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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-2019-01-006修訂 2019/01/21 EASA 2019-0004Correction Thales Global Positioning System/Satellite Based Augmentation System (GPS/SBAS) receivers, Topstar 200 LPV, identified by Part Number (P/N) C17149HA01 and P/N C17149JA02, using SBAS. and These receivers are known to be installed on, but not limited to, certain ATR 42-500 and ATR 72-212A aeroplanes (see Note 1 of this AD), and Sikorsky S-76D helicopters. CAA-2019-01-006修訂.pdf
CAA-2019-01-004 2019/01/21 FAA 2018-26-06 This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, as specified in paragraphs (c)(1) through (c)(4) of this AD. (1) Airplanes in Group 1, and in Group 2, Configuration 1, as identified in Boeing Special Attention Service Bulletin 737-52-1170, Revision 1, dated December 19, 2017 (“BSASB 737-52-1170, R1”). (2) Airplanes in Group 2, Configuration 2, as identified in BSASB 737-52-1170, R1. (3) Airplanes in Group 3, as identified in BSASB 737-52-1170, R1, except where this service bulletin specifies the groups as line numbers 4275 through 6724 inclusive, and 6736, this AD specifies those groups as line number 4275 through any line number of an airplane with an original Certificate of Airworthiness or an original Export Certificate of Airworthiness dated on or before the effective date of this AD. (4) All Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes with an original Certificate of Airworthiness or an original Export Certificate of Airworthiness dated after the effective date of this AD. (5) 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-2019-01-004.pdf
CAA-2018-12-011A修訂 2019/01/21 EASA 2018-0276R1Correction Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN). CAA-2018-12-011A修訂.pdf
CAA-2018-12-011A(已有後續修訂版) 2019/01/21 EASA 2018-0276R1 Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN). CAA-2018-12-011A.pdf
CAA-2019-01-007 2019/01/17 EASA 2019-0005 A320-214, A320-271N, A321-211 and A321-231 aeroplanes, manufacturer serial numbers (MSN) as listed in Appendix 1 of this AD. CAA-2019-01-007.pdf
CAA-2019-01-006(已有後續修訂版) 2019/01/16 EASA 2019-0004 Thales Global Positioning System/Satellite Based Augmentation System (GPS/SBAS) receivers, Topstar 200 LPV, identified by Part Number (P/N) C17149HA01 and P/N C17149JA02, using SBAS. and These receivers are known to be installed on, but not limited to, certain ATR 42-500 and ATR 72-212A aeroplanes (see Note 1 of this AD), and Sikorsky S-76D helicopters. CAA-2019-01-006.pdf
CAA-2019-01-002 2019/01/16 Transport Canada Civil Aviation CF-2019-02 6 series 200, DHC-6 series 210, DHC-6 series 300, DHC-6 series 310, DHC-6 series 320 and DHC-6 series 400 aeroplanes, all serial numbers. CAA-2019-01-002.pdf
CAA-2018-12-004A修訂 2019/01/15 EASA 2018-0265R1Correction Rotax 915 iSc3 A, 915 iSc3 B engines and Rotax 914 F2, 914 F3 and 914 F4 engines, all serial numbers. CAA-2018-12-004A修訂.pdf
CAA-2019-01-005 2019/01/14 FAA 2018-26-05 This AD applies to The Boeing Company Model 777-200, 777-200LR, 777-300, 777-300ER, and 777F series airplanes, certificated in any category, excluding line numbers 1165 and subsequent. CAA-2019-01-005.pdf
CAA-2019-01-003 2019/01/14 FAA 2018-26-01 This AD applies to CFM International S.A.(CFM) CFM56-7B20, CFM56-7B22, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27A, CFM56-7B26/B1, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B20/2, CFM56-7B22/2, CFM56-7B24/2, CFM56-7B26/2, CFM56-7B27/2, CFM56-7B20/3, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B26/3, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B3, CFM56-7B27A/3, CFM56-7B26/3F, CFM56-7B26/3B2F, CFM56-7B27/3F, CFM56-7B27/3B1F, CFM56-7B20E, CFM56-7B22E, CFM56-7B22E/B1, CFM56-7B24E, CFM56-7B24E/B1, CFM56-7B26E, CFM56-7B26E/B1, CFM56-7B26E/B2, CFM56-7B27AE, CFM56-7B27E, CFM56-7B27E/B1, CFM56-7B27E/B3, CFM56-7B26E/F, CFM56-7B26E/B2F, CFM56-7B27E/F, and CFM56-7B27E/B1F turbofan engine models. CAA-2019-01-003.pdf
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