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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-2004-12-010	2004/12/20	FAA	2004-24-03	Hamilton Sundstrand Power Systems T-62T Series Auxiliary Power Units (APUs)
CAA-2004-12-009	2004/12/20	DGAC	F-2004-193	A300, A310 and A300-600
CAA-2004-12-008	2004/12/20	FAA	2004-25-14	Model DC-9-14, DC-9- 15, and DC-9-15F Airplanes; DC-9-20, DC-9-30, DC-9-40, DC-9-50 Series Airplanes; DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9- 87 (MD-87) Airplanes; and Model MD-88 Airplanes
CAA-2004-12-007	2004/12/17	Transport Canada Civil Aviation	CF-2004-27	Bell 206B
CAA-2004-12-006(已有後續修訂版)	2004/12/17	Transport Canada Civil Aviation	CF-2004-26	DHC-8 Series 100, 200, 300
CAA-2004-12-005	2004/12/13	FAA	2004-25-10	767-300 and -400ER Series
CAA-2004-12-004	2004/12/09	Transport Canada Civil Aviation	CF-2004-25	Bell 206A, 206B and 206L
CAA-2004-12-002(已有後續修訂版)	2004/12/06	DGAC	F-2004-189	A319, A320 and A321
CAA-2004-12-003(已有後續修訂版)	2004/12/03	DGAC	F-1988-132R1	Aeroquip Vickers Equipment, AEROQUIP type 601 hose assemblies
CAA-2004-12-001(已有後續修訂版)	2004/12/02	FAA	2004-24-09	Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) (RRC) 250-B and 250-C Series Turboshaft and Turboprop Engines