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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).
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Correction to Owner's Handbooks for the listed models.