Kazan Ansat
Light Utility Helicopter
The Kazan Ansat is a twin-engined ten-seat light utility helicopter produced by the Russian manufacturer Kazan Helicopters JSC.
Propulsion | 2 Turboshaft Engines |
Engine Model | Pratt & Whitney Canada PW207K |
Engine Power (each) | 470 kW | 630 shp |
Speed | 285 km/h | 154 kts 177 mph |
Service Ceiling | 5.700 m | 18.701 ft |
Range | 635 km | 343 NM 395 mi. |
Empty Weight | 2.000 kg | 4.409 lbs |
max. Takeoff Weight | 3.300 kg | 7.275 lbs |
Rotor Blades (main/tail) | 4/2 |
Main Rotor Diameter | 11,50 m | 37 ft 9 in |
Tail Rotor Diameter | 2,00 m | 6 ft 7 in |
Rotor Disc Area | 103,9 m² | 1118 ft² |
Length (Fuselage) | 11,18 m | 36 ft 8 in |
Length | 13,64 m | 44 ft 9 in |
Height | 3,56 m | 11 ft 8 in |
First Flight | 17.08.1999 |
Production Status | in production |
ICAO Code | A2RT ANST |
Data for (Version) | Kazan Ansat |