186, 1191, 1208, 1210, 1214, 1217, 1223, 1224, 1227, 1236, 1237, 1240, 1241,
1248-1250, 1259-1262, 1267, 1271, 1275, 1277, 1279, 1280, 1282, 1286, 1288, 1291, 1293,
1295, 1302-1304, 1306, 1310, 1312, 1316, 1319, 1322, 1324, 1330, 1331, 1334, 1342, 1363,
1364, 1372, 1375, 1389, 1390, 1394, 1396, 1399, 1400, 1402, 1404, 1407, 1410, 1415-1417,
1419, 1421, 1422, 1429, 1434, 1439-1441, 1444, 1451, 1452, 1455, 1459, 1461, 1465, 1466,
1468, 1469, 1471, 1474, 1479, 1480, 1484, 1486, 1488, 1492, 1496, 1498, 1500, 1502,

### Page 7

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 7
1508, 1511, 1512, 1520, 1521, 1526, 1530, 1537, 1540, 1547, 1555, 1558, 1561, 1565,
1569, 1573, 1586, 1588, 1591, 1601, 1603, 1606, 1608, 1610, 1615, 1617, 1626, 1631,
1639, 1641, 1643, 1653, 1655, 1657, 1662, 1664, 1667, 1672, 1676, 1678, 1681, 1725,
1730, 1732, 1735, 1741, 1746, 1751, 1756, 1758, 1762, 1771, 1773, 1775, 1780, 1782,
1785, 1787, 1799, 1805, 1808, 1822, 1823, 1830, 1845, 1847, 1848, 1857, 1859, 1872,
1878, 1883, 1886, 1891, 1911, 1916, 1919, 1942, 1945, 1960, 1965, 1968, 1982, 1989
330-243
ON A/C 1004, 1032, 1051, 1062, 1070, 1092, 1115, 1175, 1320, 1332, 1344, 1350, 1368,
1380, 1386, 1406, 1414, 1418, 1428, 1442, 1448, 1506, 1524, 1534, 1550, 1578, 1584,
1594, 1688, 1708, 1722, 1750, 1768, 1772
330-243F
ON A/C 0030, 0037, 0045, 0054, 0055, 0070, 0086, 0200
330-301
ON A/C 0602, 0607, 0623, 0637, 0641, 0659, 0671, 0675, 0680, 0691, 0699, 0707, 0711,
0714, 0721, 0725, 0734, 0752, 0769, 0789, 0805, 0813, 0823, 0826, 0838, 0847, 0861,
0893, 0907, 0918, 0920, 0985, 0994, 1007, 1013, 1023, 1025, 1067, 1078, 1088, 1106,
1173, 1177, 1254, 1268, 1272, 1274, 1278, 1346, 1351, 1361, 1367, 1370, 1377, 1385,
1391, 1405, 1426, 1437, 1450, 1490, 1499, 1507, 1515, 1535, 1539, 1627, 1628, 1637,
1679, 1684, 1690, 1701, 1716, 1720, 1721, 1742, 1744, 1767, 1769, 1778, 1783, 1791,
1794, 1806, 1817, 1950, 1951
330-302
ON A/C 0553, 0558, 0564, 0574, 0593, 0595, 0603, 0695, 0705, 0712, 1287, 1294, 1300,
1360, 1381, 1458, 1476, 1487, 1501, 1514, 1529, 1571, 1580, 1616, 1620, 1622, 1629,
1640, 1642, 1644, 1696, 1704, 1706, 1713, 1718
330-303
ON A/C 0050, 0060, 0062, 0065, 0112, 0122
330-321
ON A/C 0072, 0082, 0087, 0095, 0096, 0116, 0120, 0127, 0143, 0162, 0171, 0172, 0206,
0209, 0219, 0224, 0231, 0241
330-322
ON A/C 0256, 0267, 0315, 0323, 0333, 0337, 0338, 0342, 0346, 0350, 0351, 0368, 0370,
0375, 0380, 0388, 0425, 0428, 0484, 0490, 0524, 0533, 0542, 0549, 0550, 0552, 0578,
0588, 0591, 0640, 0663, 0674, 0676, 0690, 0708, 0758, 0772, 0784, 0799, 0803, 0806,
0817, 0827, 0843, 0845, 0857-0859, 0865, 0965, 1001, 1021, 1055, 1151, 1209, 1211, 1219,
1229, 1234, 1243, 1265, 1281, 1318, 1326, 1336, 1337, 1340, 1347, 1388, 1392, 1395,
1425, 1430, 1431, 1435, 1464, 1470, 1489, 1494, 1518, 1519, 1536, 1556, 1575, 1576,
1590, 1593, 1611, 1625, 1636, 1638, 1645, 1647, 1699, 1714, 1727, 1760, 1776, 1793
330-323
ON A/C 0138, 0140, 0144, 0148, 0153, 0165
330-341
ON A/C 0012, 0017, 0071, 0083, 0099, 0102, 0106, 0109, 0111, 0113, 0118, 0121, 0132,
0155, 0177, 0234, 0244, 0669, 0673, 0679, 0776, 0850, 0855, 0895, 0915, 0959, 1163
330-342
ON A/C 0277, 0279, 0284, 0344, 0349, 0356, 0357, 0386, 0389, 0393, 0400, 0405, 0407,
0408, 0412, 0418-0421, 0423, 0439, 0479, 0496, 0497, 0512, 0515, 0539, 0548, 0565,
0568, 0570, 0576, 0579, 0581, 0629, 0636, 0642, 0645, 0648, 0654, 0662, 0670, 0687,
0692, 0701, 0713, 0716, 0720, 0741, 0773, 0777, 0781, 0782, 0786, 0791, 0830, 0833,
0836, 0851, 0862, 0866, 0879, 0889, 0896, 0905, 0908, 0913, 0922, 0928, 0935-0937,
0942, 0952, 0954, 0958, 0964, 0974, 0978, 0983, 0986, 0989, 0990, 0997, 1000, 1003,
1006, 1010, 1012, 1015, 1018, 1026, 1029, 1035, 1037, 1044, 1048, 1058, 1060, 1063,
1065, 1066, 1071, 1072, 1074, 1075, 1077, 1081, 1084-1087, 1089, 1090, 1093, 1097-1099,
1101, 1103, 1105, 1107, 1108, 1110, 1124, 1126, 1127, 1130-1132, 1137, 1141, 1143,

### Page 8

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 8
1145-1147, 1149, 1150, 1153, 1156, 1157, 1160, 1165, 1167, 1168, 1170, 1172, 1178, 1181,
1187-1190, 1192, 1193, 1195, 1196, 1199, 1201, 1204-1206, 1212, 1215, 1216, 1222, 1226,
1228, 1230-1232, 1238, 1239, 1245-1247, 1255, 1263, 1264, 1269, 1270, 1276, 1284, 1285,
1289, 1290, 1292, 1296, 1298, 1299, 1301, 1305, 1307, 1311, 1314, 1315, 1317, 1323,
1325, 1328, 1329, 1333, 1338, 1341, 1343, 1345, 1348, 1349, 1352, 1353, 1355-1359, 1362,
1366, 1369, 1371, 1373, 1374, 1376, 1378, 1382-1384, 1387, 1397, 1398, 1401, 1403, 1408,
1409, 1411, 1413, 1420, 1423, 1427, 1432, 1433, 1436, 1438, 1443, 1445-1447, 1449, 1453,
1454, 1456, 1457, 1460, 1462, 1463, 1467, 1473, 1475, 1477, 1481-1483, 1485, 1491, 1493,
1495, 1497, 1503, 1504, 1509, 1510, 1513, 1517, 1523, 1525, 1527, 1528, 1531-1533, 1538,
1541, 1542, 1544-1546, 1548, 1549, 1551-1554, 1557, 1559, 1560, 1562-1564, 1566-1568,
1570, 1572, 1574, 1577, 1579, 1581-1583, 1585, 1587, 1589, 1592, 1595-1600, 1602, 1604,
1607, 1609, 1612, 1614, 1618, 1619, 1621, 1624, 1632-1635, 1646, 1648, 1650, 1651, 1654,
1656, 1658-1660, 1663, 1665, 1666, 1668-1671, 1673-1675, 1677, 1680, 1685-1687, 1689,
1691-1693, 1695, 1697, 1698, 1703, 1709, 1711, 1712, 1715, 1723, 1724, 1726, 1729, 1731,
1733, 1734, 1738, 1739, 1743, 1745, 1749, 1752-1754, 1757, 1759, 1763-1766, 1770, 1774,
1779, 1781, 1786, 1788-1790, 1792, 1796-1798, 1800-1804, 1807, 1809-1812, 1814-1816,
1818, 1820, 1821, 1825-1829, 1831-1834, 1837-1843, 1846, 1849, 1851, 1852, 1855, 1856,
1858, 1860, 1862, 1863, 1865-1869, 1871, 1873-1875, 1879-1881, 1885, 1889, 1893, 1894,
1896, 1898, 1899, 1902, 1905, 1907, 1912, 1917, 1928
330-343
ON A/C 1819, 1836, 1844, 1850, 1861, 1870, 1876, 1884, 1887, 1890, 1892, 1895, 1897,
1900, 1901, 1903, 1904, 1906, 1908-1910, 1913-1915, 1918, 1920-1927, 1929, 1931,
1933-1935, 1937-1939, 1941, 1943, 1946-1949, 1952-1954, 1956-1959, 1961-1963, 1966,
1970-1973, 1975, 1976, 1978
330-941
CONF ALL
(2) Applicability by MSN
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0065 0070-0072 0082 0083
0086 0087 0095 0096 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 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 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

