| Allison T40 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Allison |
| Aircraft Engine Type | Turbopropulsor |
| Dry Weight (kg) | 1133.981 |
| Diameter (mm) | 596.9 |
| Length (mm) | 4241.8 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Allison_T40 |
| Fuel | 100/130 Gasoline or Kerosene based jet fuel |
| Combustion Chamber | 8 can-type per power-section |
| Maximum Takeoff Power (kW) | 3803.069 |
| Power To Weight (kW/kg) | 3.653 |
| Specific Fuel Consumption (g/(kW·h)) | 383.2 |
| Compressor Description | 17-stage axial flow (2 of) |
| Turbine Description | 4-stage axial flow (2 of) |