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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-2006-05-013	2006/05/25	FAA	2006-10-14	McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40,DC-9-50, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83),and DC-9-87 (MD-87), MD-88, MD-90-30 and Model 717-200 Airplanes
CAA-2006-05-012	2006/05/25	FAA	2006-10-16	747-100, 747-100B, 747-100B SUD, 747-200B, 747-
CAA-2006-01-001B	2006/05/25	EASA	2006-0136	A318, A319, A320 and A321
CAA-2004-01-014C	2006/05/25	EASA	2006-0129	A330
CAA-2003-01-014D	2006/05/25	EASA	2006-0130	A340
CAA-2006-05-018(已有後續修訂版)	2006/05/23	EASA	2006-0112	A318, A319, A320 and A321
CAA-2006-05-017(已有後續修訂版)	2006/05/23	EASA	2006-0107	A330 and A340-200/-300
CAA-2006-05-015(已有後續修訂版)	2006/05/23	FAA	2006-10-21	Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods
CAA-2006-05-014	2006/05/23	FAA	2006-10-17	737-600, -700, -700C, -800, and -900 Series
CAA-2006-05-011(已有後續修訂版)	2006/05/23	EASA	2006-0126-E	AS 365 N – EC 155