# Airbus Service Bulletin A330-71-3042

Copy: No revision named ("Airbus SB A330-71-3042 original issue dated 01 April 2025"), 36 pages: PDF https://openairdocs.org/files/sha256/af/c4/afc4c1c77b4cdd5fa0d5304588f8c3ed39999e268447838ab3ffcb3baba41b59; text https://openairdocs.org/service-documents/airbus/a330-71-3042/file/afc4c1c77b4c.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2026-7201, the docket of AD 2026-18-09. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-71-3042
- Page: https://openairdocs.org/service-documents/airbus/a330-71-3042

## Text (36 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2026-7201, the docket of AD 2026-18-09. 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 Apr 01/25 A330-71-3042
Page 1
CONF ALL
AIRBUS
2, ROND POINT EMILE DEWOITINE
31700 BLAGNAC
FRANCE
 
The content of this document is the property of Airbus. All rights including copyrights are reserved.
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: 71
TITLE: POWER PLANT - AIR INLET - INSPECTION OF AIR INTAKE NOSE COWL
ASSEMBLY NACELLE ANTI-ICE FEED PIPE AND RESTRAINT BRACKETS
MODIFICATION No.:
None

### Page 2

A330
SERVICE BULLETIN
SUMMARY
REV 00 Apr 01/25 A330-71-3042
Page 2
ATA SYSTEM: 71
TITLE: POWER PLANT - AIR INLET - INSPECTION OF AIR INTAKE NOSE COWL
ASSEMBLY NACELLE ANTI-ICE FEED PIPE AND RESTRAINT BRACKETS
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
A number of nacelle inlet thermal anti-ice systems inspected during normal
maintenance activities have been found with cracked or broken thermal anti-ice
piccolo tube restraint brackets. The restraint brackets act as a precautionary measure
to prevent disengagement of the thermal anti-ice spray ring from the thermal anti-ice
feed pipe in specific conditions. Broken or cracked restraint brackets can contribute
to a thermal anti-ice feed pipe disengagement and decrease the effectiveness of the
thermal anti-ice system and allow ice build-up on the inlet lip skin that could result in
damage to the engine.
Additionally, some Air Inlets may have active temporary repairs (SRM FRSZ026) which
are no longer recommended.
NOTE: “Active” is used in this document to describe the embodiment status of the
SRM repair FRSZ026. “Active” means that the temporary repair FRSZ026 has
been applied (the restraint brackets have been removed) and the restraint
brackets have not been replaced or permanently repaired.
(2) Objective/Action
This Service Bulletin is published to advise all operators of A330 aircraft equipped
with ROLLS-ROYCE Trent 700 engines of the issue of ROLLS-ROYCE Service Bulletin
No. RB211-71-AL136 which instruct an inspection of the affected area and includes
acceptance limits, repair actions.
(3) Advantages
Accomplishment of this Service Bulletin provide actions in case of disengagement of
the thermal anti-ice spray ring from the thermal anti-ice feed pipe which could result
in damage to the engine from ice build-up.
(4) Operational/Maintenance Consequences
None
C. GENERAL EVALUATION

### Page 3

A330
SERVICE BULLETIN
SUMMARY
REV 00 Apr 01/25 A330-71-3042
Page 3
EVALUATION TABLE
COMPLIANCE MANDATORY COST SAVING NO
A/C OPERATION
AFFECTED
NO VENDOR SB YES
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.
D. MAINTENANCE CONFIGURATION
No specific aircraft maintenance configuration required.
E. MATERIAL PRICE INFORMATION
(1) Inspection
(a) T ask set A330-A-71-XX-3042-01000-93BA-A Inspection
No material
F. APPLICABILITY
This Service Bulletin is applicable to this (these) operator(s):
01D 09K 12P 14F 15S 15T 23R 28M 32D 36V 39K 51X 56S 57L 58J 68M 70M 73H 79E 79L
82J 82M 83Q 83V 89G 91J 94M 96U 98W 99Y AAL ABB ABR ACA AFL AHK AIB ALK ARG ASL
AVA AWC AZU BCS BEC BEL BGA BNL BOV BRS BTK CAO CBJ CCA CES CFC CHH CMA CPA
CRK CRL CSC CSN CSZ DBP DGA DLH EVE F1I F2I FAF FJI GCR GIA GJW GTR H8O HAL HFM
HKC HUA HYS I5S IBE IRA JAV KAY KNE KZU LKE LNI LSY LYX M6D MAA MAU MEA MFX MMF
MNB MSR MXD NCR NWS OCN OHY OMA OYA PAL PLM PVG QNT QTR RNA RSY RWD SAA SAF
SAS SMF SVA SWR TAH TAR TBA THA THY TNO TOW TPA TSC TSK TUA TWB UAE UAF UBG
VIR VJC VKG WFL WPT XAX
G. CONCURRENT REQUIREMENTS
None
H. NATURE OF THE WORK
(1) Inspection
(a) T ask set A330-A-71-XX-3042-01000-93BA-A Inspection
AIRCRAFT NO
EQUIPMENT YES
I. MANPOWER
(1) Inspection
(a) T ask set A330-A-71-XX-3042-01000-93BA-A Inspection
MANPOWER
TOTAL MAN-HOURS 1.25 h
ELAPSED TIME (HOURS) 1.25 h
Additional man-hours related to Vendor SB; refer to:

### Page 4

A330
SERVICE BULLETIN
SUMMARY
REV 00 Apr 01/25 A330-71-3042
Page 4
MANPOWER
Do a SDI of the Thermal Anti-Ice Spray
Ring Feed Pipe and Restraint Brackets
for Engine 1
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-AL136
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-K923
Do a SDI of the Thermal Anti-Ice Spray
Ring Feed Pipe and Restraint Brackets
for Engine 2
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-AL136
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-K923

### Page 5

A330
SERVICE BULLETIN
SUMMARY
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8I-A-001-01 Fig.SA Sol.AA SHEET 1/2
REV 00 Apr 01/25 A330-71-3042General Overview
Page 5
J. GENERAL OVERVIEW
CONF ALL
A
A Z411 (Z421)
B
Z410
Z420
A
B
C
ICN-A330-A-71XX3042-A-FAPE3-01L8I-A-001-01

