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Steps to prevent the possible loss of elevator trim control.
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General specifications and performance data for the Piper Vagabond PA-15 and the Piper Vagabond Trainer PA-17.
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Model PA-22 rigging procedure (supplement to PA-20 Rigging Procedure).
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How to prevent an inflight electrical system failure, smoke in the cockpit, and/or fire in the wire bundle behind the instrument panel.
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Method of effecting engine change for increased horsepower.
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Extreme surface corrosion has been found to exist inside the fuselage spar carry through structures of Luscombe Series 8 aircraft, particularly in those airplanes located near coastal areas.
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Rib repair diagram for Piper J-3, J-4, and J-5 aircraft.
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Inspecting the wing center section for evidence of corrosion through the installation of inspection openings and use use of a specified scope and light source.
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Determining the maximum and minimum lengths the tail brace wire should protrude through brass nipple U41051-000.
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The new Fuel Selector Valve, part number 11383-04, should be used for all service replacements and all new installations on Piper PA-18, PA-20 and PA-22 airplanes equipped with two wing fuel tanks.