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Airworthiness Directives (ADs)

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Note: Select「+」icon to explore the Applicability of AD and Click CAA AD Number to show more detailed AD information.

CAA AD Number Issue Date Aeronautics Authority of Original AD Original AD Number Applicability Download
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. CAA-2021-07-006.pdf
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). CAA-2021-07-005.pdf
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. CAA-2021-07-004.pdf
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. CAA-2021-07-003.pdf
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. CAA-2021-07-002.pdf
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. CAA-2020-07-011A.pdf
CAA-2021-07-001 2021/07/09 EASA 2021-0161 Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. CAA-2021-07-001.pdf
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. CAA-2021-04-016A.pdf
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). CAA-2021-06-012.pdf
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. CAA-2021-06-011.pdf
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