### Page 6

A330
SERVICE BULLETIN
SUMMARY
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8J-A-001-01 Fig.SA Sol.AA SHEET 2/2
REV 00 Apr 01/25 A330-71-3042General Overview
Page 6
CONF ALL
C
PICCOLO TUBE
AREA OF INSPECTION
ICN-A330-A-71XX3042-A-FAPE3-01L8J-A-001-01

### Page 7

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 7
ATA SYSTEM: 71
TITLE: POWER PLANT - AIR INLET - INSPECTION OF AIR INTAKE NOSE COWL
ASSEMBLY NACELLE ANTI-ICE FEED PIPE AND RESTRAINT BRACKETS
1. PLANNING INFORMATION
A. APPLICABILITY
NOTE: This Service Bulletin is only applicable to aircraft equipped with engine TRENT 700
engines.
NOTE: This Service Bulletin is only applicable to aircraft on which MOD No. 204615S32667
(Service Bulletin No. 71-3032) is embodied and MOD No. 210288S35892 is not
embodied.
(1) Models
ON A/C 0250, 0251, 0254, 0261, 0265, 0266, 0271, 0276, 0281, 0283, 0285-0287, 0295,
0301, 0309, 0311, 0313, 0314, 0316, 0320, 0334, 0340, 0345, 0348, 0365, 0369, 0372,
0382, 0384, 0396, 0398, 0401, 0409, 0427, 0437, 0451, 0452, 0455, 0456, 0461, 0462,
0480, 0491, 0494, 0501, 0505, 0509, 0518, 0525-0527, 0529, 0532, 0536, 0597, 0600, 0610,
0625, 0627, 0632, 0635, 0649, 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, 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, 1998, 2007, 2008, 2011, 2012, 2015, 2022, 2023, 2030,
2036, 2043
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 0138, 0140, 0144, 0148, 0153, 0165
330-341
ON A/C 0083, 0102, 0111, 0132, 0177, 0244, 0669, 0673, 0776, 0850, 0855, 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, 0679, 0687,
0692, 0701, 0713, 0716, 0720, 0741, 0773, 0777, 0781, 0782, 0786, 0791, 0830, 0833,

### Page 8

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 8
0836, 0851, 0862, 0866, 0879, 0889, 0895, 0896, 0905, 0908, 0913, 0915, 0922, 0928,
0935-0937, 0942, 0952, 0954, 0958, 0959, 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, 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, 1831-1833, 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 1824, 1853, 1930, 1985, 2027, 2041
330-743L
CONF ALL
(2) Applicability by MSN
0083 0102 0111 0132 0138 0140 0144 0148 0153 0165 0177 0244 0250 0251 0254
0261 0265 0266 0271 0276 0277 0279 0281 0283-0287 0295 0301 0309 0311 0313
0314 0316 0320 0334 0340 0344 0345 0348 0349 0356 0357 0365 0369 0372 0382
0384 0386 0389 0393 0396 0398 0400 0401 0405 0407-0409 0412 0418-0421 0423
0427 0437 0439 0451 0452 0455 0456 0461 0462 0479 0480 0491 0494 0496 0497
0501 0505 0509 0512 0515 0518 0525-0527 0529 0532 0536 0539 0548 0565 0568
0570 0576 0579 0581 0597 0600 0610 0625 0627 0629 0632 0635 0636 0642 0645
0648 0649 0654 0656 0658 0662 0664 0666 0669 0670 0673 0679 0683 0687 0688
0692 0696 0701 0709 0713 0716 0717 0720 0724 0726 0728-0730 0732 0735 0737
0741 0750 0751 0756 0759 0773 0776 0777 0780-0782 0785 0786 0788 0791 0795
0797 0807 0809 0810 0815 0818 0821 0824 0830 0832 0833 0836 0839 0840 0850-
0852 0854 0855 0860 0862 0863 0866-0868 0873 0875 0879 0881 0884 0889 0890
0895 0896 0903 0905 0906 0908 0909 0913 0915 0916 0919 0922 0926 0928 0930
0935-0937 0941 0942 0944 0948 0952 0954 0957-0959 0963 0964 0966 0967 0971
0973-0975 0978 0982-0984 0986 0988-0992 0995 0997 0998 1000 1003 1004 1006
1008-1012 1014-1016 1018 1020 1022 1026 1028 1029 1032 1033 1035 1037 1038
1041 1044-1049 1051-1053 1058 1060 1062 1063 1065 1066 1069-1077 1080-1082
1084-1087 1089 1090 1092 1093 1095 1097-1101 1103-1105 1107 1108 1110 1114
1115 1120 1124 1126 1127 1130-1132 1137 1138 1141 1143 1145-1147 1149 1150
1153 1156 1157 1159 1160 1163 1165 1167 1168 1170-1172 1175 1178 1181 1184
1186-1193 1195 1196 1199 1201 1204-1206 1208 1210 1212 1214-1217 1222-1224
1226-1228 1230-1232 1236-1241 1245-1250 1255 1259-1264 1267 1269-1271 1275-
1277 1279 1280 1282 1284-1286 1288-1293 1295 1296 1298 1299 1301-1307 1310-
1312 1314-1317 1319 1320 1322-1325 1328-1334 1338 1341-1345 1348-1350 1352
1353 1355-1359 1362-1364 1366 1368 1369 1371-1376 1378 1380 1382-1384 1386
1387 1389 1390 1394 1396-1404 1406-1411 1413-1423 1427-1429 1432-1434 1436

