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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-2016-03-004 2016/03/04 FAA 2016-04-20 This AD applies to all The Boeing Company airplanes (1) Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. (2) Model 757-200, -200PF, -200CB, and -300 series airplanes. (3) Model 767-200, -300, -300F, and -400ER series airplanes. (4) Model 777-200, -200LR, -300, -300ER, and -777F series airplanes. CAA-2016-03-004.pdf
CAA-2016-03-001 2016/03/04 FAA 2016-04-06 This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category. CAA-2016-03-001.pdf
CAA-2016-02-007 2016/03/02 EASA 2016-0034 BR700-710A1-10 engines, manufacturer serial number (MSN) up to and including 11505 and equipped with low pressure turbine (LPT) module Part Number (P/N) M51-104 or P/N M51-111. BR700-710A2-20 engines, MSN up to and including 12492 and equipped with LPT module P/N M51-108 or P/N M51-111. and BR700-710C4-11 engines, MSN up to and including 15277, having configuration standard 710C4-11 engraved on the engine data plate and equipped with LPT module P/N M51-112. and BR700-710C4-11 engines, MSN up to and including 15329, having configuration standard 710C4-11/10 engraved on the engine data plate and equipped with LPT module P/N M51-112. CAA-2016-02-007.pdf
CAA-2016-02-006(已有後續修訂版) 2016/03/02 EASA 2016-0035 Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers (MSN). CAA-2016-02-006.pdf
CAA-2016-02-005 2016/03/01 FAA 2016-04-03 This AD applies to all The Boeing Company Model 747-400F series airplanes, certificated in any category. CAA-2016-02-005.pdf
CAA-2016-02-004 2016/03/01 FAA 2016-04-02 This AD applies to The Boeing Company Model 747-200C, -200F, -400, -400D, and -400F series airplanes; certificated in any category. CAA-2016-02-004.pdf
CAA-2016-01-003A 2016/02/22 EASA 2016-0010R1 Airbus A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A320-211, A320-212, A320-214, A320-215, A320-216, A321-111, A321-112, A321-211, A321-212, and A321-213 aeroplanes, all manufacturer serial numbers CAA-2016-01-003A.pdf
CAA-2016-02-003 2016/02/19 FAA 2016-03-06 (1) Model DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, and DC-9-15F airplanes. (2) Model DC-9-21 airplanes. (3) Model DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC 9 34F, and DC 9 32F (C-9A, C 9B) airplanes. (4) Model DC-9-41 airplanes. (5) Model DC-9-51 airplanes. (6) Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes. (7) Model MD-88 airplanes. (8) Model MD-90-30 airplanes. CAA-2016-02-003.pdf
CAA-2016-02-002 2016/02/17 EASA 2016-0028 SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers, if equipped with an internal life raft installation. CAA-2016-02-002.pdf
CAA-2016-02-001 2016/02/17 EASA 2016-0024 Part Number (P/N) PMC1102-02, P/N PMC3100-00 and P/N GMC1102-02 smoke detectors, having a date of manufacture (DMF, in digits as ‘MMYYYY’, e.g. 072010, see Appendix 2 of this AD) between November 2010 to January 2013 inclusive, and certain repaired units, as identified by P/N and serial number (s/n) in Appendix 1 of this AD. These smoke detectors are known to be installed on, but not limited to: Airbus A330, A330 Freighter and A380 aeroplanes by the aeroplane manufacturer on the production line; and in service by Supplemental Type Certificate (STC) modification on certain Airbus A319 and A320, Bombardier CL-600-2B19 (Challenger 850), Boeing (formerly McDonnell Douglas) DC-9 series 80, and Boeing 737-400(BDSF), 767 and 747-8 aeroplanes. CAA-2016-02-001.pdf
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