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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-2004-07-015B 2007/01/22 EASA 2007-0009 AIRBUS aircraft A330-200, A330-300, A340-200 and A340-300 series, all certified models and all serial numbers. The requirements of paragraphs 1, 2 and 4 of this Airworthiness Directive (AD) are not applicable to Airbus A330-200 aircraft on which AIRBUS modification 53969 or 54833 has been embodied in production or AIRBUS Service Bulletin (SB) A330-27-3134 or SB A330-27-3136 has been embodied in service. Reminder: It is the responsibility of the operator to ensure that any spare part that has been or could be installed on the aircraft does not invalidate the compliance of the aircraft with the requirements of this AD.
CAA-2005-10-001A 2007/01/19 EASA 2007-0008 AIRBUS A330-200, A330-300, A340-200 and A340-300 aircraft, all certified models, all serial numbers, except those on which AIRBUS modification 54833 has been embodied in production or AIRBUS Service Bulletin (SB) A330-27-3136 or SB A340-27-4135 has been embodied in service. Reminder: It is the responsibility of the operator to ensure that any spare part that has been or could be installed on the aircraft does not invalidate the compliance of the aircraft with the requirements of this AD.
CAA-2003-09-027B 2007/01/19 EASA 2007-0011 AIRBUS aircraft A330-200, A330-300, A340-200 and A340-300 series, all certified models and all serial numbers except those on which AIRBUS modification 50394 or 52195 or 53969 or 54833 has been embodied in production or AIRBUS Service Bulletin (SB) A330-27-3128 or SB A340-27- 4129 or Goodrich VSB 4800-27-16 Revision 03 or SB A330-27-3136 or SB A340-27-4135 has been embodied in service.
CAA-2007-01-002 2007/01/15 EASA 2007-0005 - AIRBUS A300 MSN 0202, 0205, 0225, 0299, and 0302 aircraft in Forward Facing Crew Cockpit (FFCC) configuration except aircraft which have received in service application of AIRBUS Service Bulletin (SB) A300-21-0132, - AIRBUS A310 aircraft, all certified models, all serial numbers, except aircraft which have received in service application of SB A310-21-2062, - AIRBUS A300-600 aircraft, all certified models, all serial numbers, on which AIRBUS modification No. 03881 is embodied, except aircraft which have received either incorporation of AIRBUS modification No. 12942 during production, or application of AIRBUS Service Bulletin (SB) A300-21-6049 in service.
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.
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