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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.

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CAA AD Number	Issue Date	Aeronautics Authority of Original AD	Original AD Number	Applicability	Download
CAA-2009-12-003A	2010/01/27	FAA	2009-21-10R1	This AD applies to the oxygen cylinder assemblies, approved under United States Department of Transportation Regulations for Type 3HT cylinders, identified in Table 1 of this AD. These oxygen cylinder assemblies may be installed on various transport airplanes, certificated in any category, identified in but not limited to the airplanes included in Table 2 of this AD. Table 1--Affected Oxygen Cylinder Assembly Part Numbers Manufacturer Part Numbers AVOX Systems *6350A34 series 800112-03 800112-10 800112-13 801293-03 801307-00 801307-01 801307-02 801307-03 801307-07 801307-09 801307-23 801307-24 801365-04 801365-14 801375-00 801977-05 *8915 series (*For example, 6350A34-X-X or 8915XX-XX, where “X” denotes a part number digit) B/E Aerospace 176018-115 176112-115 176177-115 176181-115 176529-97 Table 2--Affected Airplanes Manufacturer Model Airbus A300 B4-620, B4-622, B4-605R, and F4-605R airplanes A310-203, -204, -221, -222, -304, and -324 airplanes A318-111 and -112 airplanes A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes A320-111, -211, -212, -214, -231, -232, and -233 airplanes A321-111, -112, -131, -211, and -231 airplanes A330-301, -321, and -322 airplanes A340-211 and -212 airplanes A340-311 and -312 airplanes The Boeing Company 707-100 long body, -200, -100B long body, and -100B short body series airplanes; and 707-300, -300B, -300C, and -400 series airplanes 727, 727C, 727-100, 727-100C, 727-200, and 727-200F series airplanes 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900, and -900ER series airplanes 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 757-200, -200PF, -200CB, and -300 series airplanes 767-200, -300, -300F, and -400ER series airplanes 777-200, -200LR, -300, -300ER, and 777F series airplanes Gulfstream Aerospace Corporation G-IV airplanes McDonnell Douglas Corporation DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-51, DC-8-52, DC-8-53, and DC-8-55 airplanes DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-32F (C-9A, C-9B), DC-9-33F, DC-9-34, DC-9-34F, DC-9-41, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), and DC-10-40 airplanes MD-10-10F and MD-10-30F airplanes MD-11 and MD-11F airplanes MD-88 airplanes MD-90-30 airplanes Short Brothers PLC SD3-30, SD3-SHERPA, and SD3-60 SHERPA airplanes
CAA-2010-01-008	2010/01/26	FAA	2010-01-02	Boeing Company Model 747-100B SUD, -200B, -300, -400, and - 400D series airplanes。
CAA-2010-01-007	2010/01/17	FAA	2010-02-04	Boeing Company Model 737-600, -700, -700C, -800, -900, and - 900ER series airplanes.
CAA-2010-01-006	2010/01/17	FAA	2010-01-05	(1) CFM International, S.A. CFM56-7B20; -7B22; -7B24; -7B26; -7B27; -7B22/B1; -7B24/B1; - 7B27/B1; -7B26/B1; -7B20/3; -7B22/3; -7B24/3; -7B26/3; -7B27/3; -7B22/3B1; -7B24/3B1; - 7B27/3B1; -7B26/3B1; -7B26/3F; -7B27/B3; -7B27/3F; -7B27/3B1F; and -7B27/3B3 turbofan engines assembled with a low-pressure (LP) turbine rear frame, part number (P/N) 340-166-254-0; 340-166-255-0; 340-166-256-0; 340-166-257-0; 340-166-258-0; or 340-166-259-0; and (2) CFM International, S.A. CFM56-7B20/2; -7B22/2; -7B24/2; -7B26/2; and -7B27/2 turbofan engines assembled with a dual annular combustor and an LP turbine rear frame, P/N 340-177-551-0; 340-177-552-0; 340-177-553-0; 340-177-554-0; 340-177-555-0; or 340-177-556-0. (3) These engines are installed on, but not limited to, Boeing 737-600, 737-700, 737-800, and 737-900 series airplanes.
CAA-2009-11-001修訂	2010/01/15	EASA	2009-0237-E Correction	Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, - 303, -321, -322, -323, -341, -342 and -343 aeroplanes, all manufacturer serial numbers on which Airbus modification 48809 has been embodied in production, if delivered before 26 October 2009. Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313 aeroplanes, all manufacturer serial numbers on which Airbus modification 48809 has been embodied in production, if delivered before 26 October 2009. Airbus A340 aeroplanes, models -541, -542, -642 and -643, all manufacturer serial numbers, if delivered before 26 October 2009.