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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 1274-1423 1425-1521 1523-1651 1653-1660
1662-1681 1684-1701 1703 1704 1706 1708-1716 1718-1794 1796-1812 1814-1823
1825-1852 1854-1887 1889-1929 1931-1939 1941-1943 1945-1954 1956-1963 1965
1966 1968 1970-1973 1975 1976 1978 1982 1989
(3) MSN by configuration
MSN CONFIGURATION
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0065
0070 0071 0072 0082 0083 0086 0087 0095 0096 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 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
001

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MSN CONFIGURATION
0911 0913 0914 0915 0916 0918 0919 0920 0922 0923 0925
0926 0927 0928 0930 0931 0932 0934 0935 0936 0937 0939
0940 0941 0942 0943 0944 0945 0946 0947 0948 0949 0950
0951 0952 0954 0956 0957 0958 0959 0961 0962 0963 0964
0965 0966 0967 0968 0969 0970 0971 0973 0974 0975 0976
0977 0978 0979 0980 0982 0983 0984 0985 0986 0988 0989
0990 0991 0992 0994 0995 0996 0997 0998 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 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 1562 1563 1564 1565
1566 1567 1568 1569 1570 1571 1572 1573 1574 1575 1576

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MSN CONFIGURATION
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 1712 1713 1714 1715
1716 1718 1719 1720 1721 1722 1723 1724 1725 1726 1727
1728 1729 1730 1731 1732 1733 1734 1735 1736 1737 1738
1739 1740 1741 1742 1743 1744 1745 1746 1747 1748 1749
1750 1751 1752 1753 1754 1755 1756 1757 1758 1759 1760
1761 1762 1763 1764 1765 1766 1767 1768 1769 1770 1771
1772 1773 1774 1775 1776 1777 1778 1779 1780 1781 1782
1783 1784 1785 1786 1787 1788 1789 1790 1791 1792 1793
1794 1796 1797 1798 1799 1800 1801 1802 1803 1804 1805
1806 1807 1808 1809 1810 1811 1812 1814 1815 1816 1817
1818 1819 1820 1821 1822 1823 1825 1826 1827 1828 1829
1830 1831 1832 1833 1834 1835 1836 1837 1838 1839 1840
1841 1842 1843 1844 1845 1846 1847 1848 1849 1850 1851
1852 1854 1855 1856 1857 1858 1859 1860 1861 1862 1863
1864 1865 1866 1867 1868 1869 1870 1871 1872 1873 1874
1875 1876 1877 1878 1879 1880 1881 1882 1883 1884 1885
1886 1887 1889 1890 1891 1892 1893 1894 1895 1896 1897
1898 1899 1900 1901 1902 1903 1904 1905 1906 1907 1908
1909 1910 1911 1912 1913 1914 1915 1916 1917 1918 1919
1920 1921 1922 1923 1924 1925 1926 1927 1928 1929 1931
1932 1933 1934 1935 1936 1937 1938 1939 1941 1942 1943
1945 1946 1947 1948 1949 1950 1951 1952 1953 1954 1956
1957 1958 1959 1960 1961 1962 1963 1965 1966 1968 1970
1971 1972 1973 1975 1976 1978 1982 1989
(4) Configuration definition
Configuration 001
CONF 001 is applicable for all the aircraft affected by this Service Bulletin as a
standard configuration.
 
 
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
Most of the cargo compartment linings are composite sandwich panels made of a
honeycomb core bonded with a front and rear prepreg layer. They have a role in
the fire protection. The related repair procedure in the AMM advise to use material
according to CML 13XBD4. For this application code, two materials are proposed:

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Gillpatch III and Speedpatch AF800. T ests revealed that only Gillpatch III is passing the
flame penetration tests (and not Speedpatch AF800).
(2) Objective/Action
An inspection is requested to identify if any repair has been performed using Ref.
AMM T ask 25-50-00-340-803 Speed Patches (on Both Sides) Repair Method (Damage
Through) - All Cargo Compartment Linings with Honeycomb Core”, in combination with
Speedpatch AF800.
(3) Advantages
This Service Bulletin will ensure the correct fire protection function of the cargo
compartment linings.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
NOTE: The Inspection must be accomplished on all linings installed on aircraft and linings
stored in the warehouse or workshop.
T o accomplish this Service Bulletin it is necessary to:
(1) Inspection of Cargo-Compartment Linings for correct Repair Material on
Aircraft
(a) T ask set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-Compartment
Linings for correct Repair Material on Aircraft
1 Do a Detailed Inspection of the Linings in the FWD Cargo-Compartment
2 Do a Detailed Inspection of the Linings in the AFT Cargo-Compartment
3 Do a Detailed Inspection of the Linings in the Bulk Cargo-Compartment
4 Remove an Identified Lining
5 Repair the Lining (Depending on the Inspection Result)
6 Install the repaired Lining
(2) Inspection of Cargo-Compartment Linings for correct Repair Material in
Warehouse or Workshop
(a) T ask set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-Compartment
Linings for correct Repair Material in Warehouse or Workshop
1 Do a Detailed Inspection of Cargo-Compartment Linings
2 Repair the Lining (Depending on the Inspection Result)
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin must be done within 30 months from the
release date of the original issue of this ISB.
This Service Bulletin has been classified Mandatory. It is expected that an
Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA)
will be issued to confirm this classification. It is anticipated that the AD will confirm the

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(thresholds and/or intervals and/or date) given but reference should be made to the
AD for confirmation of the mandated accomplishment timescale.
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organisation Approval No. EASA.21J.031.
If an aircraft listed in the applicability 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.
(1) Inspection of Cargo-Compartment Linings for correct Repair Material on
Aircraft
(a) T ask set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-Compartment
Linings for correct Repair Material on Aircraft
PREPARATION
Job Set-up General 0.25 h
Get Access to the FWD Cargo-Compartment 0.25 h
Get Access to the AFT Cargo-Compartment 0.25 h
Get Access to the Bulk Cargo-Compartment 0.25 h
PROCEDURE
Do a Detailed Inspection of the Linings in the FWD Cargo-
Compartment
2.00 h
Do a Detailed Inspection of the Linings in the AFT Cargo-
Compartment
1.50 h
Do a Detailed Inspection of the Linings in the Bulk Cargo-
Compartment
1.50 h
Remove an Identified Lining 1.00 h
Repair the Lining (Depending on the Inspection Result) 1.00 h BENCH
Install the repaired Lining 1.00 h
PREPARATION FOR TEST
None
TEST
None
CLOSE-UP
Close Access to the Bulk Cargo-Compartment 0.25 h
Close Access to the AFT Cargo-Compartment 0.25 h
Close Access to the FWD Cargo-Compartment 0.25 h
Close-up 0.25 h
TOTAL MAN-HOURS 10.00 h

