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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-2024-04-007 2024/04/24 Transport Canada Civil Aviation CF-2024-12 Bombardier Inc. model CL-600-1A11, CL-600-2A12 and CL-600-2B16 aeroplanes, all serial numbers. CAA-2024-04-007.pdf
CAA-2024-04-006 2024/04/24 FAA 2024-06-01 This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, -900 and -900ER airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-53A1407 RB, dated December 20, 2022. CAA-2024-04-006.pdf
CAA-2023-07-002A 2024/04/24 EASA 2023-0136R1 Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343 and A330-743L aeroplanes, all manufacturer serial numbers (MSN); and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN. CAA-2023-07-002A.pdf
CAA-2024-04-005 2024/04/23 EASA 2024-0091 Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-151N, A319-153N, 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-2024-04-005.pdf
CAA-2024-04-004 2024/04/19 EASA 2024-0090 ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, and ATR 72-212A aeroplanes, manufacturer serial numbers as listed in the Appendix 1 of the AOM, as defined in this AD. CAA-2024-04-004.pdf
CAA-2024-04-003 2024/04/19 EASA 2024-0089 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 having any of the following configurations: A319 aeroplanes on which Airbus modification (mod) 160001 was embodied in production; A319 aeroplanes on which Airbus Service Bulletin (SB) A320-57-1193 was embodied in service; A319 aeroplanes on which Airbus mod 28162, mod 28238 and mod 28342 were embodied in production; A320 aeroplanes on which Airbus mod 160001 was embodied in production; A320 aeroplanes on which Airbus SB A320-57-1193 was embodied in service; A321 aeroplanes on which Airbus mod 160021 was embodied in production. CAA-2024-04-003.pdf
CAA-2024-03-003A 2024/04/18 EASA 2024-0060R1 Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. CAA-2024-03-003A.pdf
CAA-2024-03-002A 2024/04/18 EASA 2024-0058R1 Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. CAA-2024-03-002A.pdf
CAA-2022-06-001B 2024/04/17 EASA 2022-0096R2 Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-151N, A319-153N, 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-2022-06-001B.pdf
CAA-2024-04-002 2024/04/15 FAA 2024-05-11 This AD applies to nternational Aero Engines, LLC (IAE LLC) Model PW1122G–JM, PW1124G1–JM, PW1124G–JM, PW1127G–JM, PW1127G1–JM, PW1127G1A–JM, PW1127G1B–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: (i) High-pressure compressor (HPC) 7th-stage integrally bladed rotor (IBR–7) having part number (P/N) 30G2307 or 30G4407; (ii) HPC 8th-stage integrally bladed rotor (IBR–8) having P/N 30G5608, 30G5908, or 30G8908; (iii) HPC rear hub having P/N 30G4008 or 30G8208; (iv) High-pressure turbine (HPT) 1st-stage hub having P/N 30G4201, 30G6201, or 30G7301; or (v) HPT 2nd-stage hub having P/N 30G3902, 30G5502, or 30G6602. (2) This AD does not apply to parts identified in paragraphs (c)(1)(i) through (v) of this AD if thoseparts were manufactured from powdered metal material produced prior to November 1, 2015, or afterSeptember 1, 2021, as identified by part serial number in Tables 1, 2, and 3 of PW Special Instruction(SI) No. 222F–23, Revision B, dated March 1, 2024 (PW SI No. 222F–23, Revision B) or in theoriginal manufacturing records for the part. (3) If the original manufacturing records do not identify the production date of the powdered metalused to make the parts identified in paragraphs (c)(1)(i) through (v) of this AD, and the part serialnumber is not listed in Tables 1, 2, and 3 of PW SI No. 222F–23, Revision B, then the part is subjectto the requirements of this AD. CAA-2024-04-002.pdf
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