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As a precaution against possible cracking of the sliding window, at the knob, we recommend the following correction on airplanes in the above category.
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Inspect the fittings at each end of the elevator connector tube to determine if the end fittings are riveted to the tube with two rivets 90 degrees apart.
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Modifications to Decker 501A tail installation to prevent interference with the lower edge of the rudder under certain conditions.
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Failure of the fuel shut-off control attachment at the swivel fitting.
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Testing for secure attachment of flexible hose end fittings.
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Inspection of control cables and replacement of 1/8” 7 x 19 flexible stainless steel control cables on foreign registered airplanes.
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General specifications of the Piper PA-14 Family Cruiser.
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Rework to eliminate the possibility of the windshield coming out of its top retaining channel.
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Failure of the trim tab actuating wire directly in front of the tab control horn, has been reported. Failure of the wire in flight may cause the elevator to flutter.
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Procedures for replacing Magnesium Die Case Nose Wheel with a Permanent Mold Aluminum Alloy Nose Wheel.