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Beechcraft T-6 Texan II

Military Aircraft

The Beechcraft T-6 Texan II is a single-engined turboprop trainer aircraft built by Textron Aviation and formerly manufactured by Raytheon Aircraft Company. It is a license-built development of the Pilatus PC-9, modified by Beechcraft to enter the Joint Primary Aircraft Training System competition in the 1990s, with a low-wing cantilever monoplane layout, enclosed tandem seating, a single Pratt and Whitney Canada PT6A-68 turboprop and Martin-Baker Mark 16 ejection seats. It replaced the United States Air Force Cessna T-37B Tweet and the Navy T-34C Turbo Mentor during the 2010s. The T-6A was introduced at Moody and Randolph Air Force Bases in 2000 and 2001, and the Air Force awarded the full-rate production contract in December 2001. The Royal Canadian Air Force flies it as the CT-156 Harvard II, and the Greek, Israeli and Iraqi air forces use it for basic flight training.

Facts
Year
2000 1
Engine Class
Turboprop 1
Status
In Production 1
Mass (kg)
2135 1
Maximum Mass (kg)
2948 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Beechcraft T-6 Texan II (Wikipedia)

Of Make

Source Beechcraft T-6 Texan II (Wikipedia)
Sources
1. Beechcraft T-6 Texan II (Wikipedia)
  • Operational history, introduction
    The T-6A was introduced to Moody Air Force Base and Randolph Air Force Base in 2000
  • Lead
    is a single-engined, turboprop aircraft currently built by Textron Aviation
  • Specifications (T-6A)
    Pratt & Whitney Canada PT6A-68 turboprop
  • Lead, production
    currently built by Textron Aviation
  • Specifications (T-6A), empty weight
    Empty weight: 4,707 lb (2,135 kg)
  • Specifications (T-6A), max takeoff weight
    Max takeoff weight: 6,500 lb (2,948 kg)
  • Lead, country of origin
    The T-6A is used by the United States Air Force for basic pilot training
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