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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-2010-01-011A 2010/05/28 ANAC 2010-01-02R1(BRAZIL) This Airworthiness Directive (AD) is applicable to Embraer models ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-100 SR, ERJ 190-200 IGW, ERJ 190- 200 LR and ERJ 190-200 STD airplanes equipped with Air Management System (AMS) controller cards part number (P/N) 1001050-1-YYY or P/N 1001050-2-YYY containing software version Black Label 08 or lower installed.
CAA-2009-08-010A 2010/05/28 ANAC 2009-08-02R1(BRAZIL) This Airworthiness Directive (AD) is applicable to EMBRAER models ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 LR, ERJ 190- 200 STD and ERJ 190-200 IGW airplanes equipped with Goodrich Corporation door-mounted escape slide part number (P/N) 104003-1.
CAA-2006-11-004E(已有後續修訂版) 2010/05/28 ANAC 2006-11-01R5 This Airworthiness Directive is applicable to Embraer models ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR e ERJ 190-200 IGW airplanes equipped with Hamilton Sundstrand Low Pressure Check Valve (LPCV) part numbers (P/N) 1001447-3 and/or 1001447-4.
CAA-2010-05-010(已有後續修訂版) 2010/05/27 EASA 2010-0100-E(BRAZIL) SA 365 N1, AS 365 N2, N3 helicopters delivered before 01 May 2010, flying in IMC (Instrumental Meteorological Conditions), IFR (Instrument Flight Rules) or Night VFR (Visual Flight Rules) conditions, if equipped with the vertical gyro units GV76-1 installed on the rear left hand (LH) or rear right hand (RH) rack, on which modification 365P081895 (reinforcement of rack for vertical gyro unit GV76-1 in the rear compartment) has not been incorporated.
CAA-2010-05-009 2010/05/26 Transport Canada Civil Aviation CF-2010-16 Bombardier Inc. Model DHC-8 Aeroplanes, as follows: DHC-8 Series 100, 200, and 300, serial numbers 003 through 566; and DHC-8 Series 400, serial numbers 4001, 4003, 4004, 4006, 4008 through 4274
CAA-2010-05-008(已有後續修訂版) 2010/05/20 EASA 2010-0091 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-2010-05-007 2010/05/20 FAA 2010-11-52 Model S-76A, B, and C helicopters, with LITEF LCR-100, part number (P/N) 145130-7100, Attitude Heading and Reference System (AHRS) Unit, installed, certificated in any category.
CAA-2010-04-002A 2010/05/20 EASA 2010-0062R1 Halon 1211 (BCF) fire extinguishers, identified by serial number (s/n) and Part Number (P/N) in Fire Fighting Enterprises Ltd (FFE) Alert Service Bulletin (ASB) 26-116 issue B and The affected fire extinguishers are used in passenger cabins and lavatory waste bins and are known to be installed (or carried/stowed on board) on, but not limited to, Adam Aircraft Industries, Airbus, Aircraft Industries a.s (formerly LET), Alenia, BAE Systems, Boeing, Britten-Norman, Embraer, Fokker, Hawker Beechcraft (formerly Raytheon) and Pilatus aeroplanes, and Agusta and Eurocopter helicopters.
CAA-2008-02-004A 2010/05/20 EASA 2008-0034R1 Airbus Model A320-111, A320-211, A320-212, A320-214, A320-215, A320- 216, A320-231, A320-232 and A320-233 aeroplanes, all manufacturer’s serial numbers, if equipped with Hamilton Sundstrand/Dowty Ram Air Turbine (RAT) Part Number (P/N) 680203037 with a Serial Number (S/N) from 0101 to 0354 inclusive, except aeroplanes which have received Airbus modification 27189 in production or Airbus Service Bulletin (SB) A320-29-1100 in service, and without having received Airbus modification 28413 in production. Reminder: It is the responsibility of the operator to ensure that any RAT replaced on aircraft after having complied with this AD, still complies with the requirements of this AD.
CAA-2010-05-006 2010/05/18 FAA 2010-10-02 Model S-76A, B, and C helicopters, with a main rotor servo actuator (servo actuator), Sikorsky Aircraft Corporation (Sikorsky) part number (P/N) 76650-09805-109 or -110 (also marked as HR Textron or Woodward HRT P/N 3006760-109 or -110), installed, certificated in any category.
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