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Inspection to ascertain that the flattened tube end fitting at each end of the connector tube is riveted in place as shown in sketch.
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Correction to the fuel grade specification in flight manuals and fuel tank placards for the Lycoming O-290-D2 engines.
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Compromised structural integrity of the fuselage due to excessive rust and corrosion between steel tubing and preformed sheet steel material.
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Inspect for interference between the nose cowl and starter ring gear casting and for tightness of the cowl attachments.
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Inspection of the hinge assembly and correction of rivet fatigue.
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The installation of a spacer plate will in most cases completely eliminate any thumping which the nose wheel now makes at full extension.
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Shock cord application chart for listed Piper models.
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Replacing U.S. Rubber Co. flexible ducts installed in the carburetor hot air system with P-208-S duct or P-208 duct coated with neoprene.
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Changes to prevent cracks occurring in the region of the uppermost rivet used to attach the stiffener to the side cowl.
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Instance of a crack developing in service across a jury strut fitting on a lift strut.