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ELAPSED TIME (HOURS) 6.00 h
NOTE: The minimum man-hours necessary to accomplish this Service Bulletin
are those for the Inspection. Depending on the inspection result,
additional man-hours can apply.
NOTE: The man-hours given above for the procedure ”Remove an Identified
Lining”, Repair the Linings (Depending on the Inspection Result)” and
“Install the Repaired Linings” are calculated for one lining only and must
be multiplied with the number of findings.
NOTE: For an explanation of the man-hours and elapsed time, refer to the
Gantt Chart given in Appendix MANPOWER GANTT CHART.
(2) Inspection of Cargo-Compartment Linings for correct Repair Material in
Warehouse or Workshop
(a) T ask set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-Compartment
Linings for correct Repair Material in Warehouse or Workshop
PREPARATION
None
PROCEDURE
Do a Detailed Inspection of Cargo-Compartment Linings 0.25 h BENCH
Repair the Lining (Depending on the Inspection Result) 1.00 h BENCH
PREPARATION FOR TEST
None
TEST
None
CLOSE-UP
None
TOTAL MAN-HOURS 1.25 h
ELAPSED TIME (HOURS) 1.25 h
NOTE: The minimum man-hours necessary to accomplish this Service Bulletin
are those for the Inspection. Depending on the inspection result,
additional man-hours can apply.
NOTE: The man-hours given above for the procedure “Do the Detailed
Inspection of Cargo-Compartment Linings” and “Repair the Linings
(Depending on the Inspection Result)” are calculated for one lining only
and must be multiplied with the number of findings.
H. WEIGHT AND BALANCE
Not changed
I. ELECTRICAL LOAD DATA
Not changed
J. REFERENCES
(1) Inspection of Cargo-Compartment Linings for correct Repair Material on
Aircraft

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(a) T ask set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-Compartment
Linings for correct Repair Material on Aircraft
AIRCRAFT MAINTENANCE MANUAL (AMM)
06-20-00, Page Block 001 06-31-53, Page Block 001
06-41-53, Page Block 001 T ask 12-34-24-860-802
T ask 25-50-00-340-803 T ask 25-52-00-210-801
T ask 25-52-00-400-801
T ask 25-53-00-000-801
T ask 25-53-00-210-801
T ask 25-53-00-400-801
T ask 25-54-00-000-801
T ask 25-54-00-210-801
T ask 25-54-00-400-801
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)
20-55-00
ILLUSTRATED PARTS CATALOG (IPC)
25-52-02 25-53-04
25-54-04
STRUCTURAL REPAIR MANUAL (SRM)
51-42-00 51-43-00
51-44-00 51-78-00
STANDARDS MANUAL (SM)
CONSUMABLE MATERIAL LIST (CML)
(2) Inspection of Cargo-Compartment Linings for correct Repair Material in
Warehouse or Workshop
(a) T ask set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-Compartment
Linings for correct Repair Material in Warehouse or Workshop
AIRCRAFT MAINTENANCE MANUAL (AMM)
06-41-53, Page Block 001 T ask 25-50-00-340-803
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)
20-55-00
STRUCTURAL REPAIR MANUAL (SRM)
51-42-00 51-43-00
51-44-00 51-78-00
STANDARDS MANUAL (SM)
CONSUMABLE MATERIAL LIST (CML)
K. PUBLICATION AFFECTED
None
L. INDUSTRY SUPPORT INFORMATION
For the accomplishment of this Service Bulletin within 30 months after the initial issue
date of the Service Bulletin, AIRBUS will share the costs by crediting the operator supplied

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standard hardware parts and man-hours needed for the repair. Claims for this allowance
should be received no later than 90 days after completion of the last affected aircraft of
your fleet.

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2. MATERIAL INFORMATION
A. MATERIAL APPLICABILITY
Material for task set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-
Compartment Linings for correct Repair Material on Aircraft
MATERIAL QTY SEE NOTES
Consumables See SB
Components See SB
Material for task set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-
Compartment Linings for correct Repair Material in Warehouse or Workshop
MATERIAL QTY SEE NOTES
Consumables See SB
Components See SB
B. TOOLING
No tools
C. CONSUMABLES
Consumables for task set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-
Compartment Linings for correct Repair Material on Aircraft
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
08BBD1 Non Aqueous Cleaner - -Isopropyl Alcohol
14SBA1 T extile - Lint free Cotton
Consumables for task set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-
Compartment Linings for correct Repair Material in Warehouse or Workshop
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
08BBD1 Non Aqueous Cleaner - -Isopropyl Alcohol
14SBA1 T extile - Lint free Cotton
D. LIST OF NEW PARTS
Components for task set A330-A-25-XX-3743-01000-93BA-A Inspection of Cargo-
Compartment Linings for correct Repair Material on Aircraft
Procurement address D4296
AIRBUS Material, Logistics and Suppliers Standard
Parts
Customer Order Fulfilment
Phone: +49 (0) 40 50 76 40 02
E-mail: Please contact your Single Point Of Contact
(SPOC)
Internet: http://spares.airbus.com or via SPEC2000
NOTE(S)
Operator supplied standard hardware parts, required to accomplish this Service
Bulletin, are to be supplied from the operator's stock.
For standard hardware the purchase order must be addressed to AIRBUS at the
address given above. Quote the number of this Service Bulletin, the MSN and, if
applicable the Retrofit Information Letter (RIL) reference.

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ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 ASNA0113-32CA(D4296) 1 WASHER (1) (2)
2 NAS1919M04S07U(D4296) 1 RIVET (1) (2)
3 NAS1919M04S08U(D4296) 1 RIVET (1) (2)
4 NAS1919M04S09U(D4296) 1 RIVET (1) (2)
NOTE(S)
Refer to the AIRBUS Ref. SM if you find part numbers of hardware components which
you cannot identify. The SM will give you the correct part number to part number
relationship.
(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
(2): The components listed above are only necessary if a repair of the lining panel(s) is/
are necessary. The quantity of these items is to be ordered as required.
Components for task set A330-A-25-XX-3743-02000-93BA-C Inspection of Cargo-
Compartment Linings for correct Repair Material in Warehouse or Workshop
Procurement address D4296
AIRBUS Material, Logistics and Suppliers Standard
Parts
Customer Order Fulfilment
Phone: +49 (0) 40 50 76 40 02
E-mail: Please contact your Single Point Of Contact
(SPOC)
Internet: http://spares.airbus.com or via SPEC2000
NOTE(S)
Operator supplied standard hardware parts, required to accomplish this Service
Bulletin, are to be supplied from the operator's stock.
For standard hardware the purchase order must be addressed to AIRBUS at the
address given above. Quote the number of this Service Bulletin, the MSN and, if
applicable the Retrofit Information Letter (RIL) reference.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 ASNA0113-32CA(D4296) 1 WASHER (1) (2)
2 NAS1919M04S07U(D4296) 1 RIVET (1) (2)
3 NAS1919M04S08U(D4296) 1 RIVET (1) (2)
4 NAS1919M04S09U(D4296) 1 RIVET (1) (2)
NOTE(S)
Refer to the AIRBUS Ref. SM if you find part numbers of hardware components which
you cannot identify. The SM will give you the correct part number to part number
relationship.
(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.

