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Information regarding modification of the shimmy dampener to prevent separation between the assembly body and the end plate.
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Load testing a defective part (number 415-52129 Shaft Assembly Control Column) in the aileron control system.
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The use of automotive type gasoline in General Aviation aircraft is believed to be a contributing factor in numerous accident investigation reports.
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Procedure for visual inspection of coating on fuel gauge cork floats and inner fuel tanks for deterioration.
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This service release announces the field availability of a new current production Forward Fuel Header Tank which provides greater resistance to impact rupture in the event of an accident.
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Subject: This comprehensive inspection report provides recommendations for an inspection program per requirements of FAR Part 43 and Advisory Circular 91-60 (The Continued Airworthiness of Older Airplanes). Applicability: J-2 Series Cub J-3...
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Downloadable paint scheme sheet for Piper PA-14.
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Steps to preclude opening of the cabin door in flight.
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Instructions for safetying the terminal attachment nut on the magneto ground wire.
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Incorporating a heavy duty navigation light switch, Piper part number 484-575, manufactured by the Ohmite Manufacturing Company.