The experimental YO-50 was a high-wing braced monoplane with fixed tail wheel landing gear and extensive cabin glazing. Fitted with full-span leading edge slots and slotted flaps, and powered by a 420 hp Ranger SGV-770B-3 twelve-cylinder air-cooled inverted V-engine, the YO-50 had STOL performance. The three YO-50s were produced under the s/n 42-741 to
42-743, and was first flown in 1940, while on June 1, 1941, the USAAC took delivery of the first."
Span: 55 ft 6 in (16.92 m)
Length: 35 ft 2 in (10.82 m)
Load: 700 lb (318 kg)
Loaded weight: 3,887 lb (1,763 kg)
Max speed: 133 mph (214 kmh)
Cruise speed: 120 mph (193 kmh)
Landing speed: 43 mph (69 kmh)
Range: 410 mls (660 km)