-
Incorporating a thru bolt (AN3-14) instead of the spring clip which was used to attach the control stick tube to the stub.
-
Increase in gross weight 1800 to 1950 pounds (Lycoming 0-290-d engine) (125 hp only).
-
Safety measure to prevent possible icing of the lower end of the crankcase breather tube.
-
Determine if the attachment of the rudder control arm to the torque tube has been reinforced by a steel strap.
-
Inspect wing strut attachment fittings on lower fuselage longerons for cracks or evidence of poor weld.
-
Rigging and leveling procedures for Piper PA-15 and PA-17.
-
Instructions for applying the recommended fuel valve lubricant in the listed Piper models.
-
Installing an improved forward fuel header tank with thicker walls and welded seals, which provides greater resistance to impact rupture in the event of an accident.
-
Replacing leaky fuel tank with one made of stainless steel or aluminum alloy before the next flight.
-
Immediate changes necessary in the bungee installation.