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Rear and forward supports of both horizontal stabilizer modification.
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Modification for installing Silflex jack strut.
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Procedure for Installation of 180hp Franklin 6A335-B1 engine in lieu of original Franklin 6A4-165-B3.
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Steps to prevent weakening of the fuselage steel tubing cluster in the area of the rear wing spar attachment due to corrosion of the fuselage tubing.
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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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Drawing for the Piper PA-18 150hp Primer System.
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Downloadable paint scheme sheet for Piper J-3.
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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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Reports of collapsed wing mounted fuel tanks due to inadequate venting of the tank.
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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.