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Rigging and leveling procedure for Piper PA-20 airplanes.
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Over time, a chafing condition resulting from the control cable sliding against the stationary pulley groove can cause the control cable to wear completely through, possibly resulting in loss of aileron control during flight.
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Rigging and leveling procedures for Piper PA-12.
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Steps to prevent the possibility of a catastrophic accident in the event of tail brace wire failure.
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Extreme surface corrosion has been found to exist inside the fuselage spar carry through structures of Luscombe Series 8 aircraft, particularly in those airplanes located near coastal areas.
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General specifications of the Piper PA-11 Cub Special.
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Due to recurring failures of the control cables, all cables should be carefully inspected at each section which passes either over a pulley or through a fairlead.
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Cross reference chart of old Van Sickle part numbers to modern Cleveland mechanical brake and wheel part numbers.
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Rib repair diagram for Piper J-3, J-4, and J-5 aircraft.
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Rigging and leveling procedures for Piper J-3 Cub Special and PA-11 aircraft.