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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-2022-02-014(已被CAA-2023-06-008取代) 2022/02/25 FAA 2022-05-04 Boeing Model 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, except for Model 737-200 and -200C series airplanes equipped with an SP-77 flight control system. CAA-2022-02-014.pdf
CAA-2022-02-013 2022/02/25 FAA 2022-02-14 Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin B787-81205-SB320045-00 RB, Issue 001, dated November 9, 2020. CAA-2022-02-013.pdf
CAA-2022-02-012 2022/02/25 EASA 2022-0028 Airbus A319-151N, A319-153N, A319-171N, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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-2022-02-012.pdf
CAA-2022-02-011 2022/02/23 Japan CAB TCD-9876-2022 Kawasaki BKll7, BKll7 A-3, BKll7 A-4, BKll7 B-1, BKll7 B-2, BKll7 C-1 and BKll7 C-2 helicopters. CAA-2022-02-011.pdf
CAA-2022-02-010(已被CAA-2023-02-001取代) 2022/02/23 EASA 2022-0026 Airbus 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, A320-251N, A320-271N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N and A321-253N aeroplanes, all manufacturer serial numbers (MSN), if equipped with an affected galley, as identified by Part Number (P/N) and serial number (s/n) in Table 1 and Table 2 of Appendix 1 of this AD, or as identified by P/N in Tables 3, 4 or 5 of Appendix 1 of this AD. CAA-2022-02-010.pdf
CAA-2022-02-009 2022/02/23 FAA 2022-03-15 all serial numbers of the airplane models listed in table 1 to paragraph (c), certificated in any category, that are either: (1) Modified with a Garmin G3X Touch Electronic Flight Instrument System under Supplemental Type Certificate No. SA01899WI, installed in accordance with Master Drawing List Document No. 005-01320-00, Revision 9 or earlier, interfaced with a Garmin Engine Adapter GEA 24 connected to resistive fuel probes; or (2) Modified with a Garmin GI 275 Multi-Function Display under STC No. SA02658SE, installed in accordance with MDL Revision 9 or earlier, interfaced with a Garmin Engine Adapter GEA 24 connected to resistive fuel probes. Note 1 to paragraph (c): Garmin Mandatory STC Service Bulletin No. 2134, Revision A, and Garmin Mandatory STC Service Bulletin No. 2135, Revision A, both dated April 23, 2021, contain information for how to determine if your airplane has a resistive probe interface. CAA-2022-02-009.pdf
CAA-2022-02-008 2022/02/23 FAA 2022-02-03 CFM International, S.A. CFM56-3 and CFM56-7B model turbofan engines equipped with an accessory gearbox assembly with the following part numbers (P/Ns): (1) For CFM56-3, CFM56-3B, and CFM56-3C model turbofan engines, AGB P/N: 335-300-103-0, 335-300-105-0, 335-300-106-0, 335-300-107-0, 335-300-108-0, 335-300-109-0, or 335-300-110-0, installed. (2) For CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/2, CFM56-7B26/3, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B26/3B2F, CFM56-7B26/3F, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27/2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B1F, CFM56-7B27/3B3, CFM56-7B27/3F, CFM56-7B27/B1, and CFM56-7B27/B3 model turbofan engines, AGB P/N: 340-046-503-0, 340-046-504-0, or 340-046-505-0, installed. (3) For CFM56-7B27A, CFM56-7B27A/3, or CFM56-7B27AE model turbofan engines, AGB P/N: 340-188-601-0, 340-188-603-0, or 340-188-605-0, installed. CAA-2022-02-008.pdf
CAA-2021-01-003A 2022/02/23 EASA 2021-0002R1 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, A321-252N, A321-253N, A321-271N, A321-272N, A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX aeroplanes, all manufacturer serial numbers. CAA-2021-01-003A.pdf
CAA-2022-02-007 2022/02/21 FAA 2022-03-16 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, GEnx-2B67, GEnx-2B67B, and GEnx-2B67/P model turbofan engines with a compressor discharge pressure bolted joint assembled or reassembled with the 11C4525P01 torque fixture or assembled with the 11C4629P01 torque wrench. CAA-2022-02-007.pdf
CAA-2022-02-006 2022/02/18 FAA 2022-03-19 General Electric Company Passport 20-17BB1A, Passport 20-18BB1A, and Passport 20-19BB1A model turbofan engines. CAA-2022-02-006.pdf
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