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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-2023-10-005 2023/10/16 EASA 2023-0179 Airbus A320-214, A320-216, A320-251N, A320-271N and A321-253NX aeroplanes, manufacturer serial numbers 8781, 8998, 9015, 9036, 9049, 9068, 9077, 9130, 9175, 9197, 9200, 9211, 9216, 9246, 9252, 9253, 9254, 9264, 9273, 9287, 9300, 9306, 9313, 9316, 9317, 9328, 9329, 9331, 9332, 9341, 9343, 9354, 9358, 9363, 9373, 9378, 9384, 9391, 9394, 9428, 9431, 9439, 9446, 9453, 9454, 9457, 9465, 9473, 9482, 9526, 9559, 9574, 9590, 9595, 10019 and 10044. CAA-2023-10-005.pdf
CAA-2023-10-004 2023/10/13 EASA 2023-0176 Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. CAA-2023-10-004.pdf
CAA-2023-10-003 2023/10/11 FAA 2023-20-08 General Electric Company (GE) Model CF6–80C2B1F, CF6–80C2B2F, CF6–80C2B4F, CF6–80C2B5F, CF6–80C2B6F, CF6–80C2B7F, CF6–80C2K1F engines, having engine serial numbers (S/Ns) 630–136 through 630–156 inclusive, engine S/Ns 707–510 through 707–645 inclusive, which have accumulated less than 400 engine cycles since new (CSN) on the effective date of this AD. CAA-2023-10-003.pdf
CAA-2023-10-002 2023/10/11 FAA 2023-18-06 The Boeing Company Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747–400, 747–400D, 747–400F, 747SR series airplanes, certificated in any categy, as identified in Boeing Alert Requirements Bulletin 747–57A2367 RB, Revision 1, dated March 20, 2023. CAA-2023-10-002.pdf
CAA-2023-10-001 2023/10/06 Transport Canada Civil Aviation CF-2023-65 Bombardier Inc. model BD-700-1A10 BD-700-1A11 aeroplanes, serial numbers 9001 through 9879, 9998 60001 through 60065. CAA-2023-10-001.pdf
CAA-2023-09-008 2023/09/27 FAA 2023-13-05 (1) This AD applies to all The Boeing Company Model 737–600, –700, –700C, –800, –900, –900ER series airplanes, certificated in any categy. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefe, 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-2023-09-008.pdf
CAA-2023-09-007 2023/09/23 FAA 2023-17-08 This AD applies to General Electric Company (GE) Model GEnx–1B64/P2, GEnx–1B67/P2, GEnx–1B70/75/P2, GEnx–1B70/P2, GEnx–1B70C/P2, GEnx–1B74/75/P2, GEnx–1B76/P2, GEnx–1B76A/P2, GEnx–2B67/P engines with an installed: (1) Stages 6–10 compress rot spool having a part number (P/N) serial number (S/N) listed in paragraph 4, Appendix—A, Table 1 of GE GEnx–1B Service Bulletin 72–0515, R00, dated January 31, 2023 (GEnx–1B 72–0515 R00); (2) Fward seal having a P/N S/N listed in paragraph 4, Appendix—A, Table 2 of GEnx–1B 72–0515 R00; (3) Stages 6–10 compress rot spool having a P/N S/N listed in paragraph 4, Appendix—A, Table 1 of GE GEnx–2B Service Bulletin 72–0452, R00, dated January 31, 2023. (GEnx–2B 72–0452 R00); (4) Fward seal having a P/N S/N listed in paragraph 4, Appendix—A, Table 2 of GEnx–2B 72–0452 R00. CAA-2023-09-007.pdf
CAA-2023-09-006 2023/09/19 FAA 2023-18-04 This AD applies to General Electric Company Model CF6–80E1A2, CF6–80E1A3, CF6–80E1A4, CF6–80E1A4/B engines with an installed fward outer seal, high-pressure turbine rot (HPTR) stage 1 disk, rotating seal having a part number (P/N) serial number (S/N) identified in Table 1 to paragraph (c) of this AD. CAA-2023-09-006.pdf
CAA-2023-09-003 2023/09/12 FAA 2023-16-07 This AD applies to International Aero Engines, LLC (IAE LLC) Model PW1122G–JM, PW1124G1–JM, PW1124G–JM, PW1127G–JM, PW1127G1–JM, PW1127GA–JM, PW1129G–JM, PW1130G–JM, PW1133G–JM, PW1133GA–JM, PW1428G–JM, PW1428GA–JM, PW1428GH–JM,PW1431G–JM, PW1431GA–JM, and PW1431GH–JM engines with an installed: (1) High-pressure turbine (HPT) 1st-stage hub, part number (P/N) 30G6201 or 30G7301, with aserial number (S/N) listed in Tables 1, 2, 3, or 4 of Pratt & Whitney (PW) Special Instruction No.149F–23, dated August 4, 2023; or (2) HPT 2nd-stage hub, P/N 30G5502 or 30G6602, with an S/N listed in Tables 1, 2, 3, or 4 of PWSpecial Instruction No. 149F–23, dated August 4, 2023. CAA-2023-09-003.pdf
CAA-2021-07-018取消 2023/09/11 EASA 2021-0180-CN Airbus A300, A300-600 and A310 aeroplanes, all certified models, all manufacturer serial numbers (MSN); Airbus A300F4-608ST aeroplanes, all MSN; Airbus A318, A319, A320 and A321 aeroplanes, all certified models, all MSN; Airbus A330 aeroplanes, all certified models except A330-223F and A330-243F, all MSN, and Airbus A340 aeroplanes, all certified models, all MSN. CAA-2021-07-018取消.pdf
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