### Page 9

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 9
1438-1449 1451-1457 1459-1463 1465-1469 1471 1473-1475 1477 1479-1486 1488
1491-1493 1495-1498 1500 1502-1504 1506 1508-1513 1517 1520 1521 1523-1528
1530-1534 1537 1538 1540-1542 1544-1555 1557-1570 1572-1574 1577-1579 1581-
1589 1591 1592 1594-1604 1606-1610 1612 1614 1615 1617-1619 1621 1624 1626
1631-1635 1639 1641 1643 1646 1648 1650 1651 1653-1660 1662-1678 1680 1681
1685-1689 1691-1693 1695 1697 1698 1703 1708 1709 1711 1712 1715 1722-1726
1729-1735 1738 1739 1741 1743 1745 1746 1749-1754 1756-1759 1762-1766 1768
1770-1775 1779-1782 1785-1790 1792 1796-1805 1807-1812 1814-1816 1818 1820-
1833 1837-1843 1845-1849 1851-1853 1855-1860 1862 1863 1865-1869 1871-1875
1878-1881 1883 1885 1886 1889 1891 1893 1894 1896 1898 1899 1902 1905 1907
1911 1912 1916 1917 1919 1928 1930 1942 1945 1960 1965 1968 1982 1985 1989
1998 2007 2008 2011 2012 2015 2022 2023 2027 2030 2036 2041 2043
(3) MSN by configuration
MSN CONFIGURATION
0083 0102 0111 0132 0138 0140 0144 0148 0153 0165 0177
0244 0250 0251 0254 0261 0265 0266 0271 0276 0277 0279
0281 0283 0284 0285 0286 0287 0295 0301 0309 0311 0313
0314 0316 0320 0334 0340 0344 0345 0348 0349 0356 0357
0365 0369 0372 0382 0384 0386 0389 0393 0396 0398 0400
0401 0405 0407 0408 0409 0412 0418 0419 0420 0421 0423
0427 0437 0439 0451 0452 0455 0456 0461 0462 0479 0480
0491 0494 0496 0497 0501 0505 0509 0512 0515 0518 0525
0526 0527 0529 0532 0536 0539 0548 0565 0568 0570 0576
0579 0581 0597 0600 0610 0625 0627 0629 0632 0635 0636
0642 0645 0648 0649 0654 0656 0658 0662 0664 0666 0669
0670 0673 0679 0683 0687 0688 0692 0696 0701 0709 0713
0716 0717 0720 0724 0726 0728 0729 0730 0732 0735 0737
0741 0750 0751 0756 0759 0773 0776 0777 0780 0781 0782
0785 0786 0788 0791 0795 0797 0807 0809 0810 0815 0818
0821 0824 0830 0832 0833 0836 0839 0840 0850 0851 0852
0854 0855 0860 0862 0863 0866 0867 0868 0873 0875 0879
0881 0884 0889 0890 0895 0896 0903 0905 0906 0908 0909
0913 0915 0916 0919 0922 0926 0928 0930 0935 0936 0937
0941 0942 0944 0948 0952 0954 0957 0958 0959 0963 0964
0966 0967 0971 0973 0974 0975 0978 0982 0983 0984 0986
0988 0989 0990 0991 0992 0995 0997 0998 1000 1003 1004
1006 1008 1009 1010 1011 1012 1014 1015 1016 1018 1020
1022 1026 1028 1029 1032 1033 1035 1037 1038 1041 1044
1045 1046 1047 1048 1049 1051 1052 1053 1058 1060 1062
1063 1065 1066 1069 1070 1071 1072 1073 1074 1075 1076
1077 1080 1081 1082 1084 1085 1086 1087 1089 1090 1092
1093 1095 1097 1098 1099 1100 1101 1103 1104 1105 1107
1108 1110 1114 1115 1120 1124 1126 1127 1130 1131 1132
1137 1138 1141 1143 1145 1146 1147 1149 1150 1153 1156
1157 1159 1160 1163 1165 1167 1168 1170 1171 1172 1175
1178 1181 1184 1186 1187 1188 1189 1190 1191 1192 1193
1195 1196 1199 1201 1204 1205 1206 1208 1210 1212 1214
1215 1216 1217 1222 1223 1224 1226 1227 1228 1230 1231
1232 1236 1237 1238 1239 1240 1241 1245 1246 1247 1248
1249 1250 1255 1259 1260 1261 1262 1263 1264 1267 1269
1270 1271 1275 1276 1277 1279 1280 1282 1284 1285 1286
1288 1289 1290 1291 1292 1293 1295 1296 1298 1299 1301
1302 1303 1304 1305 1306 1307 1310 1311 1312 1314 1315
1316 1317 1319 1320 1322 1323 1324 1325 1328 1329 1330
001

### Page 10

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 10
MSN CONFIGURATION
1331 1332 1333 1334 1338 1341 1342 1343 1344 1345 1348
1349 1350 1352 1353 1355 1356 1357 1358 1359 1362 1363
1364 1366 1368 1369 1371 1372 1373 1374 1375 1376 1378
1380 1382 1383 1384 1386 1387 1389 1390 1394 1396 1397
1398 1399 1400 1401 1402 1403 1404 1406 1407 1408 1409
1410 1411 1413 1414 1415 1416 1417 1418 1419 1420 1421
1422 1423 1427 1428 1429 1432 1433 1434 1436 1438 1439
1440 1441 1442 1443 1444 1445 1446 1447 1448 1449 1451
1452 1453 1454 1455 1456 1457 1459 1460 1461 1462 1463
1465 1466 1467 1468 1469 1471 1473 1474 1475 1477 1479
1480 1481 1482 1483 1484 1485 1486 1488 1491 1492 1493
1495 1496 1497 1498 1500 1502 1503 1504 1506 1508 1509
1510 1511 1512 1513 1517 1520 1521 1523 1524 1525 1526
1527 1528 1530 1531 1532 1533 1534 1537 1538 1540 1541
1542 1544 1545 1546 1547 1548 1549 1550 1551 1552 1553
1554 1555 1557 1558 1559 1560 1561 1562 1563 1564 1565
1566 1567 1568 1569 1570 1572 1573 1574 1577 1578 1579
1581 1582 1583 1584 1585 1586 1587 1588 1589 1591 1592
1594 1595 1596 1597 1598 1599 1600 1601 1602 1603 1604
1606 1607 1608 1609 1610 1612 1614 1615 1617 1618 1619
1621 1624 1626 1631 1632 1633 1634 1635 1639 1641 1643
1646 1648 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 1680 1681 1685 1686
1687 1688 1689 1691 1692 1693 1695 1697 1698 1703 1708
1709 1711 1712 1715 1722 1723 1724 1725 1726 1729 1730
1731 1732 1733 1734 1735 1738 1739 1741 1743 1745 1746
1749 1750 1751 1752 1753 1754 1756 1757 1758 1759 1762
1763 1764 1765 1766 1768 1770 1771 1772 1773 1774 1775
1779 1780 1781 1782 1785 1786 1787 1788 1789 1790 1792
1796 1797 1798 1799 1800 1801 1802 1803 1804 1805 1807
1808 1809 1810 1811 1812 1814 1815 1816 1818 1820 1821
1822 1823 1824 1825 1826 1827 1828 1829 1830 1831 1832
1833 1837 1838 1839 1840 1841 1842 1843 1845 1846 1847
1848 1849 1851 1852 1853 1855 1856 1857 1858 1859 1860
1862 1863 1865 1866 1867 1868 1869 1871 1872 1873 1874
1875 1878 1879 1880 1881 1883 1885 1886 1889 1891 1893
1894 1896 1898 1899 1902 1905 1907 1911 1912 1916 1917
1919 1928 1930 1942 1945 1960 1965 1968 1982 1985 1989
1998 2007 2008 2011 2012 2015 2022 2023 2027 2030 2036
2041 2043
(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

