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Instructions for correcting an incorrectly installed pointer on the fuel selector valve.
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Failures of the diaphragm in the B711 Scott Master Cylinder used on the PA-22 Tri-Pacer within 300 or 400 hours of operation.
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A recent survey of PA-20 and PA-22 aircraft has revealed that a certain number of these airplanes are operating with the strainer to carburetor flexible fuel line in a deteriorated condition.
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It is recommended that a #6 x 3/8" Parker Screw be installed in the rudder pedal tube clamp of the right hand rudder pedals to eliminate the possible rotation of the rudder pedal cross tube on the torque tube arm.
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The installation of a spacer plate will in most cases completely eliminate any thumping which the nose wheel now makes at full extension.
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Instructions for sealing any gaps or holes in the firewalls with non-hardening fireproof putty.
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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.