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Removing the R003-201 propeller blades and visually inspecting the propeller blade retainer ferrule for cracks.
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Instructions to prevent the entry of fire and fumes into the cabin compartment in the event of a powerplant fire.
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How to eliminate the possibility of confusion in the operation of the fuel selector valve.
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Procedure for replacing the fuselage gas tank overflow line due to the imperial brass compression sleeve having necked the line causing it to fail.
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Inspection of motor mount for cracks in the tubing near the welds, especially in the member from the top firewall bulkhead to the rear engine mounting bosses.
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Install a new battery box drain tube to extend at least 1/2 inch below the fuselage belly skin if this has not been already incorporated in the airplane.
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Specifications and performance data for Piper PA-22 "125" and "135" airplanes.
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Flexing of the lower aileron skin has resulted in fatigue cracks in the beam in the balance weight area.
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Remove the fairing at the wing root of each wing and inspect the wing root area for interference between the forward fuel line and the aileron cable and/or aileron pulley.
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Reinforce the upper end of the tie strap on the landing gear with a 4130 steel plate.