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ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
(2): The components listed above are only necessary if a repair of the lining panel(s) is/
are necessary. The quantity of these items is to be ordered as required.
E. LIST OF EXISTING PARTS
No parts

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3. ACCOMPLISHMENT INSTRUCTIONS
Task set A330-A-25-XX-3743-01000-93BA-A
Inspection of Cargo-Compartment Linings for correct Repair Material on Aircraft
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 Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given in
other documents or in other sections of the Service Bulletin. When the words “refer to”
are used and the operator has a procedure accepted by the local authority he belongs to,
the accepted alternative procedure can be used. When the words “in accordance with”
are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service Bulletin.
Operators can therefore, as deemed necessary, omit or add access and/or close-up steps
to add flexibility to their maintenance operations as long as the technical intent of the
Service Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer
to paragraph 1.J., References, for the definition of acronyms.
NOTE: The purpose of 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 is classified mandatory or expected to be classified mandatory by
an Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishment
instructions are Required for Compliance (RC) and must be done to comply with the AD.
T o allow more flexibility, the rule "refer to" and "in accordance with" will apply to these
paragraphs 3.C. and 3.E. 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: 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, including RC paragraph contained herein, contact
AIRBUS for further instructions and approval.
NOTE: Discarded parts must be managed at the operator's discretion.
A. TASK SET ASSOCIATED INFORMATION
Task Manpower

### Page 21

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 21
TOTAL MAN-HOURS 10.00 h
ELAPSED TIME (HOURS) 6.00 h
B. PREPARATION
(1) Task A330-A-25-XX-3743-01001-540A-A - Job Set-up General
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 12-34-24-860-802
Procedure
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -
Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM T ask
12-34-24-860-802.
(2) Task A330-A-25-XX-3743-02001-540A-A - Get Access to the FWD Cargo-
Compartment
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 25-52-00-210-801
Procedure
(a) Put an access platform in position below the FWD cargo-compartment door.
(b) Do the Job Set-up procedure as specified in the visual inspection of linings in the
FWD cargo-compartment, refer to Ref. AMM T ask 25-52-00-210-801.
(3) Task A330-A-25-XX-3743-03001-540A-A - Get Access to the AFT Cargo-
Compartment
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h

### Page 22

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 22
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 25-53-00-210-801
Procedure
(a) Put an access platform in position below the AFT cargo-compartment door.
(b) Do the Job Set-up procedure as specified in the visual inspection of linings in the
AFT cargo-compartment, refer to Ref. AMM T ask 25-53-00-210-801.
(4) Task A330-A-25-XX-3743-04001-540A-A - Get Access to the Bulk Cargo-
Compartment
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 25-54-00-210-801
Procedure
(a) Put an access platform in position below the bulk cargo-compartment door.
(b) Do the Job Set-up procedure as specified in the visual inspection of linings in the
bulk cargo-compartment, refer to Ref. AMM T ask 25-54-00-210-801.
C. PROCEDURE
(1) Task A330-A-25-XX-3743-01001-311A-A - Do a Detailed Inspection of the
Linings in the FWD Cargo-Compartment
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
130
Manpower/Resources/Skills
Man-hours 2.00 h
Minimum Number of person 1
Elapsed Time 2.00 h
Skills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
T ask 25-52-00-210-801
Procedure

### Page 23

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 23
(a) Standard Practices given in this procedure:
1 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.
2 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.
3 For the identification of access panels, refer to Ref. AMM 06-41-53, Page
Block 001.
(b) Do a detailed inspection of all linings made of honeycomb core (except on
door actuator linings, tarpaulin and door linings), refer to Ref. AMM T ask
25-52-00-210-801, for visible Gillpatch III or Speedpatch AF800 repair.
NOTE: If a repair patch (non-metallic) cannot be identified (writings erased or
missing), consider it is a Speedpatch AF800.
Ref. Fig. Flow Chart for Inspection of Linings on Aircraft
Ref. Fig. Inspection of Linings in the FWD Cargo-Compartment
Ref. Fig. Identification of installed Repair Patch
1 If no visible Gillpatch III or Speedpatch AF800 is installed on the related
lining:
a No further action is required for the related lining in the FWD cargo-
compartment.
2 If visible Gillpatch III or Speedpatch AF800 is installed on the related lining:
a Remove the related lining and inspect the other side for visible repair
patch, refer to Ref. T ask A330-A-25-XX-3743-01ZZZ-520Z-A.
3 Make sure that all linings have been inspected.

### Page 24

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01 SHEET 1/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 24
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
WITH HONEYCOMB CORE
VISUAL INSPECTION OF 
CARGO LINING
VISIBLE
GILLPATCH III
OR
YES
PATCH
ON BOTH SIDES
(DAMAGE THROUGH)?NONO FURTHERACTION
YES
AF800
ON AT LEAST
ONE SIDE?
YES
ACCESS TO THE
CARGO COMPARTMENT
AS PER AMM
AF800 REPAIR
PATCH?
REMOVE THE LINING
AS PER AMM
REINSTALL
THE LINING
AS PER AMM
NONO FURTHERACTION
NONO FURTHERACTION REINSTALLTHE LININGAS PER AMM
REFER TO
01 IF NON-METALLIC PATCH
CANNOT BE IDENTIFIED,
CONSIDER IT IS AF800.
01
01
SHEET 02
REFER TO
SHEET 02
ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01

### Page 25

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01 SHEET 2/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 25
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
OF RIVET HEADS
TO SYSTEMS - WIRING -
STRUCTURE
YES
ALL
LININGS
INSPECTED?
NO FURTHER
ACTION
INSTALL THE LINING
NO
  30mm ?
DISCARD AND REPLACE
THE LINING
REFER TO
NOYES
OR
IN ACCORDANCE WITH MMEL
BEFORE NEXT FLIGHT
REPAIR THE LINING
02 GENERALLY SPEAKING,
THE RIVET HEADS HAVE TO BE
AT A DISTANCE OF 30 mm MINIMUM TO ANY AIRCRAFT PART
(THIS INCLUDES ALSO PIPES, INSULATION BLANKETS, ETC.)
02
SHEET 01
REFER TO
SHEET 01
DISTANCE
OPERATE THE AC
ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01

### Page 26

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3Z-A-001-01 SHEET 1/2
REV 00 Sep 23/19 A330-25-3743Inspection of Linings in the FWD Cargo-Compartment
Page 26
CONF ALL
Z130
SIDEWALL PANELS
FR20
FR39.1
CEILING PANELS
A
PARTITION PANELS
B
INCLINED PANELS
NOTE:
ALL LININGS WITH HONEYCOMB CORE
HAVE TO BE INSPECTED.
DEPENDING ON AIRCRAFT TYPE CONFIGURATION
THE CARGO COMPARMENT LAYOUT CAN BE DIFFERENT.
A
ICN-A330-A-25XX3743-A-FAPE3-00J3Z-A-001-01

### Page 27

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J40-A-001-01 SHEET 2/2
REV 00 Sep 23/19 A330-25-3743Inspection of Linings in the FWD Cargo-Compartment
Page 27
CONF ALL
C
B EXAMPLE
CARGO SIDE
CARGO SIDE
C
NOTE:
QUANTITY AND POSITION OF REPAIR PATCH
CAN CHANGE. ICN-A330-A-25XX3743-A-FAPE3-00J40-A-001-01

### Page 28

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743Identification of installed Repair Patch
Page 28
CONF ALL
EXAMPLE
CARGO SIDE
SPEEDPATCH AF800 GILLPATCH III
CARGO SIDECARGO SIDE
NOTE:
IF REPAIR PATCHES ARE INSTALLED01
ON BOTH SIDES, CHECK THE PATCH TYP.
IF PATCH CANNOT BE IDENTIFIED,
CONSIDER IT IS SPEEDPATCH AF800.
01
REPAIR PATCH
INSTALLED ON
ONE SIDE
REPAIR PATCH
INSTALLED ON
BOTH SIDES
NOTE:
QUANTITY AND POSITION OF REPAIR PATCH
CAN CHANGE.
A
A
ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01

### Page 29

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 29
(2) Task A330-A-25-XX-3743-02001-311A-A - Do a Detailed Inspection of the
Linings in the AFT Cargo-Compartment
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
150
Manpower/Resources/Skills
Man-hours 1.50 h
Minimum Number of person 1
Elapsed Time 1.50 h
Skills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
T ask 25-53-00-210-801
Procedure
(a) Standard Practices given in this procedure:
1 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.
2 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.
3 For the identification of access panels, refer to Ref. AMM 06-41-53, Page
Block 001.
(b) Do a detailed inspection of all linings made of honeycomb core (except on door
actuator linings and door linings), refer to Ref. AMM T ask 25-53-00-210-801, for
visible Gillpatch III or Speedpatch AF800 repair.
NOTE: If a repair patch (non-metallic) cannot be identified (writings erased or
missing), consider it is a Speedpatch AF800.
Ref. Fig. Flow Chart for Inspection of Linings on Aircraft
Ref. Fig. Inspection of Linings in the AFT Cargo-Compartment
Ref. Fig. Identification of installed Repair Patch
1 If no visible Gillpatch III or Speedpatch AF800 is installed on the related
lining:
a No further action is required for the lining in the AFT cargo-
compartment.
2 If visible Gillpatch III or Speedpatch AF800 is installed on the related lining:
a Remove the related lining and inspect the other side for visible repair
patch, refer to Ref. T ask A330-A-25-XX-3743-01ZZZ-520Z-A.
3 Make sure that all linings have been inspected.

