Piper PA-31T
Piper PA-31T Cheyenne | |
---|---|
Type: | Business jet |
Design country: | |
Manufacturer: | |
First flight: |
29th August 1969 |
Commissioning: |
1970 |
Number of pieces: |
847 |
The Piper PA-31T Cheyenne is a light twin-engine turboprop propeller aircraft produced by the US aircraft manufacturer Piper Aircraft Corporation and a further development of the Piper PA-31 Navajo .
history
The original version of the aircraft was an upgraded version of the Piper Navajo with a pressurized cabin . The new aircraft was with two Pratt & Whitney Canada PT6 A-28 turboprop engines equipped. The aircraft was continuously improved in various further developments. Ultimately, the development resulted in Piper's largest aircraft, the PA-42 Cheyenne III and IV .
Versions
- PA-31T Cheyenne
- First built version, powered by two 462 kW Pratt & Whitney Canada PT6A -28 turboprop engines .
- PA-31T-1
- Initial designation of the later PT-31T Cheyenne II, powered by two 373 kW Pratt & Whitney Canada PT6A-II turbo test engines.
- PT-31T Cheyenne II
- Much improved variant of the first version.
- PT-31T Cheyenne IIXL
- Extended Cheyenne powered by two 559 kW Pratt & Whitney Canada PT6A-135 turboprop engines.
Technical specifications
Parameter | Cheyenne I | Cheyenne II |
---|---|---|
crew | 1 | |
Passengers | 6th | 7th |
length | 10.57 m | |
span | 12.40 m | 13.00 m |
height | 3.89 m | |
Wing area | 21.3 m² | |
payload | 1709 kg | 1809 kg |
Empty mass | 2206 kg | 2241 kg |
Max. Takeoff mass | 3915 kg | 4050 kg |
Cruising speed | 437 km / h | 463 km / h |
Top speed | 461 km / h | 542 km / h |
Service ceiling | 8595 m | 9631 m |
Range | 2241 km | 2432 km |
Engines | two propeller turbines Pratt & Whitney PT6A-11 each with 368 kW |
two propeller turbines Pratt & Whitney PT6A-28 with 456 kW each |
Comparable aircraft types
See also
Web links
Commons : Piper PA-31T Cheyenne - Collection of pictures, videos and audio files
Individual evidence
- ↑ Roger Peperell: Piper Aircraft - Freedom of Flight Supplement , Air-Britain, Tonbridge 2020, ISBN 978-0-85130-524-0 , S. 81st
- ^ Peter Bachmann: Einmotorige & Zweimotorige Flugzeug , Motorbuch-Verlag 1980