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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-2021-02-016(已有後續修訂版) 2021/03/02 EASA 2021-0053 Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. CAA-2021-02-016.pdf
CAA-2021-02-015緊急(已有後續修訂版) 2021/02/26 EASA 2021-0055-E Model E4 and E4P engines, all serial numbers (s/n) as listed in Austro Engine Service Bulletin (SB) MSB-E4-030. 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. CAA-2021-02-015緊急.pdf
CAA-2021-02-014 2021/02/25 FAA 2021-03-02 GE model CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A5F, CF6-80C2A8, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B2, CF6-80C2B2F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2B6FA, CF6-80C2B7F, CF6-80C2B8F, and CF6-80C2D1F model turbofan engines that underwent an engine shop visit before November 1, 2018, and with accessory gearbox (AGB) adapter hydromechanical unit (HMU)/main engine control (MEC) idler adapter with part number (P/N) 9395M78G01, P/N 9395M78G02, P/N 9395M78G04, P/N 9395M78G05, P/N 9395M78G08, or P/N 9395M78G10, installed. CAA-2021-02-014.pdf
CAA-2021-02-013(已有後續修訂版) 2021/02/25 ANAC 2021-02-02 models EMB-145, EMB-145ER, EMB-145EU, EMB-145EP, EMB-145LR, EMB-145MR, EMB-145LU, EMB-145MP, EMB-145MK, EMB-145XR, EMB-135BJ, EMB-135ER, EMB-135KE, EMB-135KL and EMB-135LR, all serial numbers. CAA-2021-02-013.pdf
CAA-2021-02-012 2021/02/25 FAA 2021-02-07 (GE) GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, -1B67/P1, -1B67/P2, -1B70, -1B70/75/P1, -1B70/75/P2, -1B70/P1, -1B70/P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, -1B74/75/P2, -1B76/P2, and -1B76A/P2 model turbofan engines. CAA-2021-02-012.pdf
CAA-2021-02-011 2021/02/25 FAA 2021-02-06 Model 787-8, 787-9, and 787-10 airplanes, certificated in any category. CAA-2021-02-011.pdf
CAA-2021-02-010(已被CAA-2023-10-002取代) 2021/02/25 FAA 2021-02-15 Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 747-57A2367 RB, dated November 15, 2019. CAA-2021-02-010.pdf
CAA-2021-02-009 2021/02/25 FAA 2021-02-14 Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, line numbers 1 through 1934 inclusive. CAA-2021-02-009.pdf
CAA-2021-02-008 2021/02/25 FAA 2021-02-13 Model 737-600, -700, -700C, -800, and -900 series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-53A1383 RB, Revision 1, dated February 19, 2020. and Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a “change in product” alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17. CAA-2021-02-008.pdf
CAA-2021-02-007 2021/02/24 FAA 2021-02-19 Model 787-8 airplanes equipped with bilge assemblies with decompression panels having part number (p/n) C412707-107, C412705-117, C412705-119, or C412705-121. and Model 787-9 airplanes equipped with bilge assemblies with decompression panels having p/n C419701-123, C419701-125, C419701-127, or C419701-129. and Model 787-10 airplanes equipped with bilge assemblies with decompression panels having p/n 852Z0151-100, 852Z0153-101, or 852Z0156-103. CAA-2021-02-007.pdf
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