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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-2016-09-006 2016/09/13 FAA 2016-18-11 Gulfstream Aerospace Corporation airplanes (1) All Model G-1159 airplanes. (2) All Model G-1159A airplanes. (3) All Model G-1159B airplanes. (4) All Model G-IV airplanes. (5) All Model GV airplanes. (6) Model GIV-X airplanes, serial numbers 4001 through 4350 inclusive. (7) Model GV-SP airplanes, serial numbers 5001 through 5542 inclusive. CAA-2016-09-006.pdf
CAA-2016-09-003(已被CAA-2020-01-001取代) 2016/09/13 FAA 2016-18-02 This AD applies to The Boeing Company Model 777-200 and -300ER series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 777-35-0041, dated April 8, 2016. CAA-2016-09-003.pdf
CAA-2016-09-002(已被CAA-2019-02-008取代) 2016/09/13 FAA 2016-18-01 (1) This AD applies to certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 737-32-1448, Revision 1, dated May 29, 2015. (2) Installation of Supplemental Type Certificate (STC) ST00830SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/184DE9A71EC3FA5586257EAE00707DA6?OpenDocument&Highlight=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-2016-09-002.pdf
CAA-2016-09-005 2016/09/08 FAA 2016-18-10 International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 engines. CAA-2016-09-005.pdf
CAA-2016-09-004 2016/09/05 Transport Canada Civil Aviation CF-2016-26 Bombardier Inc. model BD-100-1A10 aeroplanes, serial numbers (S/Ns) 20003 to 20532. CAA-2016-09-004.pdf
CAA-2016-09-001修訂 2016/09/05 EASA 2016-0176Correction 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, 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. CAA-2016-09-001修訂.pdf
CAA-2016-09-001(已有後續修訂版) 2016/09/05 EASA 2016-0176 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, 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. CAA-2016-09-001.pdf
CAA-2015-06-011B(已有後續修訂版) 2016/09/05 EASA 2015-0124R2 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 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN. CAA-2015-06-011B.pdf
CAA-2016-08-009 2016/09/02 FAA 2016-17-10 The Boeing Company Model 777-200, 777-200LR, 777-300, 777-300ER, and 777F series airplanes, certificated in any category. CAA-2016-08-009.pdf
CAA-2016-08-008(已有後續修訂版) 2016/08/23 EASA 2016-0167 CAS 536-series attendant seats, having Part Number (P/N) 53600, all dash numbers, all serial numbers. These seats are known to be installed on, but not limited to, ATR-GIE Avions de Transport Régional ATR 42 and ATR 72 aeroplanes. CAA-2016-08-008.pdf
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