The Convair Model 106 Skycoach was an experimental four-seat light aircraft designed and built by the Stinson Division of Convair at the end of World War II. It had a pusher layout with a fixed spatted tricycle undercarriage and twin tail booms flanking the propeller, with the pilot and three passengers in a cabin in the fuselage nacelle ahead of a 230 horsepower Franklin six-cylinder piston engine. Flight tests at San Diego found the performance unexceptional, with a top speed of 142 miles per hour against a Beechcraft Bonanza that cruised at 165 miles per hour on less power. Convair abandoned development and scrapped the sole prototype in 1947.
Facts
Engine Class Top Speed (km/h) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Convair 106 Skycoach (Wikipedia)
Of Make
Source Convair 106 Skycoach (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Convair 106 Skycoach (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
designed and built by the Stinson Division of Convair
Sources
1. Convair 106 Skycoach (Wikipedia)
Lead
was an experimental four-seat light aircraft
Design and development
Convair abandoned development, scrapping the sole prototype
Design and development, engine class
Franklin 6A8-225-B8 six-cylinder horizontally-opposed piston engine
Specifications (Model 106 Skycoach)
Maximum speed: 142 mph (229 km/h, 123 kn)
Lead, manufacturer
designed and built by the Stinson Division of Convair
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