| SPECIFICATION | Airbus H125/B3e | |
|---|---|---|
| Engine | Safran Helicopter Engines Arriel 2D | |
| Maximum Takeoff Weight | 6173 lb (2800kg) | |
| Passenger Capacity | 5 +1 | |
| Standard Fuel Capacity | 940 lb (426 kg) | |
| Maximum Operating Altitude | 23000 ft | |
| Registered Mark | 9N-ANL | |
| SPECIFICATION | Airbus H125/B3e | |
|---|---|---|
| Engine | Safran Helicopter Engines Arriel 2D | |
| Maximum Takeoff Weight | 6173 lb (2800kg) | |
| Passenger Capacity | 5 +1 | |
| Standard Fuel Capacity | 940 lb (426 kg) | |
| Maximum Operating Altitude | 23000 ft | |
| Registered Mark | 9N-ANL | |
