The Beechcraft U-21 Ute is an American utility aircraft built by Beechcraft for the United States Army. It began as a re-engined turboprop version of the Queen Air: in 1963 Beechcraft fitted a Model 65-80 Queen Air with two Pratt and Whitney Canada PT6A-6 turboprops as the Model 87, a proof of concept for the King Air, and its Army designation moved from L-23G to NU-8F and then YU-21. The Army awarded a production contract for the U-21A in October 1966, an aircraft that kept the unpressurized Queen Air fuselage and added the wings, tail and undercarriage of the King Air, carrying up to ten passengers in troop transport configuration. Some were built or modified for signals intelligence as the RU-21, and many were sold to civil buyers as military surplus after the Army retired them.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Beechcraft U-21 Ute (Wikipedia)
Of Make
Source Beechcraft U-21 Ute (Wikipedia)
Sources
1. Beechcraft U-21 Ute (Wikipedia)
Design and development, prototype conversion
In 1963, Beechcraft modified a single Model 65-80 Queen Air
Lead
is an American utility aircraft built by Beechcraft for the United States Army
Specifications (U-21A)
Pratt & Whitney Canada T74-CP-700 (PT6A-20) turboprop engines
Specifications (U-21A), empty weight
Empty weight: 5,434 lb (2,464 kg)
Specifications (U-21A), max takeoff weight
Max takeoff weight: 9,650 lb (4,377 kg)
Specifications (U-21A), maximum speed
Maximum speed: 265 mph (426 km/h
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