The Piper PA-31T Cheyenne is a turboprop development of the earlier PA-31P Pressurized Navajo.
[edit] Development
Originally, the aircraft was an upgraded version of the Pressurized Navajo equipped with two Pratt & Whitney Canada PT6A-28 turboprop engines. Later, the aircraft was further refined and developed, including aerodynamic improvements and fuselage extensions. The PA-31T led to the development of the PA-42 Cheyenne III and IV.
[edit] Variants
- PA-31T Cheyenne
- Initial production version, powered by two 620-shp (462-kW) Pratt & Whitney Canada PT6A-28 turboprop engines.
- PA-31T-1
- Original designation of the PT-31T Cheyenne II. Powered by 500-shp (373-kW) Pratt & Whitney Canada PT6A-II turboprop engines.
- PT-31T Cheyenne II
- Improved version, renamed version of original powered by two 620-shp (462-kW) Pratt & Whitney Canada PT6A-28 turboprop engines.
- PT-31T Cheyenne IIXL
- Stretched version, powered by two 750-shp (559-kW) Pratt & Whitney Canada PT6A-135 turboprop engines.
[edit] Specifications
Data from Jane's all The World's Aircraft 1976-77 [1]
General characteristics
Performance
- Maximum speed: 326 mph (525 km/h, 283 knots) at 11,000 ft (3,360 m)
- Cruise speed: 244 mph (393 km/h, 212 knots) at 25,000 ft (7,600 m)
- Stall speed: 88 mph (142 km/h, 77 knots) (flaps down)
- Range: 1,702 mi (2,739 km, 1,478 nmi) (econ cruise, 45 min reserves)
- Service ceiling: 29,000 ft (8,840 m)
- Rate of climb: 2,800 ft/min (14.2 m/s)
[edit] See also
- Aircraft of comparable role, configuration and era
[edit] References
- ^ Taylor 1976, pp. 358–359.
- Taylor, John W.R. Jane's All The World's Aircraft 1976-77. London:Jane's Yearbooks, 1976, ISBN 0-354-00538-3.
[edit] External links
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