-
Mandatory replacement of airspeed indicators.
-
Installation of safety belt extension on the front seat belt to eliminate deterioration due to rear seat heater damage and chafing.
-
Provisions for locking the sliding windows with or without the green sunshade.
-
Subject: Typical and maximum number of exposed strut threads as permitted for rigging on Piper aircraft. Applicability: Piper J-3, J-4, J-5, and PA-11 through PA-22 Download PDF: Lift-Strut-Fork-Extension.pdf Piper Strut Thread (Typical ...
-
Inspect the fittings at each end of the elevator connector tube to determine if the end fittings are riveted to the tube with two rivets 90 degrees apart.
-
Inspect the two aileron stop pins (Taylorcraft P/N A-235) of the aileron control assembly.
-
Examine the two flexible fuel lines to determine whether the hose inner liner has collapsed or failed thus causing a restriction to the flow of fuel.
-
Steps to preclude weld separations on the end of the landing gear shock strut assembly.
-
Failure of a fuel pump pressure line, due to chafing on the nose cowl has resulted in a change in the routing of the fuel pump lines.
-
Checking the attachment of the rudder control arm on the torque tubes.