Kamow / Kamov Ka-226
Light Utility Helicopter
The Kamov Ka-226 is a twin-engined light utility helicopter with coaxial rotors developed by the Russian manufacturer Kamov JSC, produced by the Russian manufacturer KumAPE JSC. The Ka-226 can be operated with or without the interchangeable mission pod (cabin). The main roles include police operations, search and rescue, medical evacuation, disaster relief, air ambulance, firefighting and gas field support operations for Gazprom.
The Kamov Ka-226 is a development of the
Kamov Ka-26 with turboshaft engines. The higher performance version Ka-226T is powered by two Turbomeca Arrius 2G1 turboshaft engines.
Propulsion | 2 Turboshaft Engines |
Engine Model | Allison / Rolls-Royce 250-C20R/2 |
Engine Power (each) | 336 kW | 450 shp |
Speed | 206 km/h | 111 kts 128 mph |
Service Ceiling | 3.500 m | 11.483 ft |
Range | 600 km | 324 NM 373 mi. |
Empty Weight | 1.950 kg | 4.300 lbs |
max. Takeoff Weight | 3.400 kg | 7.495 lbs |
Rotor Blades (main/tail) | 3/3 |
Main Rotor Diameter | 13,00 m | 42 ft 8 in |
Rotor Disc Area | 132,7 m² | 1428 ft² |
Length (Fuselage) | 8,10 m | 26 ft 7 in |
Length | 13,00 m | 42 ft 8 in |
Height | 4,15 m | 13 ft 7 in |
First Flight | 04.09.1997 |
Production Status | in production |
Developed from | Kamow / Kamov Ka-26 |
ICAO Code | K226 |
Data for (Version) | Kamov / Kamow Ka-226 |