The Beechcraft Queen Air is a twin-engined light aircraft that Beechcraft produced in numerous versions from 1960 to 1978. It was based on the Twin Bonanza, sharing key components such as wings, engines and tail surfaces, but with a larger fuselage, and it served as the basis for the highly successful King Air series of turboprop aircraft. The first model, the Beech 65, is a nine-seat low-wing cantilever monoplane with retractable tricycle landing gear, initially powered by two 340 hp Lycoming IGSO-480 piston engines. The prototype first flew on 28 August 1958 and the type certificate followed on 4 February 1959. The United States Army ordered 68 early in development as the L-23F. Its main uses have been as a private aircraft, a utility aircraft and a small commuter airliner.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Beechcraft Queen Air (Wikipedia)
Of Make
Source Beechcraft Queen Air (Wikipedia)
Sources
1. Beechcraft Queen Air (Wikipedia)
Design and development, first flight
The prototype Beech 65 first flew on August 28, 1958
Lead
is a twin-engined light aircraft produced by Beechcraft
Design and development
Lycoming IGSO-480 six-cylinder, horizontally opposed piston engines
Design and development, series end
The Queen Air series ended in 1978
Specifications (Queen Air B80), empty weight
Empty weight: 5,277 lb (2,394 kg)
Specifications (Queen Air B80), max takeoff weight
Max takeoff weight: 8,800 lb (3,992 kg)
Specifications (Queen Air B80), maximum speed
Maximum speed: 215 kn (247 mph, 398 km/h)
Lead, manufacturer
is a twin-engined light aircraft produced by Beechcraft in numerous versions from 1960 to 1978
Design and development, country of origin
Early in development the United States Army, which had been a customer of the Twin Bonanza
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