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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-2009-08-002	2009/08/13	EASA	2009-0173	Rockwell Collins Mode S Transponders identified by type and Part Number (P/N) as follows: Type P/N (all serial numbers) TDR-94 622-9352-007, 622-9352-008 and 622-9352-108; TDR-94D 622-9210-007, 622-9210-008 and 622-9210-108 when installed in an aeroplane operating in European Designated Mode S Airspace and equipped with Honeywell AZ800 or AZ810 (all part numbers) air data computers (ADC) where the data bus interface between the Honeywell ADC and the Rockwell Collins transponder is providing the Selected Altitude data input to the transponder. These transponder/ADC combinations are known to be installed on, but not limited to, the following aeroplanes: - ATR 42 and ATR 72 series (See exemption under ‘Required Action’). - Bombardier (formerly Canadair) CL-600-2A12 (601 Variant) and CL-600-2B16 (601-3A and 601-3R Variants). - Bombardier (formerly De Havilland Canada) DHC-8 series. - Dassault Aviation Mystere-Falcon 900 series. - Gulfstream G-IV. Note: For more information regarding Mode-S designated airspace, please consult the Eurocontrol website at www.eurocontrol.int/mode-s and local Aeronautical Information Circulars (AIC).
CAA-2009-08-003	2009/08/07	EASA	2009-0168	F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers, if an actuator Part Number (P/N) 9409122 or P/N 53-0013 is installed on one or both fuel fire shut-off valves.
CAA-2009-08-001	2009/08/07	Transport Canada Civil Aviation	CF-2009-32	Bell Helicopter Textron Canada (BHTC) Helicopter Models: 206A Serial number 004 through 660 and 672 through 715; 206B converted from Model 206A, all serial numbers; 206B Serial number 661 through 671 and 716 through 4661, 4663 through 4665, 4667 and 4670; 206L Serial number 45004 through 45153 and 46601 through 46617; 206L-1 Serial number 45154 through 45790; 206L-3 Serial number 51001 through 51612; 206L-4 Serial number 52001 through 52389, 52391 and 52393; 222 Serial number 47006 through 47089; 222B Serial number 47131 through 47156; 222U Serial number 47501 through 47574 230 Serial number 23001 through 23038; 407 Serial number 53000 through 53887, 53890 through 53916, 53918, 53920, 53921,53923 through 53926, 53928; 427 Serial number 56001 through 56073, 58001, 58002; 430 Serial number 49001 through 49129.
CAA-2009-07-014	2009/08/03	FAA	2009-15-13	This AD applies to Honeywell International Inc. T5313B, T5317A, T5317A-1, T5317B, and T5317BCV turboshaft engines with combustion chamber housing (CCH), part numbers (P/Ns) 1-130-610-05, 1-130-610-12, and 1-130-610-17, installed. These engines are installed on, but not limited to, Bell 205 and 210 Series and Kaman K-1200 helicopters.
CAA-2009-07-013	2009/07/28	FAA	2009-15-12	Boeing Model 747-400 and -400D series airplanes.
CAA-2009-07-012	2009/07/23	EASA	2009-0154-E	CFM56-5B engine models equipped with Hydromechanical units HMU VIN 8061- 532 (P/N 1348M79P10), VIN 8061-535 (P/N 1348M79P13), VIN 8061-536 (P/N 1348M79P14), Serial Numbers (S/N) as identified within paragraph 1.A of CFM Service Bulletin CFM56-5B S/B 73-0238 Revision 1 and which have not been modified in accordance with CFM56-5A S/B 73-0208, CFM56-5B S/B 73-0239 or CFM56-5C S/B 73-0180. These engines are known to be installed on, but not limited to Airbus A318, A319, A320 and A321 series aeroplanes.
CAA-2009-07-010	2009/07/23	EASA	2009-0156	Airbus A330 aeroplanes, models -301, -302, -303, -321, -322, -323, -341,-342 and -343, all manufacturer serial numbers, and Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313, all manufacturer serial numbers,if equipped with Carbon Fiber Reinforced Plastic (CFRP) rudders having part numbers (P/N) and serial numbers (S/N) as listed in the Appendix A to this AD.
CAA-2009-07-011	2009/07/21	EASA	2009-0159-E	Model ATR 42-200, 42-300, 42-320, 42-400 and 42-500 aeroplanes, and Model ATR 72-101, 72-102, 72-201, 72-202, 72-211, 72-212 and 72-212A aeroplanes that are equipped with PPG Aerospace cockpit forward side glass windows part number (p/n) NP158862-1 and/or p/n NP158862-2.
CAA-2009-07-009	2009/07/17	ANAC	2007-02-02R2(BRAZIL)	This Airworthiness Directive (AD) applies to all Embraer ERJ 190 airplane models equipped with firewall hydraulic shutoff valve (FWSOV) part number (P/N) 975287-3 or 975287-5.
CAA-2009-07-008	2009/07/17	EASA	2009-0153	Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, - 303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers on which Airbus modification 49144 (install rudder fly by wire) has been embodied in production. Airbus A340 aeroplanes, models -311, -312, and -313, all manufacturer serial numbers on which Airbus modification 49144 has been embodied in production. Airbus A340 aeroplanes, models -541, -542, -642, -643, all manufacturer serial numbers.