| CAA-2021-06-009(已有後續修訂版) |
2021/06/23 |
EASA |
2021-0146 |
Trent 1000 ‘Pack B’ engines, models Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE,
Trent 1000-D, Trent 1000-E, Trent 1000-G and Trent 1000-H, all engine serial numbers (ESN);
Trent 1000 ‘Pack C’ engines, models Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2,
Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2,
Trent 1000-K2 and Trent 1000-L2, all ESN; Trent 1000 ‘TEN’ engines, models Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3 and Trent 1000-R3, all ESN; and Trent 7000-72 and Trent 7000-72C engines, all ESN.
These engines are known to be installed on, but not limited to, Boeing 787 and Airbus A330 (NEO)
aeroplanes.
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| CAA-2016-07-011B |
2021/06/23 |
EASA |
2016-0146R2 |
Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232
aeroplanes, all manufacturer serial numbers, except aeroplanes which have embodied Airbus
modification (mod) 161341 in production.
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| CAA-2021-06-006 |
2021/06/21 |
EASA |
2021-0141 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers, except those on
which Airbus modification (mod) 112721, mod 112722, or mod 113501 has been embodied in
production.
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| CAA-2021-06-008緊急(已被CAA-2021-08-006緊急取代) |
2021/06/17 |
EASA |
2021-0143-E |
Model E4 and E4P engines, all serial numbers (s/n).
These engines are known to be installed on, but not limited to, Diamond Aircraft Industries
DA 40 NG, DA 42 NG, DA 42 M-NG and DA 62 aeroplanes.
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| CAA-2021-06-007 |
2021/06/17 |
FAA |
2021-11-24 |
Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, Line Numbers (L/Ns) 1 through 7596 inclusive, except L/Ns 7352, 7362, 7377, 7417, 7457, 7522, 7587, and 7592.
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| CAA-2021-06-005(已被CAA-2022-05-005取代) |
2021/06/17 |
EASA |
2021-0140 |
Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N, A321-272NX aeroplanes, all manufacturer serial numbers.
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| CAA-2021-06-003(已更新) |
2021/06/11 |
EASA |
2021-0137 |
191 series pilot seats, having Part Number (P/N) 19101-00-00, and 191 series co-pilot seats, having
P/N 19102-00-00.
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| CAA-2021-05-006A(已被CAA-2023-08-001取代) |
2021/06/11 |
EASA |
2021-0130R1 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
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| CAA-2021-04-001A |
2021/06/11 |
FAA |
2021-11-21 |
CFM International, S.A. 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 model turbofan engines, with a high-pressure turbine (HPT) case, part number (P/N) 2668M94G01, that contains a stage 7 port, P/N 2614M30P01, with a port casting serial number (S/N) listed in Table 1 in Planning Information, Paragraph 3.A., of CFM Service Bulletin (SB) LEAP-1A-72-00-0421-01A-930A-D, Issue 001, dated October 22, 2020.
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| CAA-2021-06-004 |
2021/06/10 |
FAA |
2021-11-15 |
International Aero Engines V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 model turbofan engines with an installed: (1) High-pressure turbine (HPT) 1st-stage disk, part number (P/N) 2A5001, with a serial number (S/N) listed in Appendix A, Table 1, of IAE Non-Modification Service Bulletin (NMSB) No. V2500-ENG-72-0713, Revision 1, dated January 26, 2021 (IAE NMSB V2500-ENG-72-0713, Revision 1) or IAE NMSB No. V2500-E5-72-0015, dated December 15, 2020 (IAE NMSB V2500-E5-72-0015); and/or (2) HPT 2nd-stage disk, P/N 2A4802, with an S/N listed in Appendix A, Table 2, of IAE NMSB V2500-ENG-72-0713, Revision 1, or IAE NMSB V2500-E5-72-0015.
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