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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-2025-06-009 2025/07/01 FAA 2025-12-03 This AD applies to CFM International, S.A. Model (CFM) 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 engines. CAA-2025-06-009.pdf
CAA-2025-06-008 2025/06/27 EASA 2025-0133 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, and A319-173N, aeroplanes, all manufacturer serial numbers. CAA-2025-06-008.pdf
CAA-2025-06-007 2025/06/27 Transport Canada Civil Aviation CF-2025-30 Diamond Aircraft Industries Inc (DAI) Models DA40 NG, DA40, DA40 F and DA40 D, All Serial Numbers CAA-2025-06-007.pdf
CAA-2017-06-004B 2025/06/27 EASA 2017-0098R2 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, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 160055 or mod 160056 has been embodied in production, and except A319 aeroplanes on which mod 28162, 28238 and 28342 have been embodied (“Corporate Jet”). CAA-2017-06-004B.pdf
CAA-2025-06-001A 2025/06/19 EASA 2025-0128R1 Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines having engine serial numbers (ESN) listed in Appendix 1 of the NMSB, and Trent XWB-97 engines having ESN listed in Appendix 2 of the NMSB. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes. CAA-2025-06-001A.pdf
CAA-2025-06-005 2025/06/18 Transport Canada Civil Aviation CF-2025-28 Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aeroplanes, serial numbers 60057, 60058, 60060 through 60063, and 60065 through 60121. CAA-2025-06-005.pdf
CAA-2025-05-019修訂 2025/06/17 FAA 2025-06-13Correction This AD applies to The Boeing Company Model 787-9 and 787-10 airplanes, certificated in anycategory, as identified in Boeing Alert Requirements Bulletin B787-81205-SB530084-00 RB, Issue 002, dated September 5, 2024. CAA-2025-05-019修訂.pdf
CAA-2025-06-004 2025/06/09 EASA 2025-0129 Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN). CAA-2025-06-004.pdf
CAA-2025-06-003 2025/06/09 FAA 2025-11-03 This AD applies to General Electric Company Model 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, and GEnx-2B67/P engines with at least one of the following installed: (1) High Pressure Turbine (HPT) stage 1 disk having part number (P/N) 2383M83G03 and a serial number (S/N) listed in Table 1 of GE GEnx-1B Service Bulletin 72-0542 R00, dated April 15, 2024 (GE GEnx-1B SB 72-0542 R00); (2) HPT stage 2 disk having P/N 2300M84P02 and a S/N listed in Table 2 of GE GEnx-1B SB 72-0542 R00; (3) HPT stage 1 disk having P/N 2383M83G03 and a S/N listed in Table 1 of GE GEnx-2B Service Bulletin 72-0471 R00, dated April 15, 2024 (GE GEnx-2B SB 72-0471 R00); or (4) HPT stage 2 disk having P/N 2300M84P02 and a S/N listed in Table 2 of GE GEnx-2B SB 72-0471 R00. CAA-2025-06-003.pdf
CAA-2025-06-002 2025/06/09 FAA 2025-11-05 This AD applies to The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin B787-81205-SB530086-00 RB, Issue 001, dated October 18, 2024. CAA-2025-06-002.pdf
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