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Inspection of the wing forward spar fuselage attachment assembly for cracks or corrosion, and replacing or repairing any cracked or corroded part.
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Steps to prevent possible fuel unbalance and fuel line chafing.
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Reports of broken core strands in the rudder cables where they pass over the pulley at fuselage Station 18.75.
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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 left and right wing front and aft lift struts for cracks and corrosion.
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Inspect the two aileron stop pins (Taylorcraft P/N A-235) of the aileron control assembly.
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Reports of interference between the elevator horn bolt and the fin cover plate apparently caused by improper field installation of the cover plate through bolt.
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Inspect wing strut attachment fittings on lower fuselage longerons for cracks or evidence of poor weld.
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To reduce the amount of oil passing through the breather tube and exhausting on the under-side of the aircraft, Continental Motors Corporation has a newly designed engine fitting which extends further into the engine case.
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In order to supply an alternate source of breather air to eliminate the possibility of pressurizing the engine case in the event that icing occurs at the breather tube end, a slot has been added to the lower portion of the breather tube.