| Arrano 1A ✕ | |
|---|---|
| Family | Arrano |
| Aircraft Engine Manufacturer | Safran Helicopter Engines |
| Aircraft Engine Type | Turboshaft |
| Comment | H160 |
| Dry Weight (kg) | 200 |
| Length (mm) | 1150 |
| Width (mm) | 570 |
| Control System | FADEC Dual Channel |
| Modules | 5 |
| Fuel | Jet-A1 |
| LP Compressor Stages | 0 |
| IP Compressor Stages | 0 |
| HP Compressor Stages | 2 |
| HP Compressor Technology | 2 centrifugal |
| Combustion Chamber | Annular reverse flow |
| HP Turbine Stages | 1 |
| HP Turbine Technology | axial |
| IP Turbine Stages | 0 |
| LP Turbine Stages | 1 |
| LP Turbine Technology | axial |
| Maximum Takeoff Power (kW) | 862 |
| Output Take Off Speed (rpm) | 8000 |
| Output Clockwise Rotation | No |