The purpose of this CAN is to notify operators and maintenance providers of two recent reports provided to CAA of MD369 Tail rotor gearbox (TGB) input pinion shaft failures.
CAA have received a report of a Cessna 152 aircraft experiencing a jammed rudder (deflected to one side) during take-off, because of a failed steering tube.
The purpose of this continuing Airworthiness Notice is to provide guidance regarding the assessment whether an engine qualifies for a time between overhaul extensions per the requirements in Lycoming SI 1009BC.
The purpose of this CAN is to notify helicopter operators and maintenance providers of a recent accident in which an MD369E suffered a separation failure of a main rotor blade.
The purpose of this CAN is to notify helicopter operators and maintenance providers of a number of recent occurrences reported to CAA of finding excessive play in AS350 tail rotor pitch control rod ball joints. Recently reported findings appear limited to pitch control rods manufactured under a FAA PMA by EXTEX.
This Continued Airworthiness Notice (CAN) alerts operators and maintenance providers of possible safety concerns related to incorrect assembly of the throttle cable to the Fuel Control Unit (FCU) on Gippsland GA8 Airvan aircraft.
This Continuing Airworthiness Notice (CAN) is issued to bring attention to defect reports submitted to the CAA of finding corrosion in the attachment lugs of fuselage extrusion P/N 28-2-1095-1 on five P2008 aircraft. For further details of the location of the corrosion found, refer to the photos in this CAN.
This Continuing Airworthiness Notice (CAN) is issued to bring attention to a defect report submitted to the CAA of finding cracks in the stabilator torque tubes on ten P2008 aircraft. For further details of the location of the cracks found, refer to the two photos in this CAN.
The purpose of this CAN is to notify affected helicopter operators and maintenance providers of a recent occurrence reported to the CAA of finding a significant crack in the tail rotor gearbox on a 369D helicopter.
CAA received a report from a maintenance provider of finding an Airwolf Aerospace Tension-Torsion strap with a PMA/STC holder log card which specified an incorrect life limit.
The purpose of this Continuing Airworthiness Notice (CAN) is to provide guidance for aircraft operators and maintenance engineers regarding compliance with Airworthiness Directives.
The purpose of this CAN is to notify helicopter operators and maintenance providers of a recent occurrence reported to the CAA of significant cracks found in the 4 Bladed Tail Rotor Hub of a MD500 helicopter.
The purpose of this CAN is to notify helicopter operators and maintenance providers of a recent occurrence reported to CAA of a winch cable which was damaged during a winching operation.
This Continuing Airworthiness Notice (CAN) is issued to bring attention to an issue reported to the CAA recently, where MS21042L3 nuts appeared to lose their self-locking function during installation.
The purpose of this CAN is to notify helicopter operators and maintenance providers of two recent occurrences reported to CAA of helicopter windows departing the aircraft doors during the first flight following window installation.
The purpose of this CAN is to notify helicopter operators of a number of recent occurrences recently reported to CAA of failures of lifting equipment, specifically load cells.
The purpose of this CAN is to notify MD369 helicopters operators and maintenance providers of occurrences recently reported to CAA of finding duplex bearing distress in numerous MD369 Tail Rotor Gearboxes (TRG).
The purpose of this Continuing Airworthiness Notice (CAN) is to provide guidance about manufacturers’ service information, such as Service Bulletins (SB), Service Letters (SL) etc.
The purpose of this Continuing Airworthiness Notice (CAN) is to advise MD helicopter operators and maintainers of a possible safety concern with the thruster control output drum assembly..
The purpose of this Continuing Airworthiness Notice (CAN) is to advise operators and maintainers of Guimbal Cabri G2 helicopters, of a possible safety issue with the main rotor swashplate assembly.
