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Procedure for dye penetrant inspection of control column tee for evidence of cracks.
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Prevention of cracks developing in the side flanges of the stabilizer attaching bracket.
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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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Testing for secure attachment of flexible hose end fittings.
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Modifying the battery box lid to eliminate the possibility of "shorting" the battery terminal wing nuts.
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Installing an additional standard fuse (15A Bussman #AGC-15) in the wire between the cigar lighter and the ammeter at the next 100 hour inspection to protect against a short circuit condition.
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Procedures for replacing Magnesium Die Case Nose Wheel with a Permanent Mold Aluminum Alloy Nose Wheel.
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Instructions for installing Micarta fairleads on the fifth and eighth nose ribs to prevent slack aileron cables from rubbing on the metal edge.
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Modifications to the fuel injector vent.
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Approved changes to make the heat control on the instrument panel more readily accessible for a pilot flying solo in the rear seat.