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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-2008-07-001 2008/07/04 FAA 2008-13-22 Boeing Model 747-400, 747-400D, and 747-400F series airplanes.
CAA-2003-11-007B 2008/06/25 FAA 2008-13-03 Boeing Model 747-400, 747-400D, and 747-400F series airplanes.
CAA-2007-07-002C(已有後續修訂版) 2008/06/20 EASA 2008-0017R1 AIRBUS A330 aircraft, models -201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342 and -343, all serial numbers. AIRBUS A340 aircraft, models -211, -212, -213, -311, -312, -313, -541, -542, -642 and -643, all serial numbers.
CAA-2006-08-015A 2008/06/20 FAA 2006-16-18R1 Sandel Avionics Incorporated (Sandel) Model ST3400 terrain awareness warning system/radio magnetic indicator (TAWS/RMI) units approved under Technical Standard Order(s) C113, C151a, or C151b; as identified in Sandel ST3400 Service Bulletin SB3400-01, Revision B, dated September 15, 2004; as installed on various small and transport category airplanes.
CAA-2008-06-008 2008/06/13 FAA 2008-12-04 Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes.
CAA-2008-06-007 2008/06/13 FAA 2008-12-05 Boeing Model 777-200, -200LR, -300, and -300ER series airplanes.
CAA-2008-06-006(已有後續修訂版) 2008/06/09 EASA 2008-0110-E SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3 and SA 366 G1 helicopters, all serial numbers, equipped with horizontal stabilizers part numbers: - 365A13 3030 1906, 365A13 3030 1907, 365A13 3030 1908, 365A13 3030 1909; - 365A13 3036 0001, 365A13 3036 0002, 365A13 3036 0003 and delivered after 01 July 2001 (included).
CAA-2008-06-005 2008/06/09 Transport Canada Civil Aviation CF-1996-24R1 Applies to all Pratt & Whitney Canada (P&WC) PT6A Series engines manufactured after 1 January 1995 or which have had a bleed-off valve (BOV) changed after 1 January 1995, and which are installed in single-engine aircraft.
CAA-2008-06-004 2008/06/09 EASA 2008-0096-E Eurocopter (formerly Eurocopter France) AS 332 L1 and L2, AS 365 N3, EC 155 B1 and EC 225 LP helicopters
CAA-2008-06-003 2008/06/04 FAA 2008-11-13 Boeing Model 777-200, -200LR, -300, and -300ER series airplanes.
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