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.
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.
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) 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.
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.
This Continuing Airworthiness Notice (CAN) is issued to advise operators and maintainers of inspections required by the manufacturer to ensure the safe operation of affected fire buckets.
This Continuing Airworthiness Notice (CAN) is issued to bring attention to McFarlane Aviation Service Bulletin SB-10, dated 7 February 2020. The SB is applicable to Cessna 150, 152, 170, 172, 175, 180, 182, 185, 205 and 210 aircraft fitted with a McFarlan
This Continuing Airworthiness Notice (CAN) alerts operators of affected helicopters of the risk of fuel contamination when refuelling in dusty environments and mitigate the risk with good fuel-handling procedures when operating at remote locations.
Tail Wheel Spring Attachment
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
Stabiliser Hinge Assembly Fasteners - Inspection and Replacement
Kelly Fuel Pump Diaphragm Assembly
Liquefied Petroleum Gas (LPG) Fuel Cylinders used in Hot Air Balloons
Electronic Fuel Pumps P/N 7.21440.530
Aircraft Series Safety Recommendation
Nose Gear Link Assembly P/N 40336-000
Hose Unions at Fuel Control
Fuel Contamination due to Fuel Filler Cap Failure
Aircraft Fuel System