### Page 11

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 11
(1) History
A number of nacelle inlet thermal anti-ice systems inspected during normal
maintenance activities have been found with cracked or broken thermal anti-ice
piccolo tube restraint brackets. The restraint brackets act as a precautionary measure
to prevent disengagement of the thermal anti-ice spray ring from the thermal anti-ice
feed pipe in specific conditions. Broken or cracked restraint brackets can contribute
to a thermal anti-ice feed pipe disengagement and decrease the effectiveness of the
thermal anti-ice system and allow ice build-up on the inlet lip skin that could result in
damage to the engine.
Additionally, some Air Inlets may have active temporary repairs (SRM FRSZ026) which
are no longer recommended.
NOTE: “Active” is used in this document to describe the embodiment status of the
SRM repair FRSZ026. “Active” means that the temporary repair FRSZ026 has
been applied (the restraint brackets have been removed) and the restraint
brackets have not been replaced or permanently repaired.
(2) Objective/Action
This Service Bulletin is published to advise all operators of A330 aircraft equipped
with ROLLS-ROYCE Trent 700 engines of the issue of ROLLS-ROYCE Service Bulletin
No. RB211-71-AL136 which instruct an inspection of the affected area and includes
acceptance limits, repair actions.
(3) Advantages
Accomplishment of this Service Bulletin provide actions in case of disengagement of
the thermal anti-ice spray ring from the thermal anti-ice feed pipe which could result
in damage to the engine from ice build-up.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
T o accomplish this Service Bulletin it is necessary to:
(1) Inspection
(a) T ask set A330-A-71-XX-3042-01000-93BA-A Inspection
1 Do a SDI of the Thermal Anti-Ice Spray Ring Feed Pipe and Restraint
Brackets for Engine 1
2 Do a SDI of the Thermal Anti-Ice Spray Ring Feed Pipe and Restraint
Brackets for Engine 2
3 Complete and Send the Inspection Report Sheet
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin must be done .
This Service Bulletin has been classified Mandatory. It is expected that an
Airworthiness Directive (AD) published by the European Union Aviation Safety Agency
(EASA) will be issued to confirm this classification. It is anticipated that the AD will

### Page 12

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 12
confirm the thresholds and intervals given but reference should be made to the AD for
confirmation of the mandated accomplishment timescale.
FRSZ026 is a temporary repair that may be active or not (repair previously published
in RR Trent 700 nacelle Ref. SRM 54-10-01 Air Intake Cowl). Consult repair records for
the accomplishment of SRM repair FRSZ026, or equivalent.
The two tables below are presented for the accomplishment timescale: T able 1 in case
a temporary FRSZ026 repair is active, and T able 2 in case there is no active repair
FRSZ026.
T able 1, CONF 001 – Special Detailed Inspection (SDI) of the Thermal Anti-Ice Spray
Ring Feed Pipe and Restraint Brackets for Engine 1 and 2.
COMPLIANCE TIME
CONDITIONS ACTION
THRESHOLD GRACE PERIOD
REPETITIVE
INTERVAL
Aircraft with
TRENT 700
engine having
incorporated an
improved inlet
primary structure
and piccolo tube
(MOD 204615
and SB 71-H847)
and not yet
fitted with the
extended feed
pipe modification
via Rolls-Royce
Service Bulletin
RB211-71-K923
(MOD 210288)
on which SRM
FRSZ026 (or
equivalent) is
active on the
intake cowl
Inspect the anti-
ice feed pipe
disengagement
in accordance
with Ref. T ask
set A330-A-
71-XX-3042-
01ZZZ-93BZ-A
Within 300 Flight
cycles (FC) or
before the expiry
of the 8000
Flight hours
(FH) allowance
of FRSZ026,
whichever is
reached first.
None None
If the thermal
anti-ice feedpipe
are fully or
partially
disengaged
Remove the
nose cowl and
send to an
approved MRO
shop for damage
check and
RB211-71-K923
embodiment.
Before next flight None None
  No further action None None None
If one or both
restraint brackets
are found
severed or
cracked and
feedpipe is
fully engaged
Do the
embodiment of
RB211-71-K923
Before next flight None None
  No further action None None None

### Page 13

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 13
T able 2, CONF 001 – SDI of the Thermal Anti-Ice Spray Ring Feed Pipe and Restraint
Brackets for Engine 1 and 2.
COMPLIANCE TIME
CONDITIONS ACTION
THRESHOLD GRACE PERIOD
REPETITIVE
INTERVAL
Aircraft with
TRENT 700
engine having
incorporated an
improved inlet
primary structure
and piccolo tube
(MOD 204615
and SB 71-H847)
and not yet
fitted with the
extended feed
pipe modification
via Rolls-Royce
Service Bulletin
RB211-71-K923
(MOD 210288)
on which SRM
FRSZ026 (or
equivalent) is
not active on
the intake cowl
Inspection of
anti-ice feed pipe
disengagement
for A330 CEO
TRENT 700 Ref.
T ask set A330-
A-71-XX-3042-
01ZZZ-93BZ-A
First inspection
must be
conducted
within 5000FC
First inspection
must be
conducted with
a Grace Period
of 12 months
from current
SB release date
Subsequent
inspections must
be conducted
every 340FC until
implementation
of the
terminating
action (RB211-
71-K923)
If the thermal
anti-ice feedpipe
are fully or
partially
disengaged
Remove the
nose cowl and
send to an
approved MRO
shop for damage
check and
RB211-71-K923
embodiment
Before next flight None None
  No further action None None None
If one or both
restraint brackets
are found
severed or
cracked and
feedpipe is
fully engaged
Do the
embodiment of
RB211-71-K923
Before next flight None None
  No further action None None None
If feedpipe is
fully engaged
and restraint
brackets
acceptable
Do the
embodiment
of RB211-71-
K923 as an
optional action
None None None
  No further action None None None
F. APPROVAL
The technical content of this document is approved under the authority of the Design
Organisation Approval ref. EASA.21J.031.

