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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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Installation of safety belt extension on the front seat belt to eliminate deterioration due to rear seat heater damage and chafing.
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How to detect cracks or other damage in the forward wing spar cap.
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Steps to prevent weakening of the fuselage steel tubing cluster in the area of the rear wing spar attachment due to corrosion of the fuselage tubing.
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Attach an operating limitation placard to the instrument panel near the throttle control in full view of the pilot.
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Replace the aluminum front spar wing-to-fuselage attachment fittings with steel forgings.
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Attach an operating limitation placard to the instrument panel near the throttle in full view of the pilot.
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Steps to prevent rain water from entering the fuel tanks.