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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-2006-08-011	2006/08/15	FAA	2006-16-09	McDonnell Douglas Model MD-90-30 airplanes
CAA-2006-08-009	2006/08/15	FAA	2006-16-02	McDonnell Douglas Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes
CAA-2006-08-007(已有後續修訂版)	2006/08/15	CAA-NL	NL-2006-011	F28 Mark 0070 and Mark 0100
CAA-2006-08-005	2006/08/15	EASA	2006-0220	This equipment is known to be installed on but not limited to the following aircraft: A318-100, A319-100, A320-200, A321-200, A330-200, A330-300, A340-200, A340-300, A340-600, B737-300, B737-400, B737-500, B737-700, B737-800, B737-900, B747-300, B747-400, B767-300, B777-200, B777-300.
CAA-2006-08-008	2006/08/11	EASA	2006-0232	A330 aircraft and A340-200/-300 series
CAA-2006-08-004	2006/08/11	EASA	2005-6353R1	AS 365 N, SA 366 and SA 365 C Helicopters
CAA-2006-08-003(已有後續修訂版)	2006/08/04	EASA	2006-0224	A330
CAA-2006-08-002	2006/08/03	FAA	2006-15-18	Boeing Model 737-100, -200, -200C, - 300, -400, -500, -600, -700, -700C, -800 and -900 series
CAA-2006-08-001	2006/08/03	FAA	2006-15-15	McDonnell Douglas Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes
CAA-2006-07-023(已有後續修訂版)	2006/07/28	EASA	2006-0219	ATR 42 and ATR 72