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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-2003-02-004A	2004/02/06	FAA	2004-03-01	Air Cruisers Company Emergency Evacuation Slide/Raft system
CAA-2004-02-002	2004/02/05	FAA	2004-02-09	DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88
CAA-2002-06-012A	2004/02/05	DGAC	F-2001-153R2	A340-200/-300
CAA-2004-02-005	2004/02/04	DGAC	F-2001-154R2	A330
CAA-2004-02-004	2004/02/04	DGAC	F-2004-019	A319, A320 and 321
CAA-2004-02-003	2004/02/03	DGAC	F-1999-242-289R1	A300-600, A310
CAA-2004-02-001	2004/02/03	FAA	2004-02-06	McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F (KC-10A- and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F Airplanes; and Model MD- 11 and MD-11F
CAA-2002-11-005B	2004/02/03	DGAC	F-2004-018	A319, A320 and 321
CAA-2002-09-014A(已有後續修訂版)	2004/02/03	DGAC	F-2004-020	A340-200/-300
CAA-2002-09-005A訂正	2004/02/03	DGAC	F-2002-476(B)R1 Correction	A319 and A320