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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.
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Testing for secure attachment of flexible hose end fittings.
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Testing for secure attachment of flexible hose end fittings.
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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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A noticeable aging of the spar finish occurs in listed airplane models that are continually exposed to adverse atmospheric conditions.
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Tightening engine mounting bolts to obtain a torque of (40) inch pounds.
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Replacing the shimmy dampener currently installed in the affected model aircraft with new shimmy dampener, part number 13086-00, and instructions for continuing maintenance at regular intervals.
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Increase in gross weight 1800 to 1950 pounds (Lycoming 0-290-d engine) (125 hp only).
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Approximate amount of materials required to recover PA-20 and PA-22 models using raw fabric and cellulose acetate butyrate dope.
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Model PA-22 rigging procedure (supplement to PA-20 Rigging Procedure).