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Instructions for installing shock cords on Piper PA-12 and PA-14 aircraft.
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The following is cited from LPC Bulletin 1033, the installation instructions for the PA-22 taildragger conversion.
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Corrosion between the aluminum terminal and aluminum wire at the battery positive post, resulting in overheating of the wire due to high electrical resistance.
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Cross reference chart of original Piper part numbers mapped to current part numbers.
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Replacement of front lift strut wing attachment fittings to prevent failure of lift strut wing fitting due to tie-down loads.
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Several accidents have occurred involving engine fuel starvation attributed to a lack of detent action in the fuel selector valve.
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Required inspection for incorrect swaging width of the cable Nicopress sleeves on the elevator, rudder, aileron, and flap control cables, and make a temporary POH limitation entry.
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Last Updated: 10/11/2021
in Technical Information StinsonThis 90 page document contains the production history of Stinson 108 Series aircraft, listed by serial number.
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Replacing certain fuel selector valve cams or fuel selector valves that Cessna shipped from December 6, 1998, through May 10, 1999.
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Provides inspection and fatigue life requirements applicable to the wing lift strut forks.