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The longitudinal trim system for the Ercoupe has been redesigned to employ a movable section on the trailing edge of the elevator.
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Reports of binding in the stabilizer rear support bearing and, as the link tube at the adjustment yoke is of similar construction, there is a possibility that the same difficulty may occur there.
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Downloadable paint scheme sheet for Piper PA-16.
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Inspection and rework to detect the use of improper screws attaching the left and right rudder pedal shaft assemblies to the nose wheel steering tie rods.
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Inspect front and rear control stick socket castings for cracks at the ears to which the push-pull tube attaches.
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To facilitate the inspection of Piper airplanes in the field, the Service Department has made up 100, 500 and 1000 hour inspection forms for Piper PA-18, PA-18A, PA-22, PA-23 and PA-24 models.
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Contains the Ceconite Application, Maintenance and Repair Procedures for Piper PA-18 and PA-25 models.
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Specifications and performance data for Piper PA-18 with Continental 90hp and Lycoming 108hp engines.
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Verify that the propeller is properly indexed to the crankshaft flange.
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Instructions to preclude failure of brittle bolts and the danger of the nose wheel turning crosswise during landing on aircraft incorporating Electrol hose gear with aluminum scissors.