Document ID: chunk:federal_register_of_legislation:F2007L01148:body:0:p1
Version: federal_register_of_legislation:F2007L01148
Segment Type: other
Provision Reference: 
Character Range: 0–2897

AIRWORTHINESS DIRECTIVE
On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/A320/180 Amdt 1 and issues the following AD under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Airbus Industrie A319, A320 and A321 Series Aeroplanes
AD/A320/180 Amdt 2  Fuel Tank Decals  6/2007 DM

Applicability:  AIRBUS A319-100 series and A320-200 series, all certified models, serial numbers (MSN) 928, 934, 936, 938, 945, 946, 947, 950, 951, 964, 965, 969, 971, 972, 973, 976, 977, 978, 979, 981, 982, 984, 985, 988, 989, 990, 992, 994, 997, 998, 1002, 1003, 1005, 1014, 1016, 1018, 1026, 1028, 1029, 1030, 1031, 1033, 1035, 1037, 1038, 1039, 1046, 1047, 1049, 1050, 1051, 1054, 1057, 1058, 1059, 1062, 1063, 1064, 1068, 1071, 1074, 1076, 1077, 1084, 1085, 1090, 1093, 1095, 1096, 1097, 1098, 1101, 1103, 1104, 1105, 1110, 1111, 1113, 1115, 1119, 1120, 1122, 1124, 1126, 1128, 1130, 1135, 1136, 1138, 1142, 1143, 1147, 1154, 1155, 1156, 1157, 1159, 1160, 1162, 1163, 1165, 1166, 1169, 1171, 1173, 1179, 1181, 1184, 1187, 1189, 1191, 1194, 1196, 1200, 1201, 1205, 1208, 1209, 1210, 1211, 1213, 1217, 1221, 1222, 1224, 1225, 1231, 1244, 1245, 1246, 1247, 1248, 1249, 1251, 1252, 1253, 1263, 1264, 1265, 1267, 1268, 1269, 1274, 1279, 1280, 1282, 1287, 1289, 1290, 1292, 1295, 1297, 1300, 1308, 1309, 1311, 1315, 1318, 1319, 1326, 1328, 1329, 1335, 1336, 1343, and 1346,

                This AD is not applicable to the aircraft incorporating Airbus Service Bulletin (SB) A320-28-1149 at any Revision status.
Requirement:       1. Unless already accomplished, insert in the aircraft Minimum Equipment List (MEL), the Temporary Revision (TR) of the A318/319/320/321 MMEL (Master Minimum Equipment List) No 01-28/01Z issue 01, which states that the aircraft is not authorized to fly with one pump inoperative, and comply with this Requirement.

                Note 1:  This MMEL TR will be introduced in the next MMEL general revision.

                   2. In the event of a pump failure, inspect the failed pump, the other pump located in the same half wing and their canister, and carry out any necessary rectifications in accordance with the instructions of Airbus SB A320-28-1102 Revision 2 or later DGAC approved revisions.

                   3. Unless already accomplished, inspect the 4 wing pumps and canisters, and carry out