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Download PDFs of various Attach Hardware Lists for Piper J-3.
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Inspection of the left and right wing front and aft lift struts for cracks and corrosion.
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Recommended repair and alteration for fraying rudder cables.
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Emphasizes proper wheel bearing greasing procedures.
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Instructions for installing conventional landing gear on Piper PA-22 Series aircraft per STC SA45RM.
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Inspect wing drag wire system for loose or broken drag wires and inspect ribs for damage.
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In devising a system of identification for fixed pitch propellers, Sensenich Corporation worked out a code system which not only identifies the propellers, but also describes them.
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To preclude the possibility of in-flight fires, the following inspection and rework is necessary to eliminate combustible material and possible ignition sources from the area aft of the firewall underneath the forward cabin floor.
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Prevent failure of the fuel line fittings or the gascolator due to the current airplane design configuration. Such failure could result in a lack of fuel to the engine with consequent loss of control of the airplane.
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Inspecting for weld separation where the rudder pedal cable attachment fitting is welded to the rudder pedal.