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Per Lycoming Division of Avco Corporation, it is permissible to use a torque value of 40 inch pounds to provide adequate tightness to maintain proper engine support in lieu of the linear dimension as previously specified.
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Instructions for inspecting the battery box lid for proper clearance between the lid and the battery terminals.
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Inspection of all PA-20 name plates and those bearing the model designation "PA-20A" be removed and returned to the Factory Service Department for replacement.
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Installing an additional standard fuse (15A Bussman #AGC-15) in the wire between the cigar lighter and the ammeter at the next 100 hour inspection to protect against a short circuit condition.
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Modification of the cabin heat box plate to prevent interference with the movement of the safety belt attaching link.
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Installation of a placard on the Pilot's instrument panel warning against using improper procedures in applying the parking brake.
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Inspection of the aluminum fuel lines forward of the fuel valve.
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Incorporating a new style stop on the brake lever to prevent the brake lever from hitting the gas line.
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Incorporating a heavy duty navigation light switch, Piper part number 484-575, manufactured by the Ohmite Manufacturing Company.
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Inspecting the engine mount to determine if there is any evidence of fatigue cracks in the vicinity of the welds at both the firewall and the engine attachment points.