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Inspect landing gear shock strut end fittings for cracks or other defects in the small bend radii.
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Effective on all Ercoupes serially numbered 2623 and subsequent, the engine cowling will be secured with Camloc fasteners.
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Visual inspection of the throttle cable and housing for fatigue and possible cracking.
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Reports of breakage of the larger diameter tail brace wires (No. 8-36) and steps for replacing.
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Recommended modifications for winter operations of Piper J-3, PA-11 and PA-12 aircraft.
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Mandatory replacement of 1/8 - 7 x 19 flexible stainless steel control cables to prevent cracked nicopress sleeves.
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Replace each of the four internal wrenching bolts which attach the engine to the engine mount with an AN 6 bolt and a special offset washer.
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Frequently check for leakage or seepage of the fuselage fuel tank, and check all plumbing connections for proper tightness and weld seams of the tank for possible cracks.
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Instructions for replacing wing fuel tanks constructed of ternplate with aluminum tanks.
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Installing a spring on the fuel shut-off to assist opening of the valve.