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The described procedure provides the best performance and observance of proper mixture control will materially decrease fuel consumption.
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The front ash trays shall be modified to the self-contained type or a "No Smoking" placard installed.
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Inspection of the flexible hose in the engine breather line for contraction and possible clogging.
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Replacing aluminum alloy fitting AN914-2D, which is located between the fuel filter and the carburetor, with copper alloy fitting AN914-2.
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It has been found necessary to provide a positive lock on the zipper at the bottom of the baggage compartment to eliminate the possibility of it opening while in flight, and having articles fall into the controls.
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Inspection of front stabilizer fittings for cracks.
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Aircraft equipped with either a single or dual fuel quantity gauge installation must have the placard installed.
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Prevent possible resonant vibratory conditions with McCauley Model 1A200/HFA fixed pitch propellers installed on Lycoming 0-360-C2A, or -C2E type engines.
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Reports of fraying of the control column cable assemblies resulting from contact of the cable assemblies with the set screw in the aileron stops.
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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.