### Page 30

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01 SHEET 1/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 30
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
WITH HONEYCOMB CORE
VISUAL INSPECTION OF 
CARGO LINING
VISIBLE
GILLPATCH III
OR
YES
PATCH
ON BOTH SIDES
(DAMAGE THROUGH)?NONO FURTHERACTION
YES
AF800
ON AT LEAST
ONE SIDE?
YES
ACCESS TO THE
CARGO COMPARTMENT
AS PER AMM
AF800 REPAIR
PATCH?
REMOVE THE LINING
AS PER AMM
REINSTALL
THE LINING
AS PER AMM
NONO FURTHERACTION
NONO FURTHERACTION REINSTALLTHE LININGAS PER AMM
REFER TO
01 IF NON-METALLIC PATCH
CANNOT BE IDENTIFIED,
CONSIDER IT IS AF800.
01
01
SHEET 02
REFER TO
SHEET 02
ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01

### Page 31

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01 SHEET 2/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 31
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
OF RIVET HEADS
TO SYSTEMS - WIRING -
STRUCTURE
YES
ALL
LININGS
INSPECTED?
NO FURTHER
ACTION
INSTALL THE LINING
NO
  30mm ?
DISCARD AND REPLACE
THE LINING
REFER TO
NOYES
OR
IN ACCORDANCE WITH MMEL
BEFORE NEXT FLIGHT
REPAIR THE LINING
02 GENERALLY SPEAKING,
THE RIVET HEADS HAVE TO BE
AT A DISTANCE OF 30 mm MINIMUM TO ANY AIRCRAFT PART
(THIS INCLUDES ALSO PIPES, INSULATION BLANKETS, ETC.)
02
SHEET 01
REFER TO
SHEET 01
DISTANCE
OPERATE THE AC
ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01

### Page 32

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J41-A-001-01 SHEET 1/2
REV 00 Sep 23/19 A330-25-3743Inspection of Linings in the AFT Cargo-Compartment
Page 32
CONF ALL
FR53.2
FR66
SIDEWALL PANELS 
PARTITION PANELS
CEILING PANELS
A
Z150
B
NOTE:
ALL LININGS WITH HONEYCOMB CORE
HAVE TO BE INSPECTED.
DEPENDING ON AIRCRAFT TYPE CONFIGURATION
THE CARGO COMPARMENT LAYOUT CAN BE DIFFERENT.
INCLINED PANELS 
A
ICN-A330-A-25XX3743-A-FAPE3-00J41-A-001-01

### Page 33

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J42-A-001-01 SHEET 2/2
REV 00 Sep 23/19 A330-25-3743Inspection of Linings in the AFT Cargo-Compartment
Page 33
CONF ALL
C
B EXAMPLE
CARGO SIDE
CARGO SIDE
C
NOTE:
QUANTITY AND POSITION OF REPAIR PATCH
CAN CHANGE. ICN-A330-A-25XX3743-A-FAPE3-00J42-A-001-01

### Page 34

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743Identification of installed Repair Patch
Page 34
CONF ALL
EXAMPLE
CARGO SIDE
SPEEDPATCH AF800 GILLPATCH III
CARGO SIDECARGO SIDE
NOTE:
IF REPAIR PATCHES ARE INSTALLED01
ON BOTH SIDES, CHECK THE PATCH TYP.
IF PATCH CANNOT BE IDENTIFIED,
CONSIDER IT IS SPEEDPATCH AF800.
01
REPAIR PATCH
INSTALLED ON
ONE SIDE
REPAIR PATCH
INSTALLED ON
BOTH SIDES
NOTE:
QUANTITY AND POSITION OF REPAIR PATCH
CAN CHANGE.
A
A
ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01

### Page 35

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 35
(3) Task A330-A-25-XX-3743-03001-311A-A - Do a Detailed Inspection of the
Linings in the Bulk Cargo-Compartment
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
160
Manpower/Resources/Skills
Man-hours 1.50 h
Minimum Number of person 1
Elapsed Time 1.50 h
Skills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
T ask 25-54-00-210-801
Procedure
(a) Standard Practices given in this procedure:
1 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.
2 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.
3 For the identification of access panels, refer to Ref. AMM 06-41-53, Page
Block 001.
(b) Do a detailed inspection of all linings made of honeycomb core (except on door
linings), refer to Ref. AMM T ask 25-54-00-210-801, for visible Gillpatch III or
Speedpatch AF800 repair.
NOTE: If a repair patch (non-metallic) cannot be identified (writings erased or
missing), consider it is a Speedpatch AF800.
Ref. Fig. Flow Chart for Inspection of Linings on Aircraft
Ref. Fig. Inspection of Linings in the Bulk Cargo-Compartment
Ref. Fig. Identification of installed Repair Patch
1 If no visible Gillpatch III or Speedpatch AF800 is installed on the related
lining:
a No further action is required for the related lining in the bulk cargo-
compartment.
2 If visible Gillpatch III or Speedpatch AF800 is installed on the related lining:
a Remove the related lining and inspect the other side for visible repair
patch, refer to Ref. T ask A330-A-25-XX-3743-01ZZZ-520Z-A.
3 Make sure that all linings have been inspected.

### Page 36

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01 SHEET 1/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 36
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
WITH HONEYCOMB CORE
VISUAL INSPECTION OF 
CARGO LINING
VISIBLE
GILLPATCH III
OR
YES
PATCH
ON BOTH SIDES
(DAMAGE THROUGH)?NONO FURTHERACTION
YES
AF800
ON AT LEAST
ONE SIDE?
YES
ACCESS TO THE
CARGO COMPARTMENT
AS PER AMM
AF800 REPAIR
PATCH?
REMOVE THE LINING
AS PER AMM
REINSTALL
THE LINING
AS PER AMM
NONO FURTHERACTION
NONO FURTHERACTION REINSTALLTHE LININGAS PER AMM
REFER TO
01 IF NON-METALLIC PATCH
CANNOT BE IDENTIFIED,
CONSIDER IT IS AF800.
01
01
SHEET 02
REFER TO
SHEET 02
ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01

### Page 37

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01 SHEET 2/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 37
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
OF RIVET HEADS
TO SYSTEMS - WIRING -
STRUCTURE
YES
ALL
LININGS
INSPECTED?
NO FURTHER
ACTION
INSTALL THE LINING
NO
  30mm ?
DISCARD AND REPLACE
THE LINING
REFER TO
NOYES
OR
IN ACCORDANCE WITH MMEL
BEFORE NEXT FLIGHT
REPAIR THE LINING
02 GENERALLY SPEAKING,
THE RIVET HEADS HAVE TO BE
AT A DISTANCE OF 30 mm MINIMUM TO ANY AIRCRAFT PART
(THIS INCLUDES ALSO PIPES, INSULATION BLANKETS, ETC.)
02
SHEET 01
REFER TO
SHEET 01
DISTANCE
OPERATE THE AC
ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01

