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Steps to prevent the possibility of a catastrophic accident in the event of tail brace wire failure.
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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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Installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion.
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Required inspection for incorrect swaging width of the cable Nicopress sleeves on the elevator, rudder, aileron, and flap control cables, and make a temporary POH limitation entry.
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Rigging and leveling procedures for Piper PA-12.
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Over time, a chafing condition resulting from the control cable sliding against the stationary pulley groove can cause the control cable to wear completely through, possibly resulting in loss of aileron control during flight.
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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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Downloadable paint scheme sheet for Piper J-3.
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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.
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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.