| Powerplant | Turbomeca Arrius 2R (uninstalled thermodynamic rating)
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| Takeoff | 505 shp | 377 kW
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| Max Continuous | 459 shp | 342 kW
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| Hover Ceiling IGE | 14,450 ft | 4,404 m
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| Hover Ceiling OGE | 10,460 ft | 3,188 m
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| Max Cruise | 125 kts | 231 km/h
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| Service Ceiling (Pressure Altitude) | 18,610 ft PA | 5,672 m PA
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| Range at VLRCMGW, Sea Level, ISA, no reserve | 306 nm | 566 km
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| Max Endurance (No reserves, 60 KIAS) | > 3.9+ hrs
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| Baggage Compartment Volume | 18 ft3 | 0.5 m3
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| Cabin Floor Area** | 22 ft2 | 2.0 m2
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| Empty Weight - (base aircraft) | 2,180 lbs | 989 kg
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| External Useful Load | 2,295 lbs | 1,041 kg
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| Internal Useful Load | 1,500 lbs | 680 kg
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| Max Gross Weight (external) | 4,475 lbs | 2,030 kg
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| Max Gross Weight (internal) | 3,680 lbs | 1,669 kg
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| Standard avionics features include |
Fully integrated Garmin G1000H™ flight deck with twin 10.4” LCD screens reduces pilot workload.
Traffic Information System (TIS)
Moving Map display
Diagnostics/maintenance page
Airport diagrams
Flight Planning
Power Situation Indicator (PSI)
Engine Instruments and Crew Alerting System (EICAS)
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| Optional flight displays |
increase situational awareness
Helicopter Terrain Awareness and Warning System (HTAWS)
Garmin’s Helicopter Synthetic Vision Technology™ (HSVT)
“Pathway in the Sky” display
Traffic Alert System (TAS)
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| Engine Instrument and Crew Alert System (EICAS) | Integrated engine display using Bell patented Power Situation Indicatovr (PSI) and visual and aural crew alert system on Primary and Multifunction Displays
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| Optional Autopilot | Two and Three Axis Autopilot Available
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