| Turbomeca Makila ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Turbomeca |
| Aircraft Engine Type | Turboshaft |
| Dry Weight (kg) | 278.9 |
| Diameter (mm) | 498 |
| Length (mm) | 1836 |
| Height (mm) | 620 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Turbomeca_Makila |
| Combustion Chamber | Annular |
| Maximum Takeoff Power (kW) | 1801 |
| Compressor Description | 3-stage axial flow LP, single-stage centrifugal flow HP (both mounted on HP shaft) |
| Turbine Description | 2-stage axial flow HP turbine, 2-stage axial flow free power turbine with rearwards output shaft |