### Page 38

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3W-A-001-01 SHEET 1/2
REV 00 Sep 23/19 A330-25-3743Inspection of Linings in the Bulk Cargo-Compartment
Page 38
CONF ALL
Z160
PARTITION PANELS
FR65
FR67
FR69
FR71
FR73SIDEWALL PANELS 
CEILING PANELS
B
A
NOTE:
ALL LININGS WITH HONEYCOMB CORE
HAVE TO BE INSPECTED.
DEPENDING ON AIRCRAFT TYPE CONFIGURATION
THE CARGO COMPARMENT LAYOUT CAN BE DIFFERENT.
INCLINED PANELS
A
ICN-A330-A-25XX3743-A-FAPE3-00J3W-A-001-01

### Page 39

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3X-A-001-01 SHEET 2/2
REV 00 Sep 23/19 A330-25-3743Inspection of Linings in the Bulk Cargo-Compartment
Page 39
CONF ALL
C
B EXAMPLE
CARGO SIDE
CARGO SIDE
C
NOTE:
QUANTITY AND POSITION OF REPAIR PATCH
CAN CHANGE. ICN-A330-A-25XX3743-A-FAPE3-00J3X-A-001-01

### Page 40

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743Identification of installed Repair Patch
Page 40
CONF ALL
EXAMPLE
CARGO SIDE
SPEEDPATCH AF800 GILLPATCH III
CARGO SIDECARGO SIDE
NOTE:
IF REPAIR PATCHES ARE INSTALLED01
ON BOTH SIDES, CHECK THE PATCH TYP.
IF PATCH CANNOT BE IDENTIFIED,
CONSIDER IT IS SPEEDPATCH AF800.
01
REPAIR PATCH
INSTALLED ON
ONE SIDE
REPAIR PATCH
INSTALLED ON
BOTH SIDES
NOTE:
QUANTITY AND POSITION OF REPAIR PATCH
CAN CHANGE.
A
A
ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01

### Page 41

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 41
(4) Task A330-A-25-XX-3743-01001-520A-A - Remove an Identified Lining
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 1.00 h
Minimum Number of person 1
Elapsed Time 1.00 h
Skills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
T ask 25-52-00-400-801
T ask 25-53-00-000-801
T ask 25-53-00-400-801
T ask 25-54-00-000-801
T ask 25-54-00-400-801
Procedure
(a) Remove an identified lining and inspect the other side for visible repair patch.
1 Remove the related lining:
- For the FWD cargo-compartment, refer to Ref. AMM T ask
25-54-00-000-801.
- For the AFT cargo-compartment, refer to Ref. AMM T ask
25-53-00-000-801.
- For the bulk cargo-compartment, refer to Ref. AMM T ask
25-54-00-000-801.
a If a repair patch is installed only on one side:
<1> Re-install the related lining:
- For the FWD cargo-compartment, refer to Ref. AMM T ask
25-52-00-400-801.
- For the AFT cargo-compartment, refer to Ref. AMM T ask
25-53-00-400-801.
- For the bulk cargo-compartment, refer to Ref. AMM T ask
25-54-00-400-801.
<2> No further action is required for the related lining.
b If a repair patch is installed on both sides of the same damage area
(damage through) and none of them is a Speedpatch AF800:
<1> Re-install the related lining:
- For the FWD cargo-compartment, refer to Ref. AMM T ask
25-52-00-400-801.
- For the AFT cargo-compartment, refer to Ref. AMM T ask
25-53-00-400-801.
- For the bulk cargo-compartment, refer to Ref. AMM T ask
25-54-00-400-801.
<2> No further action is required for the related lining.

### Page 42

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 42
c If a repair patch is installed on both sides of the same damage area
(damage through) and at least one of them is a Speedpatch AF800:
<1> Repair the related lining in accordance with Ref. T ask A330-
A-25-XX-3743-01ZZZ-690Z-C.
(5) Task A330-A-25-XX-3743-01001-690A-C - Repair the Lining (Depending on the
Inspection Result)
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 1.00 h
Minimum Number of person 1
Elapsed Time 1.00 h
Skills Cabin
Material necessary to do the job
Consumables
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
08BBD1 Non Aqueous Cleaner - -Isopropyl Alcohol
14SBA1 T extile - Lint free Cotton
Components
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 ASNA0113-32CA As req. WASHER
2 NAS1919M04S07U As req. RIVET
3 NAS1919M04S08U As req. RIVET
4 NAS1919M04S09U As req. RIVET
Referenced Information
Manuals/Drawings References/Sheets
CML CONSUMABLE MATERIAL LIST (CML)
SRM
51-42-00
51-43-00
51-44-00
51-78-00
Procedure
(a) Standard Practices given in this procedure:
1 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
2 Get fastener hole diameters and drill data in accordance with Ref. SRM
51-44-00.
3 Get alternative and substitute fastener data in accordance with Ref. SRM
51-43-00.
4 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

### Page 43

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 43
addition, washers may be installed for fastener grip length in accordance
with SRM Chapter 51.
5 Do the cleaning process in accordance with Ref. SRM 51-78-00.
6 For the specification of Material application codes given in this Service
Bulletin, refer to Ref. CML.
(b) Attach the repair patches with blind rivets, refer to Ref. Fig. Attach the Repair
Patch with Blind Rivets.
1 Calculate the quantity of the necessary blind rivets for each side of the
repair patch.
2 Mark the position of the blind rivets on the visible side of the lining and
make sure that:
- Distance “E” to edges of the repair patch is 11 +/-1 mm (0.43 +/-
0.04 in.).
- Distance “D” between the marks is between 40 mm (1.57 in.) and 78
mm (3.07 in.) and has to be adapted in accordance to the used patch
size to achieve an adequate fastener hole pitch along each side.
3 Drill pilot holes at the marks through the repair patch and the lining.
4 Drill the holes to the final diameter in accordance with Ref. SRM 51-44-00.
5 Deburr the holes.
6 Clean the prepared area with:
  T extile - Lint free Cotton14SBA1  
  Non Aqueous Cleaner - -
Isopropyl Alcohol
08BBD1  
7 Make sure that the cleaned area is dry.
8 Install the rivets.
a T o the ceiling panel install:
As required RIVET NAS1919M04S07U Item 2
with
As required WASHER ASNA0113-32CA Item 1
b T o the sidewall panel and inclined panel install:
As required RIVET-BLIND NAS1919M04S08U Item 3
with
As required WASHER ASNA0113-32CA Item 1
c T o the partition panel (AFT panel in the FWD cargo-compartment and
FWD panel in the AFT cargo-compartment) install:
As required RIVET-BLIND NAS1919M04S08U Item 3
with
As required WASHER ASNA0113-32CA Item 1
d T o the partition panel (FWD panel in the FWD cargo-compartment and
AFT panel in the bulk cargo-compartment) install:
As required RIVET NAS1919M04S09U Item 4

### Page 44

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 44
with
As required WASHER ASNA0113-32CA Item 1
NOTE: If the grip length is too short, contact AIRBUS for further
instructions.
9 Clean the repaired area with:
  T extile - Lint free Cotton14SBA1  
  Non Aqueous Cleaner - -
Isopropyl Alcohol
08BBD1  
10 Make sure that the cleaned area is dry.

