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 pitch link assemblies. This CAN is re-issued at revision 1 to raise awareness of the instructions in Guimbal SB 21-006B, which provides inspections and preventative maintenance actions related to the safety concern identified in this CAN.
This Continuing Airworthiness Notice (CAN) revised to expand the CAN applicability and bring attention to cracks found in the elevator bellcrank assembly brackets P/N 0411289-1 and P/N 0411290 on a second Cessna A152 aeroplane.
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) is issued to bring attention to an airworthiness concern with G205 stick grips manufactured by The Ray Allen Company fitted on aircraft with a horizontal stabiliser electric pitch trim system. This CAN is also ap
This Continuing Airworthiness Notice (CAN) is issued to bring attention to a recent airworthiness concern with the flaperon control system on an Avid C model Mk 4 aircraft. Other Avid aircraft variants fitted with flaperons, including early Kitfox aircraf
Tail Wheel Spring Attachment
This Continuing Airworthiness Notice (CAN) is issued to bring attention to a recent airworthiness concern reported to the CAA. Several Cresco and FU24 aircraft were found to have incorrect aileron rigging.
This Continuing Airworthiness Notice (CAN) alerts operators of affected aircraft of the importance of attaching the shoulder harness to the lower bar of the seatback frame.
This CAN is issued to alert operators and maintainers of a recent failure of a tail rotor fork bolt P/N 369A1602-3 on a Hughes 369D helicopter. The bolt should be installed using the elongation method to ensure proper clamp-up of the tail rotor hub and fo
To advise aircraft operators and maintainers that the CAA has received a number of reports of finding cracked TRBs with P/N C029-1 and C029-2 on Robinson R44 series helicopters.
RHC SB-83 requires the introduction of a Special Pilot Caution into the AFM u
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
Liquefied Petroleum Gas (LPG) Fuel Cylinders used in Hot Air Balloons
Robinson R22 Main Rotor Drive System and Drive Belts
Series Aircraft Rudder Pedal Assemblies
MDHI Torque Event Inspections
Ethanol Blended Auto Fuel
