Helicopter
R66 NxG

Engine
Rolls-Royce RR300 Turbine
Horsepower
300 shp turboshaft; derated to 270 shp takeoff & 224 shp continuous
Maximum Gross Weight
2700 lb (1225 kg)
Approximate Empty Weight (Including Oil & Std Avionics)
1290 lb (585 kg)
Fuel Capacity / Weight
73.6 gal / 493 lb (224 kg)
Pilot, Passengers, and Baggage (with Maximum Fuel)
917 lb (416 kg)
Maximum Airspeed (Vne) at Maximum Gross Weight
130 kts (240 km/h)
Cruise Speed at Maximum Gross Weight
up to 110 kts (204 km/h)
Maximum Range (No Reserve)
approx 350 nm (650 km)
Hover Ceiling IGE at Maximum Gross Weight
over 10,000 ft
Hover Ceiling OGE at Maximum Gross Weight
over 10,000 ft
Rate of Climb
over 1000 fpm
Maximum Operating Altitude
14,000 ft
Electrical System
28 volt