### Page 45

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J46-A-004-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743Attach the Repair Patch with Blind Rivets
Page 45
CONF ALL
E
E
E
E
L D
D
D = DISTANCE BETWEEN THE BLIND RIVETS
N = QUANTITY OF BLIND RIVET
L = LENGTH OF THE REPAIR PATCH
E = DISTANCE TO THE EDGE
LEGEND
NECESSARY BLIND RIVETS
FOR EACH EDGE IS:
N = L-(2xE)D +1
EXAMPLE
CARGO SIDE
A
A
BLINDRIVET
WASHER
PANEL
PATCH
CARGO SIDE
EXAMPLE
CARGO SIDE
A
A
2
3
4
1
11 ± 1mm (0.43 ± 0.04in)
BETWEEN 40mm (1.57in) AND 78mm (3.07in)
ACHIEVE AN ADEQUATE PITCH ALONG EACH SIDE
NOTE:
THE QUANTITY OF THE 
L D
D
A A
DEPENDING ON01
01
RELATED LINING
ICN-A330-A-25XX3743-A-FAPE3-00J46-A-004-01

### Page 46

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 46
(6) Task A330-A-25-XX-3743-01001-720A-A - Install the repaired Lining
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 1.00 h
Minimum Number of person 1
Elapsed Time 1.00 h
Skills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
06-41-53, Page Block 001
T ask 25-52-00-400-801
T ask 25-53-00-400-801
T ask 25-54-00-400-801
IPC
25-52-02
25-53-04
25-54-04
Procedure
(a) Standard Practices given in this procedure:
1 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.
2 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.
3 For the identification of access panels, refer to Ref. AMM 06-41-53, Page
Block 001.
(b) T emporarily attach the repaired lining and check the distance of the installed
blind rived heads to the systems, wiring or structure of the aircraft, refer to Ref.
Fig. Flow Chart for Inspection of Linings on Aircraft.
1 If the dimension is less than 30 mm (1.81 in.):
a Discard the related lining.
b Order a new lining through the common channel.
<1> For the FWD cargo-compartment, refer to Ref. IPC 25-52-02.
<2> For the AFT cargo-compartment, refer to Ref. IPC 25-53-04.
<3> For the bulk cargo-compartment, refer to Ref. IPC 25-54-04.
c Install the new lining:
<1> For the FWD cargo-compartment, refer to Ref. AMM T ask
25-52-00-400-801.
<2> For the AFT cargo-compartment, refer to Ref. AMM T ask
25-53-00-400-801.
<3> For the bulk cargo-compartment, refer to Ref. AMM T ask
25-54-00-400-801.
2 If the dimension is equal to or more than 30 mm (1.81 in.):

### Page 47

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 47
a Install the related lining:
<1> For the FWD cargo-compartment, refer to Ref. AMM T ask
25-52-00-400-801.
<2> For the AFT cargo-compartment, refer to Ref. AMM T ask
25-53-00-400-801.
<3> For the bulk cargo-compartment, refer to Ref. AMM T ask
25-54-00-400-801.
(c) Make sure that all linings have been inspected.
1 If a lining is not inspected:
a Do the inspection of the related lining, refer to Ref. T ask A330-A-25-
XX-3743-01ZZZ-311Z-A or Ref. T ask A330-A-25-XX-3743-02ZZZ-311Z-
A or Ref. T ask A330-A-25-XX-3743-03ZZZ-311Z-A.
2 If all linings are inspected:
a No further action is required.

### Page 48

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01 SHEET 1/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 48
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
WITH HONEYCOMB CORE
VISUAL INSPECTION OF 
CARGO LINING
VISIBLE
GILLPATCH III
OR
YES
PATCH
ON BOTH SIDES
(DAMAGE THROUGH)?NONO FURTHERACTION
YES
AF800
ON AT LEAST
ONE SIDE?
YES
ACCESS TO THE
CARGO COMPARTMENT
AS PER AMM
AF800 REPAIR
PATCH?
REMOVE THE LINING
AS PER AMM
REINSTALL
THE LINING
AS PER AMM
NONO FURTHERACTION
NONO FURTHERACTION REINSTALLTHE LININGAS PER AMM
REFER TO
01 IF NON-METALLIC PATCH
CANNOT BE IDENTIFIED,
CONSIDER IT IS AF800.
01
01
SHEET 02
REFER TO
SHEET 02
ICN-A330-A-25XX3743-A-FAPE3-00J44-A-003-01

### Page 49

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01 SHEET 2/2
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inspection of Linings on aircraft
Page 49
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
OF RIVET HEADS
TO SYSTEMS - WIRING -
STRUCTURE
YES
ALL
LININGS
INSPECTED?
NO FURTHER
ACTION
INSTALL THE LINING
NO
  30mm ?
DISCARD AND REPLACE
THE LINING
REFER TO
NOYES
OR
IN ACCORDANCE WITH MMEL
BEFORE NEXT FLIGHT
REPAIR THE LINING
02 GENERALLY SPEAKING,
THE RIVET HEADS HAVE TO BE
AT A DISTANCE OF 30 mm MINIMUM TO ANY AIRCRAFT PART
(THIS INCLUDES ALSO PIPES, INSULATION BLANKETS, ETC.)
02
SHEET 01
REFER TO
SHEET 01
DISTANCE
OPERATE THE AC
ICN-A330-A-25XX3743-A-FAPE3-00J45-A-005-01

### Page 50

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 50
D. PREPARATION FOR TEST
None
E. TEST
None
F. CLOSE-UP
(1) Task A330-A-25-XX-3743-02001-740A-A - Close Access to the Bulk Cargo-
Compartment
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 25-54-00-210-801
Procedure
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the Close-up procedure as specified in the visual inspection of linings in the
bulk cargo-compartment, refer to Ref. AMM T ask 25-54-00-210-801.
(c) Remove the access platform.
(2) Task A330-A-25-XX-3743-03001-740A-A - Close Access to the AFT Cargo-
Compartment
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 25-53-00-210-801
Procedure
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the Close-up procedure as specified in the visual inspection of linings in the
AFT cargo-compartment, refer to Ref. AMM T ask 25-53-00-210-801.

### Page 51

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 51
(c) Remove the access platform.
(3) Task A330-A-25-XX-3743-04001-740A-A - Close Access to the FWD Cargo-
Compartment
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 25-52-00-210-801
Procedure
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the Close-up procedure as specified in the visual inspection of linings in the
FWD cargo-compartment, refer to Ref. AMM T ask 25-52-00-210-801.
(c) Remove the access platform.
(4) Task A330-A-25-XX-3743-01001-740A-A - Close-up
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Procedure
(a) Put the aircraft back to its initial configuration.
G. ADMINISTRATIVE
(1) Task A330-A-25-XX-3743-01001-90AA-A - Administrative
Procedure
Confirm in the applicable aircraft records that you have completed all the work defined
in this Service Bulletin task set as required.

### Page 52

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 52
Task set A330-A-25-XX-3743-02000-93BA-C
Inspection of Cargo-Compartment Linings for correct Repair Material in Warehouse or Workshop
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 Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given in
other documents or in other sections of the Service Bulletin. When the words “refer to”
are used and the operator has a procedure accepted by the local authority he belongs to,
the accepted alternative procedure can be used. When the words “in accordance with”
are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service Bulletin.
Operators can therefore, as deemed necessary, omit or add access and/or close-up steps
to add flexibility to their maintenance operations as long as the technical intent of the
Service Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer
to paragraph 1.J., References, for the definition of acronyms.
NOTE: The purpose of 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 is classified mandatory or expected to be classified mandatory by
an Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishment
instructions are Required for Compliance (RC) and must be done to comply with the AD.
T o allow more flexibility, the rule "refer to" and "in accordance with" will apply to these
paragraphs 3.C. and 3.E. 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: 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, including RC paragraph contained herein, contact
AIRBUS for further instructions and approval.
NOTE: Discarded parts must be managed at the operator's discretion.
A. TASK SET ASSOCIATED INFORMATION
Task Manpower
TOTAL MAN-HOURS 1.25 h

### Page 53

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 53
ELAPSED TIME (HOURS) 1.25 h
B. PREPARATION
None
C. PROCEDURE
(1) Task A330-A-25-XX-3743-04001-311A-C - Do a Detailed Inspection of Cargo-
Compartment Linings
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-41-53, Page Block 001
Procedure
(a) Standard Practices given in this procedure:
1 For the identification of access panels, refer to Ref. AMM 06-41-53, Page
Block 001.
(b) Do a detailed inspection on both sides of all linings made of honeycomb core
(except on door actuators, tarpaulins and door linings) for visible Gillpatch III or
Speedpatch AF800 repair.
NOTE: If a repair patch (non-metallic) cannot be identified (writings erased or
missing), consider it is a Speedpatch AF800.
Ref. Fig. Flow Chart for Inspection of Linings in Warehouse or Workshop
Ref. Fig. Identification of installed Repair Patch
1 If no non-metallic repair patch is installed on the lining:
a No further action is required.
2 If a non-metallic repair patch is installed on only one side of the lining:
a No further action is required.
3 If a repair patch is installed on both sides of the same damage area
(damage through):
a Identify the installed repair material.
<1> If none of them is a Speedpatch AF800:
<a> No further action is required.
<2> If at least one of them is a Speedpatch AF800:
<a> Repair the related lining in accordance with Ref. T ask
A330-A-25-XX-3743-02ZZZ-690Z-C.
4 Make sure that all linings have been inspected.