### Page 14

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 14
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
(a) T ask set A330-A-71-XX-3042-01000-93BA-A Inspection
PREPARATION
Job Set-Up 0.50 h
PROCEDURE
Complete and Send the Inspection Report Sheet 0.25 h
PREPARATION FOR TEST
None
TEST
None
CLOSE-UP
Close-Up 0.50 h
TOTAL MAN-HOURS 1.25 h
ELAPSED TIME (HOURS) 1.25 h
Additional man-hours related to Vendor SB; refer to:
Do a SDI of the Thermal Anti-Ice Spray
Ring Feed Pipe and Restraint Brackets
for Engine 1
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-AL136
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-K923
Do a SDI of the Thermal Anti-Ice Spray
Ring Feed Pipe and Restraint Brackets
for Engine 2
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-AL136
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-
71-K923
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.
H. WEIGHT AND BALANCE
Not changed
I. ELECTRICAL LOAD DATA
Not changed
J. REFERENCES
(1) Inspection

### Page 15

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 15
(a) T ask set A330-A-71-XX-3042-01000-93BA-A Inspection
AIRCRAFT MAINTENANCE MANUAL (AMM)
06-20-00, Page Block 00 T ask 12-34-24-860-802
T ask 71-13-00-010-805
T ask 71-13-00-410-805
T ask 71-61-41-000-802
T ask 71-61-41-400-802
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)
20-55-00
IN SERVICE INFORMATION (ISI)
00.00.00179 00.00.00217
OPERATOR INFORMATION TELEX (OIT)
999.0066/15
STRUCTURAL REPAIR MANUAL (SRM)
54-10-01
TECHNICAL FOLLOW UP (TFU)
71.61.00004
VENDOR SERVICE BULLETIN (VSB)
ROLLS ROYCE PLC (K0680) VSB RB211-71-AL136
ROLLS ROYCE PLC (K0680) VSB RB211-71-K923
K. PUBLICATION AFFECTED
None
L. INDUSTRY SUPPORT INFORMATION
AIRBUS will not provide industry support for accomplishment of this Service Bulletin.
Refer to Ref. ROLLS ROYCE PLC (K0680) VSB RB211-71-AL136 for the industry support terms
of the Vendor Service Bulletin parts and labor.

### Page 16

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 16
2. MATERIAL INFORMATION
A. MATERIAL APPLICABILITY
Material for task set A330-A-71-XX-3042-01000-93BA-A Inspection
MATERIAL QTY SEE NOTES
Referenced tools See SB
B. TOOLING
Referenced tools for task set A330-A-71-XX-3042-01000-93BA-A Inspection
T o accomplish this Service Bulletin it is necessary to use the tools listed in:
Ref. ROLLS ROYCE PLC (K0680) VSB RB211-71-AL136
Ref. AMM T ask 71-13-00-010-805
Ref. AMM T ask 71-13-00-410-805
C. CONSUMABLES
No consumables
D. LIST OF NEW PARTS
No parts
E. LIST OF EXISTING PARTS
No parts

### Page 17

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 17
3. ACCOMPLISHMENT INSTRUCTIONS
Task set A330-A-71-XX-3042-01000-93BA-A (A330-A-71-XX-3042-01ZZZ-93BZ-A)
Inspection
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 A 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: Section 3. includes procedures given in other documents or in other sections of this
Service Bulletin.
- You must obey the given procedure when the words "in accordance with" are used.
- You can use an accepted alternative procedure only when the words "refer to" are
used and you have a procedure that is accepted by the related local authority.
NOTE: T o add flexibility to your maintenance operations you can select to ignore steps or add
steps from paragraphs 3.B., 3.D., and 3.F . of section 3. as long as:
- you can do paragraphs 3.C. and 3.E.,
- and the technical intent of the Service Bulletin is met within the set parameters,
- and you can put the aircraft back into a serviceable condition.
NOTE: In section 3., the names of the manuals are given with their related acronyms. Refer to
the 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), paragraphs 3.C. and 3.E. of section 3. are Required for
Compliance (RC) and you must do them to comply with the AD.
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessary
to ensure the continued airworthiness of the aircraft.
For any deviations from the instructions, including the Required for Compliance (RC)
paragraphs contained in this Service Bulletin, contact AIRBUS for further instructions and
approval.
NOTE: The flowcharts supplement the information given in paragraphs "3.C. PROCEDURE"
and "1.E. COMPLIANCE". The flowcharts are not the primary source for the tasks or the
compliance times given in this Service Bulletin.
A. TASK SET ASSOCIATED INFORMATION
Task Manpower
TOTAL MAN-HOURS 1.25 h
ELAPSED TIME (HOURS) 1.25 h
Additional man-hours related to Vendor SB; refer to:
ROLLS ROYCE PLC (K0680) VSB RB211-71-AL136
ROLLS ROYCE PLC (K0680) VSB RB211-71-K923

### Page 18

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 18
B. PREPARATION
(1) Task A330-A-71-XX-3042-01001-540A-A (A330-A-71-XX-3042-01ZZZ-540Z-A)
Job Set-Up
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 12-34-24-860-802T ask 71-13-00-010-805
Procedure
NOTE: For the basic aircraft configuration, refer to AMM Chapter “Introduction -
Aircraft Status for Maintenance” in the Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM T ask 12-34-
24-860-802.
(b) Open the fan cowls of engine 1 and engine 2, refer to Ref. AMM T ask 71-13-00-
010-805.
C. PROCEDURE
(1) Task A330-A-71-XX-3042-01001-300A-A (A330-A-71-XX-3042-01ZZZ-300Z-A)
Do a SDI of the Thermal Anti-Ice Spray Ring Feed Pipe and Restraint
Brackets for Engine 1
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
411
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00
T ask 71-61-41-000-802
T ask 71-61-41-400-802
ISI 00.00.00217
OIT 999.0066/15
VSB
ROLLS ROYCE PLC (K0680) VSB RB211-71-
AL136
ROLLS ROYCE PLC (K0680) VSB RB211-71-
K923
Procedure
Ref. Fig.FA Flow Chart
(a) Standard practice given in this procedure:

