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.
CAA have received a report from a maintenance provider of finding a cracked tail rotor control pedal assembly at the RH seat location on a Cabri G2. For further information refer to Figures 1 and 2 in the CAN.
CAA have received a defect report of a finding of significant damage in the wing rear spar to fuselage attach fittings on a Cresco aircraft caused by movement of the bolts.
The purpose of this Continuing Airworthiness Notice (CAN) is to alert operators and maintainers of Guimbal Cabri G2 helicopters of a possible safety issue with the main rotor flight control pitch links.
This Continuing Airworthiness Notice (CAN) is issued to bring attention to two defect reports submitted to the CAA for Cessna 208B aircraft. The first report is about finding severely corroded and cracked elevator torque tubes on a Cessna 208B, and the second report is about finding a corroded rudder torque tube assembly on another Cessna 208B aircraft.
The purpose of this Continuing Airworthiness Notice (CAN) is to alert operators and maintainers of the importance of accomplishing a thorough inspection of the flap supports and rollers bearings for wear and corrosion. Service experience indicates the possibility of flap support wear by the flap roller bearings. Failure to accomplish a thorough inspection of the flap supports and roller bearings could result in damage to the flap supports, restriction of flap free movement, and a possible flap asymmetric condition.
This Continuing Airworthiness Notice (CAN) is issued to bring attention to Dart Aerospace USA Inc. Service Bulletin SB19-4, dated 19 July 2018 applicable to Bell 206/407 series helicopters and Agusta A109/A119 series helicopters embodied with Dart Aerospa
This Continuing Airworthiness Notice (CAN) alerts operators of affected helicopters of the importance of installing a guard fence between the forward two-place seat and the pilot seat to protect the collective control area from inadvertent damage and/or p
This Continuing Airworthiness Notice (CAN) is prompted by the latest revision of Robinson Helicopter Company (RHC) R22 Service Bulletin SB-109A “Bladder Fuel Tank Retrofit” dated 15 January 2018. The intent of the CAN is to ensure that all operators/maint
Incorrect installation of the stowage tray can result in an undetected gap between the tray and the aft bulkhead through which loose stowed equipment can enter the flight control system.
AS350 Resistance Type Fuel Quantity Indication System (FQIS).
Main Gear Retraction Arms P/N 42042-000 & P/N 42042-002
All Piper aircraft models fitted with a Gascolator (also called a fuel strainer or fuel filter) to separate contaminants from the fuel system.
Robinson R44 Helicopters Flight Control Hydraulic Servos
Series Aircraft Rudder Pedal Assemblies
Primary Flight Control Yoke Inspection
Ethanol Blended Auto Fuel
Aircraft fitted with a Pneumatic Pressure Operated Gyro Instrument System
