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If the window catch does not properly engage its mating part, which is riveted to the door frame, it is suggested that the door frame catch be relocated to insure proper fit.
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Inspect for and detect any internal or external corrosion of the wing lift strut tube, and thereby prevent wing strut failure and inflight separation of the wing from the airplane resulting in loss of control of the airplane.
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Procedure for examining both left and right Univair hydrasorb (U486-604-1) for any possible cracks or irregularities.
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Correction to Service Letter Number 126 regarding Metal Spar Splice Kits.
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Steps to preclude failure of the U12694 series throttle cables, which could cause loss of full travel of the throttle control.
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The use of standard inspection methods to determine any presence of unauthorized holes or cracks in the main spar assembly or any components thereof.
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Outlines the repair of Univair STC'd Stamped Ribs in accordance with the original STC and FAA Advisory Circular AC 43.13-1B.
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Download PDF Type Certificate Data Sheets for Ercoupe, Forney, Alon and Mooney M10 aircraft.
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Download PDF Type Certificate Data Sheets for Aeronca, Champion, Citabria and Bellanca aircraft.
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Download PDF Type Certificate Data Sheets for Taylorcraft Model A Series, B Series, F-19, F-21 and F-21A aircraft.