CAA-2021-07-006 |
2021/07/22 |
EASA |
2021-0171 |
SA 365 N1, AS 365 N2, AS 365 N3, EC 155 B and EC 155 B1 helicopters, all serial numbers.
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CAA-2021-07-005 |
2021/07/22 |
EASA |
2021-0170 |
AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1 and SA 365 N1 helicopters, all serial numbers (s/n).
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CAA-2021-07-004(已有後續修訂版) |
2021/07/22 |
EASA |
2021-0169 |
Trent 7000-72 and Trent 7000-72C engines, all serial numbers.
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CAA-2021-07-003 |
2021/07/22 |
EASA |
2021-0167 |
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, A320-211, A320-212, A320-214, A320-215, A320-216,
A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213,
A321-231 and A321-232 aeroplanes, all manufacturer serial numbers, except: - A318 aeroplanes on which modification (mod) 39195 has been embodied in production, or
Service Bulletin (SB) A320-00-1219 has been accomplished in service.
- A319 aeroplanes on which mod 28238, mod 28162 and mod 28342 have been embodied in
production.
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CAA-2021-07-002(已有後續修訂版) |
2021/07/19 |
EASA |
2021-0166 |
Airbus A320-214, A320-251N and A320-271N aeroplanes, manufacturer serial numbers 06640,
06674, 06720, 06799, 06819, 06824, 06829, 06849, 06860, 06868, 06904, 06914, 06946, 06952,
06967, 07033, 07047, 07053, 07074, 07083, 07116, 07145, 07147, 07162, 07172, 07192, 07200,
07205, 07209, 07321, 07329, 07331, 07333, 07359, 07370, 07380, 07391, 07396, 07399, 07429,
07504, 07507, 07510, 07512, 07517, 07533, 07547, 07563, 07571, 07594, 07618, 07629, 07701,
07703, 07731, 07737, 07751, 07753, 07786, 07795, 07813, 07914, 07971, 07990, 08020, 08035,
08048 and 08116.
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CAA-2020-07-011A |
2021/07/15 |
EASA |
2020-0167R1 |
Airbus A350-941 aeroplanes, all manufacturer serial numbers, except aeroplanes that have
embodied Airbus modification (mod) 113749 and mod 112250 in production.
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CAA-2021-07-001 |
2021/07/09 |
EASA |
2021-0161 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
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CAA-2021-04-016A |
2021/07/09 |
EASA |
2021-0115R1 |
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, A319-171N, 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 and A321-272NX aeroplanes, all
manufacturer serial numbers.
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CAA-2021-06-012 |
2021/07/05 |
UK CAA |
G-2021-0004 |
Survitec Group Limited (hereafter referred to as “Survitec” in this AD) Life
Raft with packed assembly P/N 00051054 (Port) and 00051055
(Starboard).
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CAA-2021-06-011 |
2021/07/05 |
FAA |
2021-11-07 |
General Electric Company 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 model turbofan engines with stages 6-10 compressor rotor spools in the high-pressure compressor (HPC) assembly with the following part numbers (P/N) installed:
(i) P/N 2357M30G01, P/N 2357M30G02, P/N 2439M35G01, P/N 2439M35G02, or P/N 2445M40G02, all serial numbers (S/Ns); (ii) P/N 2610M90G01 with the S/Ns listed in paragraph 4., APPENDIX–A, Table 1 of the GE GEnx-1B Service Bulletin (SB) 72-0472 R02, dated November 5, 2020 (GEnx-1B SB 72-0472); and
(iii) P/N 2628M56G01 with the S/Ns listed in paragraph 4., APPENDIX–A, Table 2 or Table 3 of GEnx-1B SB 72-0472. (2) GEnx-2B67, GEnx-2B67/P, GEnx-2B67B model turbofan engines with the following stages 6-10 compressor rotor spools P/Ns installed: (i) P/N 2357M30G02, P/N 2439M35G02, or P/N 2445M40G02, all S/Ns; (ii) P/N 2340M36G01 with S/Ns listed in paragraph 4., APPENDIX–A, Table 1 of GE GEnx-2B SB 72-0415 R02, dated November 5, 2020 (GEnx-2B SB 72-0415); and
(iii) P/N 2628M56G01 with S/Ns listed in paragraph 4., APPENDIX–A, Table 2 or Table 3 of GEnx-2B SB 72-0415.
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