| Arriel 2D 130 ✕ | |
|---|---|
| Family | Arriel |
| Aircraft Engine Manufacturer | Safran Helicopter Engines |
| Aircraft Engine Type | Turboshaft |
| Comment | H130 |
| Dry Weight (kg) | 132 |
| Length (mm) | 1140 |
| Height (mm) | 616 |
| Width (mm) | 492 |
| Control System | FADEC Dual Channel |
| Certification | 2011-01-01 |
| Modules | 5 |
| Time Between Overhaul (h) | 4000 |
| Fuel | Jet-A1 |
| LP Compressor Stages | 0 |
| IP Compressor Stages | 0 |
| HP Compressor Stages | 2 |
| HP Compressor Technology | 1 axial, 1 centrifugal |
| Combustion Chamber | Annular |
| HP Turbine Stages | 1 |
| HP Turbine Technology | axial |
| IP Turbine Stages | 0 |
| LP Turbine Stages | 1 |
| LP Turbine Technology | axial |
| Maximum Takeoff Power (kW) | 710 |
| Maximum 30min Power (kW) | 710 |
| Maximum Continuous Power (kW) | 637 |
| Output Take Off Speed (rpm) | 6000 |
| Output Clockwise Rotation | Yes |