| Aircraft Engine Manufacturer |
Pratt & Whitney Canada |
| Aircraft Engine Type |
Turbopropulsor |
| Dry Weight (kg) |
390.5 |
| Diameter (mm) |
635 |
| Length (mm) |
2046 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Pratt_%26_Whitney_Canada_PW100 |
| Fuel |
PW150: Kerosene Jet A, A-1/JP8; Wide Cut Jet B/JP4; High Flash JP5/JP1 |
| Combustion Chamber |
Reverse flow combustor |
| Maximum Takeoff Power (kW) |
1342 |
| Power To Weight (kW/kg) |
150 |
| Compressor Description |
Two-spool, single-stage centrifugal LP + single-stage centrifugal HP :: PW150: Two-spool, three-stage axial LP + single-stage centrifugal HP |
| Turbine Description |
Single-stage HP and LP turbines, two-stage power turbine |