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Download PDFs of various Attach Hardware Lists for Stinson 108 series aircraft.
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Download a color-coded chart showing the decimal equivalents for fractions from 1/64 inch to 1 inch.
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Inspect the stabilizer adjustment yoke for conformity with the approved drawing, and add reinforcement if the present one is unsatisfactory.
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Reports of breakage of the larger diameter tail brace wires (No. 8-36) and steps for replacing.
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Availability of required material and instructions for the installation of an approved shoulder harness at each seat location in all Pipers.
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Reinforcement of the stabilizer adjustment yokes due to cracks in the tubular stubs.
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Reported failures of the ribstitching both in the wing and control surface covering which may result in the fabric being torn from the structure while in flight.
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A noticeable aging of the spar finish occurs in listed airplane models that are continually exposed to adverse atmospheric conditions.
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Inspecting the condition of the seat bottoms and braces for cracks, and inspecting the control cables for wearing.
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Due to a number of reported failures of single strand .032" safety wire used on control system turnbuckles, it is considered necessary to replace the safety wire with single strand .040" brass or copper wire.