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Cracking in the leading edge of the streamlined tube of the landing gear at the point where the tube joins the inboard end of the axle.
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To eliminate the possibilities of main gear tire wear due to misalignment, the following methods may be used for checking and correction.
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Inspecting wings for broken drag wires.
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Adding strips of felt to the gas tank cover to improve the clearance between the cover reinforcements and the tank.
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As a precautionary measure, the Civil Aeronautics Authority requests that the bug screen installed inside the carburetor air scoop be removed.
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Immediate inspection of clearance between the aileron cable and the master switch wires (from the master switch to the ammeter).
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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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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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Steps to prevent fire hazard in the charging circuit.
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Failure of the floorboard and rudder pedal lug attachment to the tubular structure due to continued flexing of these parts during operation.