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Information regarding modification of the shimmy dampener to prevent separation between the assembly body and the end plate.
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Update to Service Letter #209.
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To aid in the identification of both types (old vs. new) of fuel tank caps for the Piper PA-22 airplanes, we have provided sketches on the reverse side
of this letter.
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Instructions for more rigid visual inspections of the engine and nose wheel mounts for indication of cracks at each of the 100 hour inspections.
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Closer inspection required of the brake cable and pulleys is necessary to find frayed or broken cables, generally where the cable contacts the pulleys.
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Reports have been received indicating that movement of the nose gear can be restricted due to binding of the upper nose gear oleo bearing due to lack of lubrication.
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Installation of Muffler Support Kit No. 756-803, and Tailpipe Support Kit No. 756-804, will be instrumental in extending the service life of the exhaust system.
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Specifications and performance data for Piper PA-20 "125" and "135" airplanes.
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At each 100 hour inspection, the bushing, washer and nut of the stabilizer yoke assembly should be inspected for wear and, if worn, should be replaced.
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Increase in gross weight 1800 to 1950 pounds (Lycoming 0-290-d engine) (125 hp only).