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Instructions for applying the recommended fuel valve lubricant in the listed Piper models.
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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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Points to remember when conducting routine inspections of the oil cooler lines and fittings.
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Federal Aviation Agency release pertaining to flight control hazards and protection from icing.
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Proper maintenance and inspection procedures of exhaust systems and heat exchangers for the listed models.
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Availability of a modification kit to incorporate the latest type carburetor air filter system on the aircraft models listed above.
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Instructions for the removal and replacement of brake drums on Goodrich D3-13A-1 wheels.
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Wood circuit protectors incorporate a safety feature that allows the circuit to be broken manually by pulling out the circuit protector push-pull button.
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Procedures for replacing brake drum flanges on PA-22, PA-23, PA-24 and PA-25 wheel assemblies.
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A list of the various finishes used on the interior and exterior of all Piper aircraft models J-3 thru PA-30, dated 1950 through 1964.