### Page 19

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 19
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 00.
(b) Do a SDI of the thermal anti-ice spray ring feed pipe and restraint brackets on
engine 1 in accordance with Ref. ROLLS ROYCE PLC (K0680) VSB RB211-71-
AL136.
Refer to Ref. Fig.BA Inspection of the Thermal Anti-Ice Feed Pipe and Restraint
Brackets
1 If the thermal anti-ice spray ring feed pipe is fully or partially disengaged:
a Remove the air intake cowl, refer to Ref. AMM T ask 71-61-41-000-802.
b Send the air intake cowl for implementation of Ref. ROLLS ROYCE PLC
(K0680) VSB RB211-71-K923 in an approved MRO shop.
c Install the air intake cowl, refer to Ref. AMM T ask 71-61-41-400-802.
d After completion of all inspections, complete and send the Inspection
Report sheet in accordance with Ref. T ask A330-A-71-XX-3042-01ZZZ-
90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the regulations,
refer to AIRBUS Ref. OIT 999.0066/15 and Ref. ISI
00.00.00217.
e No further action.
2 If the thermal anti-ice spray ring feed pipe is correctly engaged with one
or both restraint brackets cracked or severed or if a temporary repair
FRSZ026 is active (brackets missing):
a Do the modifications in an approved MRO shop:
<1> Remove the air intake cowl, refer to Ref. AMM T ask 71-61-41-
000-802.
<2> Send the air intake cowl for implementation of Ref. ROLLS
ROYCE PLC (K0680) VSB RB211-71-K923 in an approved MRO
shop.
<3> Install the air intake cowl, refer to Ref. AMM T ask 71-61-41-400-
802.
<4> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
or
b Do the modification on wing :
<1> Do the modification in accordance with Ref. ROLLS ROYCE PLC
(K0680) VSB RB211-71-K923.

### Page 20

A330
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REV 00 Apr 01/25 A330-71-3042
Page 20
<2> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
c No further action.
3 If the thermal anti-ice spray ring feed pipe is correctly engaged, and
restraint brackets are not missing (FRSZ026 active), cracked or severed:
a Repeat the SDI at the compliance time defined in accordance with
PLANNING INFORMATION paragraph 1.E.(2) until implementation of
the terminating action, in accordance with Ref. T ask set A330-A-71-
XX-3042-01ZZZ-93BZ-A.
or
b Do the modifications in an approved MRO shop:
<1> Remove the air intake cowl, refer to Ref. AMM T ask 71-61-41-
000-802.
<2> Send the air intake cowl for implementation of Ref. ROLLS
ROYCE PLC (K0680) VSB RB211-71-K923 in an approved MRO
shop.
<3> Install the air intake cowl, refer to Ref. AMM T ask 71-61-41-400-
802.
<4> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
<5> No further action.
or
c Do the modification on wing :
<1> Do the modification in accordance with Ref. ROLLS ROYCE PLC
(K0680) VSB RB211-71-K923.
<2> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
<3> No further action.

### Page 21

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L35-A-007-01 Fig.FA Sol.AA SHEET 1/1
REV 00 Apr 01/25 A330-71-3042Flow Chart
Page 21
CONF ALL
NOTE:
IS THE
FEED PIPE
OR
NO FURTHER ACTION
IN SHOP, DO THE
EMBODIMENT OF RB211-71-K923,
ADDRESS STIFFENER CRACKS
AND PERFORM FULL
INLET INSPECTION
YES
NO
NO
YES
ON WING, DO THE
EMBODIMENT OF RB211-71-K923
THE COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN.
THE FLOWCHARTS SUPPLEMENT THE INFORMATION GIVEN IN PARAGRAPHS "3.C. PROCEDURE"
AND "1.E. COMPLIANCE". THE FLOWCHARTS ARE NOT THE PRIMARY SOURCE FOR THE TASKS OR
FULLY OR PARTIALLY
INSTALL THE AIR INTAKE
COWL, REFER TO AMM TASK
71-61-41-400-802
REMOVE THE AIR INTAKE
COWL, REFER TO AMM TASK
71-61-41-000-802
COMPLETE AND SEND THE
INSPECTION REPORT SHEET
IS ONE OR BOTH
RESTRAINT BRACKETS MISSING
(FRSZ026), CRACKED OR
SEVERED ?
OR
FOR THE COMPLIANCE TIMES, REFER TO THE ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).01
01
IN ACCORDANCE WITH REF. ROLLS ROYCE
PLC VSB RB211-71-AL136
DO THE INSPECTION OF T-PIECE/FEED PIPE
INTERFACE AND RESTRAINT BRACKETS
DISENGAGED ?
ICN-A330-A-71XX3042-A-FAPE3-01L35-A-007-01

### Page 22

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8N-A-001-01 Fig.BA Sol.AA SHEET 1/2
REV 00 Apr 01/25 A330-71-3042Inspection of the Thermal Anti-
Ice Feed Pipe and Restraint Brackets Page 22
CONF ALL
A
A Z411 (Z421)
B
Z410
Z420
A
B
C
ICN-A330-A-71XX3042-A-FAPE3-01L8N-A-001-01

### Page 23

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8O-A-006-01 Fig.BA Sol.AA SHEET 2/2
REV 00 Apr 01/25 A330-71-3042Inspection of the Thermal Anti-
Ice Feed Pipe and Restraint Brackets Page 23
CONF ALL
C
PICCOLO TUBE
RESTRAINT BRACKET ASSEMBLY
RESTRAINT BRACKET ASSEMBLY
D
FORWARD BULKHEAD
ASSEMBLY (REF)
D
THERMAL ANTI-ICE SPRAY RING FEED PIPE
THERMAL ANTI-ICE SPRAY RING T-PIECE
ICN-A330-A-71XX3042-A-FAPE3-01L8O-A-006-01

