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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-2007-01-001	2007/01/15	FAA	2006-26-13	Boeing Model 707-100 Long Body, -100B Long Body, -100B Short Body, -E3F, -300, -300B, and -300C Series Airplanes; Model 727-100 and -200 Series Airplanes; Model 737-200, -200C, -300, -400, and -500 Series Airplanes; Model 747-100B, 747-200B, 747- 200C, 747-200F, 747-300, 747-400, 747-400D, 747SR, and 747SP Series Airplanes; Model 757- 200 and 757-200PF Series Airplanes; and Model 767-200 and -300 Series Airplanes; Equipped With Observer or Attendant Seats
CAA-2006-07-001A	2007/01/11	EASA	2006-0178R1	- AIRBUS A300 and A300-600 aircraft, all certified models and all serial numbers, except aircraft on which AIRBUS modification No. 12994 has been embodied in production, or Airbus Service Bulletin (SB) A300-32-0448 or SB A300-32-6094 embodied in service; and - A300-600ST aircraft, all certified models and all serial numbers, except aircraft on which SB A300-32-9011 has been embodied in service (AIRBUS modification No. 19579).
CAA-2006-04-002B	2007/01/11	EASA	2006-0075R2	AIRBUS A300, A300-600 and A300-600ST aircraft, all certified models and all serial numbers, on which the main landing gear retraction actuators are equipped with sliding rods with P/N C69029-2 or C69029-3.
CAA-2006-11-005修訂	2007/01/02	FAA	2006-23-02 Correction	Raytheon Aircraft Company Models C90A, B200, B200C, B300, and B300C Airplanes
CAA-2006-12-012	2006/12/26	EASA	2006-0376	ATR 42 aircraft, all models, all serial numbers, except aircraft which have received ATR modification 04372 (aileron spring tab) in production or ATR Service Bulletin (SB) ATR42-27-0081 or SB ATR42-27-0092 in service. ATR 72-101, -102, -201, -202, -211, 212 aircraft models, all serial numbers, except aircraft which have received ATR modification 04373 (aileron spring tab) in production or SB ATR72-27-1045 embodied in service.
CAA-2006-12-011	2006/12/26	FAA	2006-26-01	This AD applies to CFM International CFM56-2 series, -3 series, -5 series, and -7B series engines with fuel filters, Western Filter part numbers (P/Ns) WF337661 and WF337017 and PTI Technologies P/Ns 7595983-101 and 7588133, installed. These engines are installed on, but not limited to, Airbus A320 and A340 series airplanes, Boeing DC8-71 series, -72 series, and -73 series airplanes, and Boeing 737 series airplanes.
CAA-2006-09-001A	2006/12/20	EASA	2006-0375	Rocker-type Switches, having Carling P/N TA201-(XX)-(X), all versions. These same switches are also identified by, but not limited to, Piper P/N 47664-07; Grumman P/N TB201-TB-W or B206; and Cessna P/N S 1824-1 or S 2160-1. The affected switches are known to be installed on, but not limited to, aircraft manufactured by the Piper Aircraft Corporation, Cessna Aircraft Company and Grumman American Aviation Corporation, certificated under FAR Part 23.
CAA-2003-09-001B	2006/12/20	EASA	2006-0374	AIRBUS A300-600 aircraft, all certified models and all serial numbers.
CAA-2006-12-009	2006/12/19	CAA of Israel	52-06-11-08	Gulfstream Aerospace LP(GALP) Models 1125 ASTRA, ASTRA SPX and G100 aircraft.
CAA-2006-12-008	2006/12/19	EASA	2006-0372-E	AIRBUS aircraft A300 and A300-600, all certified models, all serial numbers except for those where LH and RH wing MLG rib 5 forward lugs have been repaired by installation of oversized interference fit bushes as per drawing R57240221