Transport Atlas

How The World Moves
Sign In
Text size
100%
Theme
Vehicle

Beechcraft U-21 Ute

Military Aircraft

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
Year
1963 1
Engine Class
Turboprop 1
Top Speed (km/h)
426 1
Mass (kg)
2464 1
Maximum Mass (kg)
4377 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
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
View the Source
Comments (0)
No comments yet. Be the first to share a thought.
Reader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.