### Page 24

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 24
(2) Task A330-A-71-XX-3042-02001-300A-A (A330-A-71-XX-3042-02ZZZ-300Z-A)
Do a SDI of the Thermal Anti-Ice Spray Ring Feed Pipe and Restraint
Brackets for Engine 2
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
411
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00
T ask 71-61-41-000-802
T ask 71-61-41-400-802
ISI 00.00.00217
OIT 999.0066/15
VSB
ROLLS ROYCE PLC (K0680) VSB RB211-71-
AL136
ROLLS ROYCE PLC (K0680) VSB RB211-71-
K923
Procedure
Ref. Fig.FA Flow Chart
(a) Standard practice given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 00.
(b) Do a SDI of the thermal anti-ice spray ring feed pipe and restraint brackets on
engine 2 in accordance with Ref. ROLLS ROYCE PLC (K0680) VSB RB211-71-
AL136.
Refer to Ref. Fig.BA Inspection of the Thermal Anti-Ice Feed Pipe and Restraint
Brackets
1 If the thermal anti-ice spray ring feed pipe is fully or partially disengaged:
a Remove the air intake cowl, refer to Ref. AMM T ask 71-61-41-000-802.
b Send the air intake cowl for implementation of Ref. ROLLS ROYCE PLC
(K0680) VSB RB211-71-K923 in an approved MRO shop.
c Install the air intake cowl, refer to Ref. AMM T ask 71-61-41-400-802.
d After completion of all inspections, complete and send the Inspection
Report sheet in accordance with Ref. T ask A330-A-71-XX-3042-01ZZZ-
90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the regulations,
refer to AIRBUS Ref. OIT 999.0066/15 and Ref. ISI
00.00.00217.
e No further action.
2 If the thermal anti-ice spray ring feed pipe is correctly engaged with one
or both restraint brackets cracked or severed or if a temporary repair
FRSZ026 is active (brackets missing):
a Do the modifications in an approved MRO shop:

### Page 25

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 25
<1> Remove the air intake cowl, refer to Ref. AMM T ask 71-61-41-
000-802.
<2> Send the air intake cowl for implementation of Ref. ROLLS
ROYCE PLC (K0680) VSB RB211-71-K923 in an approved MRO
shop.
<3> Install the air intake cowl, refer to Ref. AMM T ask 71-61-41-400-
802.
<4> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
or
b Do the modification on wing :
<1> Do the modification in accordance with Ref. ROLLS ROYCE PLC
(K0680) VSB RB211-71-K923.
<2> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
c No further action.
3 If the thermal anti-ice spray ring feed pipe is correctly engaged, and
restraint brackets are not missing (FRSZ026 active), cracked or severed:
a Repeat the SDI at the compliance time defined in accordance with
PLANNING INFORMATION paragraph 1.E.(2) until implementation of
the terminating action, in accordance with Ref. T ask set A330-A-71-
XX-3042-01ZZZ-93BZ-A.
or
b Do the modifications in an approved MRO shop:
<1> Remove the air intake cowl, refer to Ref. AMM T ask 71-61-41-
000-802.
<2> Send the air intake cowl for implementation of Ref. ROLLS
ROYCE PLC (K0680) VSB RB211-71-K923 in an approved MRO
shop.
<3> Install the air intake cowl, refer to Ref. AMM T ask 71-61-41-400-
802.

### Page 26

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 26
<4> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
<5> No further action.
or
c Do the modification on wing :
<1> Do the modification in accordance with Ref. ROLLS ROYCE PLC
(K0680) VSB RB211-71-K923.
<2> After completion of all inspections, complete and send the
Inspection Report sheet in accordance with Ref. T ask A330-A-71-
XX-3042-01ZZZ-90AZ-A.
NOTE: If there are findings, send a report to the responsible
authority and to AIRBUS in accordance with the
regulations, refer to AIRBUS Ref. OIT 999.0066/15 and
Ref. ISI 00.00.00217.
<3> No further action.

### Page 27

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L35-A-007-01 Fig.FA Sol.AA SHEET 1/1
REV 00 Apr 01/25 A330-71-3042Flow Chart
Page 27
CONF ALL
NOTE:
IS THE
FEED PIPE
OR
NO FURTHER ACTION
IN SHOP, DO THE
EMBODIMENT OF RB211-71-K923,
ADDRESS STIFFENER CRACKS
AND PERFORM FULL
INLET INSPECTION
YES
NO
NO
YES
ON WING, DO THE
EMBODIMENT OF RB211-71-K923
THE COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN.
THE FLOWCHARTS SUPPLEMENT THE INFORMATION GIVEN IN PARAGRAPHS "3.C. PROCEDURE"
AND "1.E. COMPLIANCE". THE FLOWCHARTS ARE NOT THE PRIMARY SOURCE FOR THE TASKS OR
FULLY OR PARTIALLY
INSTALL THE AIR INTAKE
COWL, REFER TO AMM TASK
71-61-41-400-802
REMOVE THE AIR INTAKE
COWL, REFER TO AMM TASK
71-61-41-000-802
COMPLETE AND SEND THE
INSPECTION REPORT SHEET
IS ONE OR BOTH
RESTRAINT BRACKETS MISSING
(FRSZ026), CRACKED OR
SEVERED ?
OR
FOR THE COMPLIANCE TIMES, REFER TO THE ACCOMPLISHMENT TIMESCALE PARA 1.E.(2).01
01
IN ACCORDANCE WITH REF. ROLLS ROYCE
PLC VSB RB211-71-AL136
DO THE INSPECTION OF T-PIECE/FEED PIPE
INTERFACE AND RESTRAINT BRACKETS
DISENGAGED ?
ICN-A330-A-71XX3042-A-FAPE3-01L35-A-007-01

### Page 28

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8N-A-001-01 Fig.BA Sol.AA SHEET 1/2
REV 00 Apr 01/25 A330-71-3042Inspection of the Thermal Anti-
Ice Feed Pipe and Restraint Brackets Page 28
CONF ALL
A
A Z411 (Z421)
B
Z410
Z420
A
B
C
ICN-A330-A-71XX3042-A-FAPE3-01L8N-A-001-01

### Page 29

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8O-A-006-01 Fig.BA Sol.AA SHEET 2/2
REV 00 Apr 01/25 A330-71-3042Inspection of the Thermal Anti-
Ice Feed Pipe and Restraint Brackets Page 29
CONF ALL
C
PICCOLO TUBE
RESTRAINT BRACKET ASSEMBLY
RESTRAINT BRACKET ASSEMBLY
D
FORWARD BULKHEAD
ASSEMBLY (REF)
D
THERMAL ANTI-ICE SPRAY RING FEED PIPE
THERMAL ANTI-ICE SPRAY RING T-PIECE
ICN-A330-A-71XX3042-A-FAPE3-01L8O-A-006-01

### Page 30

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 30
(3) Task A330-A-71-XX-3042-01001-90AA-A (A330-A-71-XX-3042-01ZZZ-90AZ-A)
Complete and Send the Inspection Report Sheet
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
ISI 00.00.00179
Procedure
(a) Complete the Inspection Report Sheet, refer to Ref. Fig.RA Inspection Report
Sheet.
(b) Send the completed Inspection Report Sheet in accordance with Ref. ISI
00.00.00179.

