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The Robinson R66 Turbine retains many of the design features of the R44, including a two-bladed rotor system, T-bar cyclic, and an open interior cabin configuration. Notable differences are the R66's increased reserve power, improved altitude performance, fifth seat, and large baggage compartment. Popular upgrades including HID landing lights, leather seats, and a stereo audio control panel are standard in the R66.
Using the following configurator you can check the price of the new R66 depending on the selected options:
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| R66 TURBINE Specification | |
| Engine | Rolls-Royce 250-C300/A1, 300 shp turboshaft |
| Horsepower | derated to 270 shp for takeoff and 224 shp continuous |
| Maximum Gross Weight | 1225 kg |
| Approximate Empty Weight (including oil & std avionics) |
581 kg |
| Fuel Capacity (280 l) | 224 kg |
| Pilot, Passengers and Baggage with Maximum Fuel |
420 kg |
| Max Airspeed (Vne) | 212,4 km/h |
| Cruise Speed | up to 240 km/h |
| Maximum Range (no reserve) | approx 650 km |
| Hover Ceiling (IGE) at Maximum Gross Weight | over 3100 m |
| Hover Ceiling (OGE) at Maximum Gross Weight | over 3100 m |
| Rate of Climb | over 5m/s (300m/min) |
| Maximum Operating Altitude | 4300 m |
| Electrical System | 28 volt |
