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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-2006-11-007B(已有後續修訂版)	2007/10/30	ANAC	2006-11-03R2(BRAZIL)	This Airworthiness Directive is applicable to all Embraer ERJ 190 aircraft models in operation and equipped with Primus EPIC software prior to load version 4.3, 4.4, 4.5, 4.6 or 4.7.
CAA-2007-10-005	2007/10/24	FAA	2007-21-13	747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes.767-200, -300, and -300F series airplanes&767-400ER series airplanes
CAA-2007-10-003A	2007/10/24	EASA	2007-0269R1	AIRBUS aircraft A330-200 and A340-300 series, all certified models, all serial numbers. This Airworthiness Directive (AD) is not applicable to aircraft A340-300 series on which both AIRBUS modifications 44205 and 45012 have been embodied in production.
CAA-2007-10-004	2007/10/16	FAA	2007-21-05	This AD applies to International Aero Engines (IAE) model V2500-A1, V2522-A5, V2524- A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, and V2528-D5 turbofan engines with high pressure turbine (HPT) stage 2 air seals, part numbers (P/Ns) 2A0487, 2A1159, 2A1160, 2A3108, 2A3179, 2A3185, 2A3425, and 2A3596, installed. These engines are installed on, but not limited to, Airbus A319, A320, A321, and Boeing MD-90 airplanes.
CAA-2006-11-007A(已有後續修訂版)	2007/10/16	ANAC	2006-11-03R1(BRAZIL)	This Airworthiness Directive is applicable to all Embraer ERJ 190 aircraft models in operation and equipped with Primus EPIC software prior to load version 19.3.
CAA-2007-10-003(已有後續修訂版)	2007/10/12	EASA	2007-0269	AIRBUS aircraft A330-200 and A340-300 series, all certified models, all serial numbers on which AIRBUS modification 44205 has been embodied. in production, except those on which AIRBUS modification 52974 or 53223 has been embodied in production.
CAA-2006-12-003C	2007/10/09	EASA	2007-0247R1-E Correction	AIRBUS aircraft A330-200, A330-300, A340-200, A340-300, A340-500 and A340-600 series, all certified models, all serial numbers.
CAA-2007-10-001	2007/10/08	FAA	2007-19-17	McDonnell Douglas Model MD-11, MD-11F, DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F Airplanes
CAA-2004-07-006F	2007/10/04	EASA	2007-0258	Tay 611-8, Tay 611-8C, Tay 620-15, Tay 650-15 and Tay 651-54 series engines with Low Pressure (LP) compressor ice impact panels of Service Bulletin TAY-72-1326 standard.
CAA-2007-10-002(已有後續修訂版)	2007/10/03	EASA	2007-0256	All the Pacific Scientific rotary buckles p/n’s 1111430-XX and 1111475-XX used on restraint systems p/n’s: 2000029-01 2000067-01 2000115-101 2000029-03 2000115-121 2000029-101 2000029-121 manufactured from November 2004 through May 2007 inclusive. These p/n’s are known to be installed on, but not limited to, Eurocopter a/c models AS 350, AS 355, EC120, EC 130, EC 155. The applicability of this AD is limited to rotorcraft only and is not intended for aeroplanes.