### Page 31

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8K-A-002-01 Fig.RA Sol.AA SHEET 1/3
REV 00 Apr 01/25 A330-71-3042Inspection Report Sheet
Page 31
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES :
FLIGHT HOURS :
DATE OF INSPECTION :
INSPECTION METHOD : SPECIAL DETAILED
INSPECTION
SHEET IN ACCORDANCE WITH ISI 00.00.00179
SEND THE COMPLETED INSPECTION REPORT
A330-71-3042
A
A Z411 (Z421)
B
Z410
Z420
A
B
C
ICN-A330-A-71XX3042-A-FAPE3-01L8K-A-002-01

### Page 32

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8L-A-006-01 Fig.RA Sol.AA SHEET 2/3
REV 00 Apr 01/25 A330-71-3042Inspection Report Sheet
Page 32
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES :
FLIGHT HOURS :
DATE OF INSPECTION :
INSPECTION METHOD : SPECIAL DETAILED
INSPECTION
SHEET IN ACCORDANCE WITH ISI 00.00.00179
SEND THE COMPLETED INSPECTION REPORT
A330-71-3042
C
PICCOLO TUBE
RESTRAINT BRACKET ASSEMBLY
RESTRAINT BRACKET ASSEMBLY
D
FORWARD BULKHEAD
ASSEMBLY (REF)
D
THERMAL ANTI-ICE SPRAY RING FEED PIPE
THERMAL ANTI-ICE SPRAY RING T-PIECE
ICN-A330-A-71XX3042-A-FAPE3-01L8L-A-006-01

### Page 33

A330
SERVICE BULLETIN
Figure ICN-A330-A-71XX3042-A-FAPE3-01L8M-A-005-01 Fig.RA Sol.AA SHEET 3/3
REV 00 Apr 01/25 A330-71-3042Inspection Report Sheet
Page 33
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES :
FLIGHT HOURS :
DATE OF INSPECTION :
INSPECTION METHOD : SPECIAL DETAILED
INSPECTION
SHEET IN ACCORDANCE WITH ISI 00.00.00179
SEND THE COMPLETED INSPECTION REPORT
A330-71-3042
DO THE INSPECTION OF T-PIECE/FEED PIPE
INTERFACE AND RESTRAINT BRACKETS
YES NO
YES NO
IS THE FEED PIPE FULLY OR
PARTIALLY DISENGAGED ?
IS ONE OR BOTH RESTRAINT 
BRACKETS MISSING (FRSZ026),
DO THE INSPECTION OF T-PIECE/FEED PIPE
INTERFACE AND RESTRAINT BRACKETS
YES NO
YES NO
CRACKED OR SEVERED ?
IS THE FEED PIPE FULLY OR
PARTIALLY DISENGAGED ?
IS ONE OR BOTH RESTRAINT 
BRACKETS MISSING (FRSZ026),
CRACKED OR SEVERED ?
ON ENGINE 1
ON ENGINE 2
ICN-A330-A-71XX3042-A-FAPE3-01L8M-A-005-01

### Page 34

A330
SERVICE BULLETIN
REV 00 Apr 01/25 A330-71-3042
Page 34
D. PREPARATION FOR TEST
None
E. TEST
None
F. CLOSE-UP
(1) Task A330-A-71-XX-3042-01001-740A-A (A330-A-71-XX-3042-01ZZZ-740Z-A)
Close-Up
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 71-13-00-410-805
Procedure
(a) Make sure that the work area is clean and clear of tools and other items of
equipment.
(b) Close the fan cowls of engine 1 and engine 2, refer to Ref. AMM T ask 71-13-00-
410-805.
(c) Put the aircraft back to its initial configuration.
G. ADMINISTRATIVE
(1) Task A330-A-71-XX-3042-02001-90AA-A (A330-A-71-XX-3042-02ZZZ-90AZ-A)
Administrative
Procedure
Confirm in the applicable aircraft records that you completed all the work specified in
this Service Bulletin.

### Page 35

A330
SERVICE BULLETIN
APPENDIX
REV 00 Apr 01/25 A330-71-3042
Page 35
APPENDIX
A. REPORTING SHEET
TITLE: POWER PLANT - AIR INLET - INSPECTION OF AIR INTAKE NOSE COWL
ASSEMBLY NACELLE ANTI-ICE FEED PIPE AND RESTRAINT BRACKETS
MODIFICATION No.: None
(1) 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.
(2) 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.
(3) 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 Bulletins?"
NOTE: ISI 00.00.00179 covers all the frequently asked questions about SB Reporting.
It is revised on a regular basis.

### Page 36

A330
SERVICE BULLETIN
APPENDIX
REV 00 Apr 01/25 A330-71-3042
Page 36
B. 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 Bulletin.
We thank you for the time you have taken in completing this form.
Quality rating of this SB 4 3 2 1
Quality rating of the Accomplishment Instructions 4 3 2 1
Quality rating of the Illustrations 4 3 2 1
Is this SB easy to understand ? Y / N
NOTE: Please rate on a scale of 1 to 4, with 4 being the highest score
If you have 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 Applicability X T ooling X Preparation
X Reason X List of Materials
Operator Supplied
X Mod/Inspection
X Manpower X Kit content X T est
X References X Re-identification X Close-up
X Publication X Illustrations
X Industry Support
Comments :
Operator : Date :
Name/Title
Please return this form to :
AIRBUS
2, ROND POINT EMILE DEWOITINE
31700 BLAGNAC
FRANCE
Or via your Resident Customer Support Office.

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