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 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.
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 a significant crack found in the upper vertical fin of a Hughes 369HS helicopter.
This Continuing Airworthiness Notice (CAN) is revised to advise operators and maintainers that MDHI have released Service Letter SL369H-158, SL369D-142, SL369E-097, SL369F-088, SL500N-044, SL600N-038 (issued as a single document) and updated the relevant aircraft ICA and introduced an inspection for the pilots interconnecting cyclic pitch torque tube assembly. The inspection includes a freedom of movement check of the torque tube and bearings.
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 revised to advise operators and maintainers that Schweizer has issued Temporary Revision No. 269C-80 applicable to the Handbook of Maintenance Instructions and Schweizer Service Information Letter (SIL) No. L-188 is now available.
This Continuing Airworthiness Notice (CAN) is issued to advise operators and maintainers of a defect report received by the CAA which identified a crack in a vertical fin spar on a MBB-BK117 helicopter.
This Continuing Airworthiness Notice (CAN) is issued to draw operators and maintainers' attention to the potential for contact between the fuel tank supporting structure and the braided hydraulic line.
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 inform aircraft operators and maintenance providers that the CAA recently became aware of a clutch assembly defect (i.e. spalling damage to a C166-5 shaft). There have been several mid-life sprag failures in R44 helicopters over the past 15 years. In response to these failures the CAA issued DCA/R44/23B to inspect the clutch oil for contamination every 500 hours TIS. The damaged shaft was not found as a result of an inspection in accordance with DCA/R44/23B and there were no sprags found damaged or broken.
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 CAN is prompted by CAA awareness of several cargo hooks in New Zealand being damaged due to torsional loads. Loads attached to a cargo hook with a spreader bar (e.g. a fertilizer bucket) may cause the cargo hook to be subjected to high torsional loads which can damage the cargo hook. To ensure continued airworthiness of the hook, additional inspections, certain on-condition repairs, and/or appropriate replacement actions have been added to the manufacturers CMM. Refer to Onboard Systems CMM 122-015-00 for the new/additional inspections required for cargo hooks used for torsional load applications.
This Continuing Airworthiness Notice (CAN) is issued to bring attention to a recent failure of a rudder steering bracket P/N D60-5710-20-00-NPC on a Diamond DA 42 aircraft.
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 advise operators and maintainers that Aeroprakt Ltd has issued Service Bulletin A32-06, dated 2 December 2019 with instructions to inspect the windscreen fitted on A-32 and A-32L (Vixxen) aircraft.
Textron Aviation Inc. (formerly Cessna Aircraft Company) model 206, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 206H and T206H aircraft, all S/N.
