The five-seat R66 Turbine helicopter is reliable, economical and easy to maintain. R66s have a two-bladed rotor system, T-bar cyclic and the latest in Robinson technology including streamlined instrument panels, energy absorbing seats and crashworthy bladder fuel tanks.  What distinguishes the R66 is a spacious 300 lb capacity baggage compartment and the Rolls Royce RR300 turboshaft engine. The RR300 engine operates on readily available Jet A fuel and offers increased reserve power, additional payload and improved altitude performance. Hydraulic controls eliminate feedback forces and provide responsive handling.

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Outfitted with pop-out floats, the R66 Turbine Marine offers an additional level of safety for over-water travel. Designed for emergencies, the six-chamber floats inflate within 2-3 seconds of activation.  The installation adds approximately 65 pounds to the helicopter’s empty weight. When not in use, floats roll-up and stow in protective covers along the aircraft’s landing skids. The streamlined, low profile design minimizes drag and allows for easy entry and exit of the cabin.

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Specifications

Engine:  Rolls Royce RR300 Turbine

Horsepower:  300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous

Maximum Gross Weight:  2700 lb (1225 kg)

Approximate Empty Weight 
(including oil & std avionics):  1280 lb (581 kg)

Fuel Capacity:   (73.6 gal) 493 lb (224 kg)

Pilot, Passengers and Baggage (with maximum fuel):  927 lb (420 kg)

Cruise Speed at Maximum Gross Weight:  up to 110 kts (204 km/h)

Maximum Range (no reserve):  approximately 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