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Reinforce the upper end of the tie strap on the landing gear with a 4130 steel plate.
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Prevention of possible failure of the engine mount.
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Inspection of aileron hinge reinforcing brackets to determine the type of material. All aluminum brackets are to be removed and replaced with steel brackets.
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Revising the present front and rear wing lift struts.
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Possibility of under-strength Nicopress sleeves in the control system.
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Installing a header tank in the fuel system to prevent engine malfunctioning caused by insufficient fuel flow.
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Inspect the shock struts for cracks at the ends of the stop bolt slots. Damaged struts shall be properly repaired or replaced.
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Examine immediately to ascertain that the fuel strainer is properly installed.
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How to prevent sudden failure of the fabric at the top of the windshield where the fabric attaches to the channel.
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Replace elbow to prevent possible fuel leakage where the elbow connects with the rear fuel valve.