Doug Robertson's Photo Gallery

2010 Robinson R66, one Rolls-Royce 250-C300/A1 Turboshaft derated to 270 sHp for takeoff, 224 shaft Hp max continuous. No.3 R66 build. Experimental R&D class. On SZP Helipad.

2010 Robinson R66, one Roll-Royce 250-C300/A1 Turboshaft derated to 270 sHp for takeoff, 224 sHp continuous. Experimental class, No.3 R66 build. On SZP Helipad.

2010 Robinson R66, one Rolls-Royce 250-C300/A1 Turboshaft derated to 270 sHp for takeoff, 224 shaft Hp max continuous. Experimental class R&D. No. 3 build R66, liftoff.

2010 Robinson R66, one Rolls-Royce 250-C300/A1 Turboshaft 270 sHp for takeoff derated to 224 max continuous sHp, Experimental class R&D-No. 3 R66 build. Departure SZP Helipad.

2010 Robinson R66, one Rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp continuous, rotor 404-412 rpm, 5 seats, Experimental class R&D, N4512G is 3rd prototype R66, on SZP helipad

2010 Robinson R66, one Rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp max continuous, Experimental class R&D, 3rd prototype R66, on SZP helipad

2010 Robinson R66, one Rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp max continuous, Experimental class R&D, third prototype, five seats, on SZP helipad

2010 Robinson R66, one Rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp max continuous, cabin doors-seating for five, two plus three across in back

2010 Robinson R66, one rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp max continuous, panel

2010 Robinson R66, one Rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp max continuous, panel

2010 Robinson R66, one Rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp max continuous, 3rd prototype, anti-torque rotor assembly

2010 Robinson R66, one Rolls Royce 250-C300/A1 Turboshaft derated to 270 shp for takeoff, 224 shp max continuous, rotor hub turns 404 to 412 rpm