### Page 54

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J43-A-003-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743Flow Chart for Inpection of Linings in warehouse or workshop
Page 54
CONF ALL
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.
FOR THE COMPLIANCE TIMES, REFER TO THE
ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).
VISUAL INSPECTION OF
CARGO LINING (BOTH SIDES)
NON-
METALLIC
PATCH?
YES
PATCH
ON BOTH SIDES
(DAMAGE THROUGH)?NONO FURTHERACTION
YES
AF800
ON AT LEAST
ONE SIDE?
YES
NONO FURTHERACTION
NONO FURTHERACTION
01 IF NON-METALLIC PATCH
CANNOT BE IDENTIFIED,
CONSIDER IT IS AF800.
01
REPAIR THE LINING (RIVETS).
ATTACH A LABEL TO THE LINING,
ASKING TO CHECK AT NEXT
INSTALLATION THAT DISTANCE
TO ANY AIRCRAFT PART IS
   30 mm
(IF <30 mm, PANEL TO BE
DISCARDED AND REPLACED)
02 GENERALLY SPEAKING
THE RIVET HEADS HAVE TO BE
AT A DISTANCE OF 30 mm MINIMUM TO ANY AIRCRAFT PART
(THIS INCLUDES ALSO PIPES, INSULATION BLANKETS, ETC.)
02
OF RIVET HEADS
ICN-A330-A-25XX3743-A-FAPE3-00J43-A-003-01

### Page 55

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743Identification of installed Repair Patch
Page 55
CONF ALL
EXAMPLE
CARGO SIDE
SPEEDPATCH AF800 GILLPATCH III
CARGO SIDECARGO SIDE
NOTE:
IF REPAIR PATCHES ARE INSTALLED01
ON BOTH SIDES, CHECK THE PATCH TYP.
IF PATCH CANNOT BE IDENTIFIED,
CONSIDER IT IS SPEEDPATCH AF800.
01
REPAIR PATCH
INSTALLED ON
ONE SIDE
REPAIR PATCH
INSTALLED ON
BOTH SIDES
NOTE:
QUANTITY AND POSITION OF REPAIR PATCH
CAN CHANGE.
A
A
ICN-A330-A-25XX3743-A-FAPE3-00J3V-A-003-01

### Page 56

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 56
(2) Task A330-A-25-XX-3743-02001-690A-C - Repair the Lining (Depending on the
Inspection Result)
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 1.00 h
Minimum Number of person 1
Elapsed Time 1.00 h
Material necessary to do the job
Consumables
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
08BBD1 Non Aqueous Cleaner - -Isopropyl Alcohol
14SBA1 T extile - Lint free Cotton
Components
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 ASNA0113-32CA As req. WASHER
2 NAS1919M04S07U As req. RIVET
3 NAS1919M04S08U As req. RIVET
4 NAS1919M04S09U As req. RIVET
Referenced Information
Manuals/Drawings References/Sheets
CML CONSUMABLE MATERIAL LIST (CML)
SRM
51-42-00
51-43-00
51-44-00
51-78-00
Procedure
(a) Standard Practices given in this procedure:
1 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
2 Get fastener hole diameters and drill data in accordance with Ref. SRM
51-44-00.
3 Get alternative and substitute fastener data in accordance with Ref. SRM
51-43-00.
4 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.
5 Do the cleaning process in accordance with Ref. SRM 51-78-00.
6 For the specification of Material application codes given in this Service
Bulletin, refer to Ref. CML.

### Page 57

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 57
(b) Attach the repair patches with blind rivets, refer to Ref. Fig. Attach the Repair
Patch with Blind Rivets.
1 Calculate the quantity of the necessary blind rivets for each side of the
repair patch.
2 Mark the position of the blind rivets on the visible side of the lining and
make sure that:
- Distance “E” to edges of the repair patch is 11 +/-1 mm (0.43 +/-
0.04 in.).
- Distance “D” between the marks is between 40 mm (1.57 in.) and 78
mm (3.07 in.) and has to be adapted in accordance to the used patch
size to achieve an adequate fastener hole pitch along each side.
3 Drill pilot holes at the marks through the repair patch and the lining.
4 Drill the holes to the final diameter in accordance with Ref. SRM 51-44-00.
5 Deburr the holes.
6 Clean the prepared area with:
  T extile - Lint free Cotton14SBA1  
  Non Aqueous Cleaner - -
Isopropyl Alcohol
08BBD1  
7 Make sure that the cleaned area is dry.
8 Install the rivets.
a T o the ceiling panel, install:
As required RIVET NAS1919M04S07U Item 2
with
As required WASHER ASNA0113-32CA Item 1
b T o the sidewall panel and inclined panel install:
As required RIVET-BLIND NAS1919M04S08U Item 3
with
As required WASHER ASNA0113-32CA Item 1
c T o the partition panel (AFT panel in the FWD cargo-compartment and
FWD panel in the AFT cargo-compartment) install:
As required RIVET-BLIND NAS1919M04S08U Item 3
with
As required WASHER ASNA0113-32CA Item 1
d T o the partition panel (FWD panel in the FWD cargo-compartment and
AFT panel in the bulk cargo-compartment) install:
As required RIVET NAS1919M04S09U Item 4
with
As required WASHER ASNA0113-32CA Item 1
NOTE: If the grip length is too short, contact AIRBUS for further
instructions.

### Page 58

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 58
9 Clean the repaired area with:
  T extile - Lint free Cotton14SBA1  
  Non Aqueous Cleaner - -
Isopropyl Alcohol
08BBD1  
10 Make sure that the cleaned area is dry.
(c) Attach a label to the related lining asking to check at next installation that the
distance between the blind rivet heads to the systems, wiring or structure of the
aircraft is equal to or more than 30 mm (1.81 in.). If the distance is less than 30
mm (1.81 in.), the lining should be discarded and replaced.

### Page 59

A330
SERVICE BULLETIN
Figure ICN-A330-A-25XX3743-A-FAPE3-00J46-A-004-01 SHEET 1/1
REV 00 Sep 23/19 A330-25-3743Attach the Repair Patch with Blind Rivets
Page 59
CONF ALL
E
E
E
E
L D
D
D = DISTANCE BETWEEN THE BLIND RIVETS
N = QUANTITY OF BLIND RIVET
L = LENGTH OF THE REPAIR PATCH
E = DISTANCE TO THE EDGE
LEGEND
NECESSARY BLIND RIVETS
FOR EACH EDGE IS:
N = L-(2xE)D +1
EXAMPLE
CARGO SIDE
A
A
BLINDRIVET
WASHER
PANEL
PATCH
CARGO SIDE
EXAMPLE
CARGO SIDE
A
A
2
3
4
1
11 ± 1mm (0.43 ± 0.04in)
BETWEEN 40mm (1.57in) AND 78mm (3.07in)
ACHIEVE AN ADEQUATE PITCH ALONG EACH SIDE
NOTE:
THE QUANTITY OF THE 
L D
D
A A
DEPENDING ON01
01
RELATED LINING
ICN-A330-A-25XX3743-A-FAPE3-00J46-A-004-01

### Page 60

A330
SERVICE BULLETIN
REV 00 Sep 23/19 A330-25-3743
Page 60
D. PREPARATION FOR TEST
None
E. TEST
None
F. CLOSE-UP
None
G. ADMINISTRATIVE
(1) Task A330-A-25-XX-3743-02001-90AA-C - Administrative
Procedure
Confirm in the applicable aircraft records that you have completed all the work defined
in this Service Bulletin task set as required.

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