Engine
Rolls-Royce RR300 turboshaft engine
Horsepower
300 shp (takeoff), approx. 275 shp continuous
Internal Payload
Approx. 430 kg
Fuel Capacity (180 gal)
180 U.S. gallons (approx. 681 liters)
Pilot, Passengers, and Baggage with Maximum Fuel
1 pilot + 1 passenger + limited baggage
Passengers
1–4 occupants (typically 1 student in military training configuration)
Maximum Range (no reserve)
Approx. 660 km
Endurance with Standard Fuel
Approx. 3.5–4 hours
Hover Ceiling IGE at Maximum Gross Weight
Approx. 2,100 m
Hover Ceiling OGE at Maximum Gross Weight
Approx. 1,200 m
Maximum Operating Altitude
Approx. 4,300 m
Cabin Volume Total
Approx. 2.3 m³
Crew Area
Side-by-side dual controls, NVG compatible
Main Cabin
Modular cabin for training and light mission roles
Cargo Area
Rear cabin area, optional external cargo hook