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R66 Turbine

 

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.

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.

With continued focus on safety, the R66 meets the latest FAA crashworthiness regulations.

Specifications & Dimensions

Helicopter                                                                        R66 Turbine with Pop-Out Floats

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 & standard avionics)                                1355 lb (615 kg)

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

Pilot, Passengers, and Baggage

(with maximum fuel)                                                       852 lb (386 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

R44 Raven II 

 

Four-seat Robinson R44 Raven II helicopters are high performing, reliable and easy to maintain. R44s have a two-bladed rotor system, T-bar cyclic and the latest in Robinson technology including streamlined instrument panels and crashworthy bladder fuel tanks.

The R44’s aerodynamic fuselage optimizes airspeed and fuel economy. Hydraulic controls eliminate feedback forces and provide responsive handling. A low tail-rotor tip speed, newly designed muffler and large cambered tail reduce flyover noise.

Raven II helicopters are powered by Lycoming’s IO-540 fuel injected engine. The IO-540 delivers better altitude performance, increased payload and eliminates the need for carburetor heat.

Specifications & Dimensions

HelicopterR44 Raven II

Engine                                                                                                       Lycoming IO-540, six cylinder, fuel injected Lycoming

Horsepower                                                                                             Derated to 245 for takeoff and 205 continuous

Maximum Gross Weight                                                                        2500 lb              (1134 kg)

Approximate Empty Weight (including oil & standard avionics)    1505 lb               (683 kg)

Standard Fuel                                                                                          29.5 gal     177 lb (80 kg)

Auxiliary Fuel                                                                                           17.0 gal      102 lb (46 kg)

Pilot, Passengers, and Baggage (with standard fuel)                       818 lb                  (371 kg)

Cruise Speed at Maximum Gross Weight                                           up to 109 kts (202 km/h)

Maximum Range (no reserve)                                                               approx 300 nm (550 km:

Hover Ceiling IGE                                                                                    8950 ft @ 2500 lb

Hover Ceiling OGE                                                                                  7500 ft @ 2300 lb

Rate of Climb                                                                                           over  1000 fpm

Electrical System                                                                                    28 volt

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