Vážení klienti, obchodní přátelé, dovolujeme si Vás informovat, že od 20.12. do 31. 12. 2024 čerpáme dovolenou. Opět se na Vás těšíme v novém roce 2025. Přejeme Vám klidné prožití Vánočních svátků a do nového roku vše nejlepší.
Tým NISA AIR
R66
TURBINE
SPECIFICATIONS
R66 Turbine | R66 Marine | |
---|---|---|
Engine | Rolls Royce RR300 Turbine | Rolls Royce RR300 Turbine |
Horsepower | 300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous | 300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous |
Maximum Gross Weight | 2700 lb (1225 kg) | 2700 lb (1225 kg) |
Approximate Empty Weight (including oil & standard avionics) | 1290 lb (585 kg) | 1355 lb (615 kg) |
Fuel Capacity (73.6 gal) | 493 lb (224 kg) | 493 lb (224 kg) |
Pilot, Passengers, and Baggage (with maximum fuel) | 917 lb (416 kg) | 852 lb (386 kg) |
Cruise Speed at Maximum Gross Weight | up to 110 kts (204 km/h) | up to 110 kts (204 km/h) |
Maximum Range (no reserve) | approximately 350 nm (650 km) | approximately 350 nm (650 km) |
Hover Ceiling IGE at Maximum Gross Weight | over 10,000 ft | over 10,000 ft |
Hover Ceiling OGE at Maximum Gross Weight | over 10,000 ft | over 10,000 ft |
Rate of Climb | over 1000 fpm | over 1000 fpm |
Maximum Operating Altitude | 14,000 ft | 14,000 ft |
Electrical System | 28 volt | 28 volt |