Attribute | Value |
---|---|
General | |
Manufacturer | Bell Helicopter |
Model | Bell Agusta BA609 |
Country | United States |
Manufactured from | 2011 year |
Manufactured to | Add |
Type | Tilt Rotors |
Icao | B609 |
Performance | |
Engine | 2x Pratt & Whitney PT6C-67A |
Power, hp | 1,940 hp |
Power, lbf | Add |
Avionics | Rockwell Collins Pro-line 21 |
Max cruise speed | 509 km/h |
Approach speed | Add |
Travel range | 1,852 km |
Fuel economy | 0.978 km/l |
Service ceiling | 7,620 m |
Rate of climb | 7.62 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 7,620 kg |
Max landing weight | Add |
Max payload | 2,500 kg |
Fuel tank capacity | 1,401 l |
Baggage volume | 1.4 m³ |
Dimensions | |
Seats | 9 |
Seats - business class | 6 |
Seats - first class | Add |
Cabin height | 1.42 m |
Cabin width | 1.52 m |
Cabin length | 5.33 m |
Exterior length | 13.3 m |
Tail height | 4.5 m |
Fuselage diameter | 1.6 m |
Wing span | 18.3 m |
Wing tips | No Winglets |