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Correction to Owner's Handbooks for the listed models.
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Increase in gross weight 1800 to 1950 pounds (Lycoming 0-290-d engine) (125 hp only).
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Tightening engine mounting bolts to obtain a torque of (40) inch pounds.
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Immediate inspection of clearance between the aileron cable and the master switch wires (from the master switch to the ammeter).
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Inspection to determine if there is interference between the inboard end of the front spar web and the aileron pulley attachment bolt in the area of the front wing hinge fitting.
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Instructions for sealing any gaps or holes in the firewalls with non-hardening fireproof putty.
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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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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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Testing for secure attachment of flexible hose end fittings.