| Turbomeca TM 333 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Turbomeca |
| Aircraft Engine Type | Turboshaft |
| Dry Weight (kg) | 162.5 |
| Diameter (mm) | 454 |
| Length (mm) | 1045 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Turbomeca_TM_333 |
| Combustion Chamber | Annular, reverse flow |
| Maximum Takeoff Power (kW) | 736 |
| Compressor Description | Two-stage axial, single-stage centrifugal |
| Turbine Description | Single-stage compressor turbine, single-stage power turbine |