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Verify that the propeller is properly indexed to the crankshaft flange.
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Inspection of bottom rib of rudder for kinks or cracks in the rib flanges just aft of the rudder horn fitting.
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Checking the operation of the voltage regulator by observing the ammeter reading.
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Inspect elevator cables for signs of fraying; replace pulleys with ones of larger radius.
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Information on the required considerable re-design of the aircraft structure to accommodate the increased gross weight and higher engine horsepower when converting a Stinson Model 108 to Model 108-1 or -2.
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Inspection, cleaning and replacement of upper bearing in the oleo strut.
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Load testing a defective part (number 415-52129 Shaft Assembly Control Column) in the aileron control system.
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Concern of dissimilar metal corrosion occurring where the steel elevator control horn attaches to the aluminum lateral stiffener located within the elevator assembly.
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Incorporating a thru bolt (AN3-14) instead of the spring clip which was used to attach the control stick tube to the stub.
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Contains the Ceconite Application, Maintenance and Repair Procedures for Piper PA-18 and PA-25 models.