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 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) 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.
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) is issued to bring attention to a defect reported to the CAA of finding a severely cracked Pilot to Co-pilot Tail Rotor Torque Tube with P/N 369H7531-11 on a Hughes 369FF (MD530F) helicopter. The investigation re
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
This Continuing Airworthiness Notice (CAN) alerts operators that it is the responsibility of the pilot to ensure that a Robinson R22 series helicopter fitted with a Helipod NZ Limited spray system is operated within the weight and balance limitations spec
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
The aircraft maintenance manual provides instructions to ensure an aircraft can be maintained in an airworthy condition.
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.
Stabiliser Hinge Assembly Fasteners - Inspection and Replacement
AS350 Resistance Type Fuel Quantity Indication System (FQIS).
Main Gear Retraction Arms P/N 42042-000 & P/N 42042-002
Control Column Grip
Cessna 150/152 Series Horizontal Stabiliser Spars - Cracks.
Cessna 200 Series Horizontal Stabilisers
Aircraft Series Safety Recommendation
Forward Spar Attach Brackets
Nose Gear Link Assembly P/N 40336-000
Aircraft fitted with a Pneumatic Pressure Operated Gyro Instrument System