9N AJN Engine


9N AJN Helicopter

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.



SPECIFICATION R66 TURBINE
Engine Rolls-Royce RR300 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 up to 125 kts (144 mph)
Maximum Range (no reserve) approx 350 nm (400 sm)
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

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