CAA-2008-05-007A	2010/01/15	FAA	2008-10-10R1	Boeing Company Model 737-600, -700, -700C, -800, and -900 series.
CAA-2010-01-005	2010/01/14	FAA	2010-01-01	Boeing Company Model 747-200F, 747-200C, 747-400, 747- 400D, and 747-400F series airplanes.
CAA-2010-01-004	2010/01/14	FAA	2010-01-08	Boeing Company Model 737-600, -700, and -800 series airplanes.
CAA-2010-01-003A(已有後續修訂版)	2010/01/14	EASA	2010-0003R1	Rockwell Collins Mode S Transponders identified by type and Part Number (P/N) as follows: Type P/N (all serial numbers) TDR-94 622-9352-008, 622-9352-108, 622-9352-308 and 622-9352-408 TDR-94D 622-9210-008, 622-9210-108, 622-9210-308 and 622-9210-408 when installed in aeroplanes featuring weight-on-wheels input to the transponder and operated in European Mode S Designated Airspace. These transponders are known to be installed on, but not limited to, the following aeroplanes (see ‘Required Actions’ section of this AD for exemptions): - ATR42 and ATR72 - Bombardier (Canadair) CL-600-2B16 (604 Variant) - Bombardier CL-600-2B19.(RJ100 and RJ200) - Cessna 525, s/n 525-0600 to 525-0684 (CJ1) - Cessna 525A, s/n 525A-0300 to 525A-0438 (CJ2) - Cessna 525B, s/n 525B-0001 through 525B-0293 (CJ3) - Cessna 560, s/n 560-0751 through 560-0802 (Citation Encore+) - Cessna 560XL, s/n 560-6001 and up (Citation XLS+) - Dassault Aviation Mystre-Falcon 50 EASA AD No : 2010-0003R1 EASA Form 110 Page 2/4 - Dassault Aviation Mystre-Falcon 900 - Dassault Aviation Falcon 900EX - Dassault Aviation Falcon 2000 - Dassault Aviation Falcon 2000EX - Piaggio Aero Industries P.180 (Avanti and Avanti II) - SAAB 2000 Note 1: Aeroplanes which are operated at take-off rotation speeds not exceeding 100 knots are not affected by the requirements of this AD. Note 2: For more information regarding Mode-S designated airspace, please consult the Eurocontrol website at www.eurocontrol.int/msa/public/standard_page/nv_modes_homepage.html and local Aeronautical Information Circulars (AIC).
CAA-2010-01-003(已有後續修訂版)	2010/01/12	EASA	2010-0003	Rockwell Collins Mode S Transponders identified by type and Part Number (P/N) as follows: Type P/N (all serial numbers) TDR-94 622-9352-008, 622-9352-108, 622-9352-308 and 622-9352-408 TDR-94D 622-9210-008, 622-9210-108, 622-9210-308 and 622-9210-408 when installed in aeroplanes featuring weight-on-wheels input to the transponder and operated in European Mode S Designated Airspace. These transponders are known to be installed on, but not limited to, the following aeroplanes (see ‘Required Actions’ section of this AD for exemptions): - ATR42 and ATR72 - Bombardier (Canadair) CL-600-2B16 (604 Variant) - Bombardier CL-600-2B19.(RJ100 and RJ200) - Cessna 525, s/n 525-0600 to 525-0684 (CJ1) - Cessna 525A, s/n 525A-0300 to 525A-0438 (CJ2) - Cessna 525B, s/n 525B-0001 through 525B-0293 (CJ3) - Cessna 560, s/n 560-0751 through 560-0802 (Citation Encore+) - Cessna 560XL, s/n 560-6001 and up (Citation XLS+) - Dassault Aviation Mystre-Falcon 50 EASA AD No : 2010-0003 EASA Form 110 Page 2/4 - Dassault Aviation Mystre-Falcon 900 - Dassault Aviation Falcon 900EX - Dassault Aviation Falcon 2000 - Dassault Aviation Falcon 2000EX - Piaggio Aero Industries P.180 (Avanti and Avanti II) - SAAB 2000 Note 1: Aeroplanes which are operated at take-off rotation speeds not exceeding 100 knots are not affected by the requirements of this AD. Note 2: For more information regarding Mode-S designated airspace, please consult the Eurocontrol website at www.eurocontrol.int/msa/public/standard_page/nv_modes_homepage.html and local Aeronautical Information Circulars (AIC).