Convair 106 Skycoach

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Model 106 Skycoach
Role 4-seat light aircraft
National origin United States
Manufacturer Convair
First flight April 1946[1]
Number built 1[1]

The Convair Model 106 Skycoach was an

Stinson Division of Convair at the end of World War II.[1]

Design and development

The Model 106 was a four-seat cabin aircraft with a

piston engine, driving a cooling fan and pusher propeller.[1]

Flight testing was carried out at San Diego, but performance was found to be unexceptional, comparing very poorly to the contemporary Beechcraft Bonanza, which could cruise at 165 mph (143 kn; 266 km/h) on only 165 hp (123 kW). With a maximum speed of only 142 mph (123 kn; 229 km/h) the Model 106 was hopelessly outclassed and Convair abandoned development, scrapping the sole prototype, (regn. NX40004, msn. 1), in 1947.[1]

Specifications (Model 106 Skycoach)

Data from General Dynamics aircraft and their predecessors[1]

General characteristics

Performance

  • Maximum speed: 142 mph (229 km/h, 123 kn)

See also

Aircraft of comparable role, configuration, and era

  • Anderson-Greenwood AG-14

References