Attribute | Value |
---|---|
General | |
Manufacturer | Kamov |
Model | Kamov Ka-226 “Hoodlum” |
Country | Russia |
Manufactured from | 2006 year |
Manufactured to | Add |
Type | Mid Size Helicopters |
Icao | KA26 |
Performance | |
Engine | 2x 2 × Rolls-Royce Allison 250-C20R |
Power, hp | 450 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 220 km/h |
Approach speed | Add |
Travel range | 965 km |
Fuel economy | 1.438 km/l |
Service ceiling | 6,203 m |
Rate of climb | 10.3 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 7,500 kg |
Max landing weight | Add |
Max payload | 1,400 kg |
Fuel tank capacity | 768 l |
Baggage volume | 1 m³ |
Dimensions | |
Seats | 9 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | 1.4 m |
Cabin width | 1.54 m |
Cabin length | 2.35 m |
Exterior length | 8.1 m |
Tail height | 4.15 m |
Fuselage diameter | 1.7 m |
Wing span | 13 m |
Wing tips | No Winglets |