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Airworthiness Directives (ADs)

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-2010-10-009(已有後續修訂版) 2010/10/20 EASA 2010-0211 Airbus A340 aeroplanes, models -211, -212, -213, -311, -312, and -313, all manufacturer serial numbers.
CAA-2010-10-007 2010/10/20 FAA 2010-21-16 McDonnell Douglas Corporation Model MD-90-30 airplanes, certificated in any category; as identified in Boeing Alert Service Bulletin MD90-29A021, Revision 2, dated March 16, 2010.
CAA-2010-10-008 2010/10/18 EASA 2010-0209 Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112,A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplane models, all serial numbers that have received Airbus modification (mod.) 26495 in production or Airbus Service Bulletin (SB) A320-27-1117 in service, except those having received Airbus mod. 38211 or mod. 150004 in production.
CAA-2010-05-008A 2010/10/15 EASA 2010-0091R1 Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplane models, all manufacturer serial numbers.
CAA-2010-09-006修訂 2010/10/14 EASA 2010-0191Correction Airbus A330 aeroplanes, models -201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers on which Airbus modification 49144 (install electrical rudder) has been embodied in production, except those on which Airbus modification 58118 and Airbus modification 200667 have been embodied in production and Airbus A340 aeroplanes, models -311, -312, and -313, all manufacturer serial numbers on which Airbus modification 49144 has been embodied in production, except those on which Airbus modification 58118 and Airbus modification 200667 have been embodied in production and Airbus A340 aeroplanes, models -541, -542, -642, -643, all manufacturer serial numbers, except those on which Airbus modification 200667 has been embodied in production.
CAA-2010-10-006 2010/10/13 EASA 2010-0205 Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -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. This AD is not applicable to aeroplanes on which Airbus modification 54500 has been embodied in production, or on which Airbus Service Bulletin (SB) A330-32-3212 or Airbus SB A340-32-4256, as applicable to the aeroplane model, has been embodied in service.
CAA-2010-10-005 2010/10/12 FAA 2010-21-17 Pratt & Whitney (PW) JT8D-9, -9A, -11, -15, -17, and -17R turbofan engines. These engines are installed on, but not limited to, Boeing 727 series, Boeing 737-200 series and McDonnell Douglas DC-9 airplanes.
CAA-2010-10-004(已有後續修訂版) 2010/10/12 EASA 2010-0204 Rockwell Collins Mode S Transponders identified by type and Part Number (P/N) as follows: TDR-94 622-9352-007, 622-9352-207, 622-9352-008, 622-9352-108, 622-9352-308, 622-9352-309, 622-9352-408, 622-9352-409. and TDR-94D 622-9210-007, 622-9210-207, 622-9210-008, 622-9210-108, 622-9210-308, 622-9210-309, 622-9210-408, 622-9210-409.when installed in combination with certain Rockwell Collins Air Data Computers (ADC) as specified below, and the Rockwell Collins Commercial Standard Digital Bus (CSDB) databus is being used to transfer altitude information between the ADC and the transponder(s).ADC Type P/N (all suffixes, all serial numbers) ADC-81A 622-4401-XXX ADC-82A 622-6475-XXX ADC-82C 622-8329-XXX ADC-82L 622-8105-XXX ADC-85 622-8051-XXX ADC-85A 622-0370-XXX For fixed-wing aeroplanes to which this AD applies, refer to Rockwell-Collins, Inc. Service Information Letter 08-1 to identify whether an installation is affected. Additionally, Rockwell-Collins, Inc. Service Information Letter 2-85 details the part numbers assigned for aeroplanes certified with the ADS-81/82 Air Data System. This AD applies only to fixed-wing aeroplanes with the affected transponders installed and operating under Instrument Flight Rules (IFR) in the designated Enhanced Surveillance (EHS) airspace in Europe. These transponders, in combination with CDSB altitude information transfer, are known to be installed on, but not limited to:Hawker Beechcraft 200 (King Air) series and 1900D aeroplanes, - Dassault Aviation Mystère-Falcon 20 and Mystère-Falcon 50 aeroplanes, and - SAAB SF340A and 340B aeroplanes.
CAA-2010-09-009修訂 2010/10/12 EASA 2010-0192Correction Airbus A330 aeroplanes, models -201, -202, -203, -223, -223F,-243,- 243F, -301, -302, -303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers.
CAA-2010-09-008修訂 2010/10/12 EASA 2010-0193Correction Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313, all manufacturer serial numbers.
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