| CAA-2021-12-012B |
2025/01/16 |
EASA |
2021-0281R2 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343 and A330-743L aeroplanes, all manufacturer serial numbers.
|
|
| CAA-2019-08-008B |
2025/01/16 |
EASA |
2019-0207R2 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN), except those on which Airbus modification (mod) 115327 has been embodied in production.
|
|
| CAA-2025-01-008 |
2025/01/15 |
EASA |
2025-0011 |
ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR72-102,
ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer
serial numbers (MSN).
|
|
| CAA-2025-01-007(已被CAA-2025-02-003取代) |
2025/01/13 |
EASA |
2025-0007 |
LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, LEAP-1A35A engines, all serial numbers (s/n).
LEAP-1C28, LEAP-1C30, LEAP-1C30B1 engines, all s/n.
These engines are known to be installed on, but not limited to, certain Airbus A319, A320 and A321, and certain COMAC C919 aeroplanes.
|
|
| CAA-2025-01-006 |
2025/01/13 |
EASA |
2025-0008 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
|
|
| CAA-2025-01-005 |
2025/01/10 |
FAA |
2024-25-07 |
This AD applies to General Electric Company (GE) Model GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2, GEnx-1B67, GEnx-1B67/P1, GEnx-1B67/P2, GEnx-1B70, GEnx-1B70/75/P1, GEnx-1B70/75/P2, GEnx-1B70/P1, GEnx-1B70/P2, GEnx-1B70C/P1, GEnx-1B70C/P2, GEnx-1B74/75/P1,GEnx-1B74/75/P2, GEnx-1B76/P2, GEnx-1B76A/P2, GEnx-2B67, GEnx-2B67B, and GEnx-2B67/Pengines with an installed:
(1) Stages 6-10 compressor rotor spool (stages 6-10 spool) having a part number (P/N) and serialnumber (S/N) listed in paragraph 4, Appendix—A, Table 1 of GE GEnx-1B Service Bulletin 72-0525,R01, dated June 10, 2024 (GEnx-1B SB 72-0525, R01); or
(2) Stages 6-10 spool having a P/N and S/N listed in paragraph 4, Appendix—A, Table 1 of GE GEnx-2B Service Bulletin 72-0460, R01, dated June 10, 2024 (GEnx-2B SB 72-0460, R01).
|
|
| CAA-2025-01-004 |
2025/01/09 |
EASA |
2025-0003 |
LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2 and LEAP-1A35A engines, all serial numbers (s/n). LEAP-1B21, LEAP-1B23, LEAP-1B25, LEAP-1B27, LEAP-1B28, LEAP-1B28B1, LEAP-1B28B2, LEAP-1B28B2C, LEAP-1B28B3, LEAP-1B28BBJ1 and LEAP-1B28BBJ2 engines, all s/n.
LEAP-1C28, LEAP-1C30 and LEAP-1C30B1 engines, all s/n.
These engines are known to be installed on, but not limited to, certain Airbus A319, A320, A321, Boeing 737-8, 737-8200, 737-9 and COMAC C919 aeroplanes.
|
|
| CAA-2025-01-003 |
2025/01/09 |
EASA |
2025-0004 |
ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN), except those on which ATR modification (mod) 10469 has been embodied in production; and ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN, except those on which ATR mod 10453 has been embodied in production.
|
|
| CAA-2025-01-002 |
2025/01/09 |
EASA |
2025-0006 |
ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer serial numbers.
|
|
| CAA-2025-01-001 |
2025/01/03 |
EASA |
2024-0235 |
DA 42, DA 42 M, DA 42 NG, DA 42 M-NG aeroplanes, all serial numbers.
|
|