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Revises compliance time, purpose, and instructions for inspection and/or replacement of wing lift strut assembly. Also announces the availability of new sealed lift struts.
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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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Vibration has caused the quick oil drain valve to break at the rubber washer seal and also at the point where the copper drain tube is soldered.
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Maintenance procedures for improving the reliability of the gascolator.
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Correcting the condition of the aileron cable pulleys rubbing on the fuel line in the area of the wing root leading edge and the upper end of the forward door post.
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There are several items of equipment in the engine installation which should be carefully inspected to insure satisfactory winter operation.
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Inspecting wings for broken drag wires.
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Recommendations to prevent motor mount failures.
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Installing tailspring attachment reinforcing units, part numbers 30882 and 30871, to prevent tailspring attachment failure.
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To provide inspection access for the lift strut attachment fitting on the forward side of the front spar and to provide details for the inspection of wing components for corrosion.