| Arriel 2C ✕ | |
|---|---|
| Family | Arriel |
| Aircraft Engine Manufacturer | Safran Helicopter Engines |
| Aircraft Engine Type | Turboshaft |
| Comment | AC312A |
| Dry Weight (kg) | 131 |
| Length (mm) | 1015 |
| Height (mm) | 576 |
| Width (mm) | 498 |
| Control System | EECU single Channel |
| Certification | 1997-08-01 |
| Modules | 5 |
| Time Between Overhaul (h) | 3500 |
| 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) | 626 |
| Maximum Continuous Power (kW) | 581 |
| OEI30sec Power (kW) | 718 |
| OEI2min Power (kW) | 646 |
| OEI Continuous Power (kW) | 626 |
| Output Take Off Speed (rpm) | 6000 |
| Output Clockwise Rotation | Yes |