Vehicle

Convair 106 Skycoach

General Aviation and Light Aircraft

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
Piston 1
Status
Abandoned 1
Top Speed (km/h)
229 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Convair 106 Skycoach (Wikipedia)

Of Make

Source Convair 106 Skycoach (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Convair 106 Skycoach (Wikipedia)Lead, manufacturer
Quote, 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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