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Instructions to prevent possible leakage of carbon monoxide into the cabin heater system in airplanes utilizing Avcon Industries, Inc., kits with defective mufflers.
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Last Updated: 10/11/2021
in Technical Information Stinson
This 90 page document contains the production history of Stinson 108 Series aircraft, listed by serial number.
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Extreme surface corrosion has been found to exist inside the fuselage spar carry through structures of Luscombe Series 8 aircraft, particularly in those airplanes located near coastal areas.
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Over time, a chafing condition resulting from the control cable sliding against the stationary pulley groove can cause the control cable to wear completely through, possibly resulting in loss of aileron control during flight.
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Procedure for inspection of the wing center section to establish the condition of the center section structure.
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Rigging and leveling procedures for Piper PA-12.
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Directions to prevent failure of the upper wing front spar strut fittings, P/N 2-1976, that could result
in an in-flight separation of the wing.
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General specifications of the Piper PA-11 Cub Special.
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Due to recurring failures of the control cables, all cables should be carefully inspected at each section which passes either over a pulley or through a fairlead.
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How to prevent engine stoppage or malfunction due to the accumulation of water or other contaminants in the fuel system.