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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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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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Load testing a defective part (number 415-52129 Shaft Assembly Control Column) in the aileron control system.
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Correcting low oil temperature in the engine during cold weather operation.
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Downloadable paint scheme sheet for Piper PA-14.
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Instructions for safetying the terminal attachment nut on the magneto ground wire.
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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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At each 100 hour inspection, the bushing, washer and nut of the stabilizer yoke assembly should be inspected for wear and, if worn, should be replaced.
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Table of grommets used in wings and fuselage for covering Piper PA-18 aircraft.
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Steps to preclude opening of the cabin door in flight.