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Attach an operating limitation placard to the instrument panel near the throttle in full view of the pilot.
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In order to prevent the seat belt anchorage from failing during crash landings, it has been found necessary to modify the seat installation as follows.
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Heat output of the heaters provided with the single opening exhaust system can be increased by incorporating the following changes.
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Instructions for applying the recommended fuel valve lubricant in the listed Piper models.
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Increase in gross weight 1800 to 1950 pounds (Lycoming 0-290-d engine) (125 hp only).
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Reports of fuel seepage into the space between the inner cabin trim and the outer fabric covering of the fuselage.
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Inspection of aileron hinge brackets to false spar attachment fittings for cracks.
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Reports of broken core strands in the rudder cables where they pass over the pulley at fuselage Station 18.75.
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There have been field reports of severe corrosion in the outer wing panel structure of several aircraft. The most effective means of preventing corrosion damage is early identification and correction.
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Failures of lift struts caused by abuse, failure to replace lift struts after ground accidents, and the use of damaged parts from scrapped airplanes as service replacement parts.