Dockets

MCAI-2023-00996-T; Airbus Model A330-200, A330-200 F, A330-800, A330-900, A330-301, -302, -303, -323, -342, and -343 airplanes; and Model A340-312 and ​‑313 airplanes; main landing gear (MLG) axles.

AD-2024-00055-T; The Boeing Company Model 737-8, 737-8200, and 737-9 airplanes; aft rudder quadrant

MCAI-2023-00725-T; Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes; revised operational loads for some aircraft flight phases.

MCAI-2024-00069-R; for Bell Textron Canada Limited Model 505 helicopters. This AD was prompted by reports of cracked vertical stabilizer top end cap assemblies

MCAI-2023-00886-T; Bombardier, Inc., Model BD-700-2A12 airplanes; fan in a transformer rectifier unit (TRU)

MCAI-2022-00599-T; Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes; revise airworthiness limitations for brake accumulators.

AD-2023-00485-T; The Boeing Company Model 737-8 and Model 737-9 airplanes; standby power system control unit

AD-2023-01064-Q; Airplanes with certain Pacific Scientific Company rotary buckle assemblies (buckles) installed

AD-2023-01037-T; The Boeing Company Model 787-8, 787-9, and 787-10 airplanes; heat damage on engine inlets around the engine anti-ice (EAI) duct.

MCAI-2023-00353-R; Bell 407 fuel system stand pipe

MCAI-2023-01003-T; Airbus SAS Model A330-800 and A330-900 series airplanes; protective cap on drain hole of a fire extinguishing pipe.

MCAI-2023-01215-A; GA8 Airvan (Pty) Ltd Model GA8 and GA8-TC320 airplanes; Solenoid (Relay) Box Electrical Bonding