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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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Aircraft equipped with either a single or dual fuel quantity gauge installation must have the placard installed.
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Installing an ash tray cover as an additional safety feature.
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Examine immediately to ascertain that the fuel strainer is properly installed.
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The tube clamps used to secure the muffler to the exhaust stacks have not been providing satisfactory service in that they permit the muffler to loosen and move around.
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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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Remove the auxiliary rudder stops to eliminate the possibility of the bellcrank flange catching on the bolt heads and locking the system.
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Partial or almost complete loss of rudder control of one or both rudders due to partial failure of the rudder horn attachments.
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Steps to preclude loss of control of the airplane as a result of failed nicopress sleeves in the control system.
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Inspection and repair of Lycoming engine mounts.