The single-engine, four-seat, fixed-gear, high-wing, Stinson 108 series was built with a six-cylinder
Franklin engine -- 6A4-150, or 6A4-165, normally -- driving a fixed-pitch propeller. The
fuselage is of fabric-covered steel tube. Aftermarket modifiers have obtained
supplemental type certificates (STC) allowing conversion to an aluminum covering. Many different engines have been installed in the 108 by STC such as the
Lycoming O-360,
Franklin O-350,
Continental O-470. In 1948, however, overproduction in the US general aviation industry led to a glut of light aircraft, with unsold 108s being stored, and on 30 June 1948, Convair shut down the Stinson factory. The name and assets of Stinson (including 200 unsold 108s) were sold to
Piper Aircraft on 1 December 1948, with Piper setting up a Stinson division in April 1949 to sell the complete aircraft inherited from Convair, and to assemble a further 125 aircraft from spare parts. These aircraft were marketed as Piper-Stinson 108s. Total new production of the Stinson Model 108, by Stinson, was 5,260; this total does not include the two converted prototypes. Stinson delivered approximately 4,935 aircraft and Piper delivered approximately 325 aircraft. Piper later sold the type certificate to
Univair Aircraft Corporation. Univair built and certified the model 108-5, but built only one example. Total new model production by Stinson and Univair was 5,261 aircraft. ==Variants==