Attribute | ![]() Bell Agusta BA609 × | ![]() Bell 412 × |
---|---|---|
General | ||
Manufacturer | Bell Helicopter | Bell Helicopter |
Model | Bell Agusta BA609 | Bell 412 |
Country | United States | United States |
Manufactured from (year) | 2011 | 1981 |
Type | Tilt Rotors | Large Helicopters |
Icao | B609 | B412 |
Performance | ||
Engine | 2x Pratt & Whitney PT6C-67A | 1x 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac |
Power, hp (hp) | 1,940 | 1,250 |
Avionics | Rockwell Collins Pro-line 21 | Garmin GTN-750 NAV/COM/WAAS GPS, Helicopter Terrain Avoidance Warning System (H-TAWS) Capability |
Max cruise speed (km/h) | 509 | 230 |
Travel range (km) | 1,852 | 659 |
Fuel economy (km/l) | 0.978 | 0.612 |
Service ceiling (m) | 7,620 | 6,096 |
Rate of climb (m/sec) | 7.62 | 6.86 |
Weights | ||
Max take off weight (kg) | 7,620 | 5,398 |
Max payload (kg) | 2,500 | 2,190 |
Fuel tank capacity (l) | 1,401 | 1,253 |
Baggage volume (m³) | 1.4 | 0.8 |
Dimensions | ||
Seats | 9 | 15 |
Seats - business class | 6 | - |
Cabin height (m) | 1.42 | 1.24 |
Cabin width (m) | 1.52 | 2.43 |
Cabin length (m) | 5.33 | 2.34 |
Exterior length (m) | 13.3 | 17.02 |
Tail height (m) | 4.5 | 4.54 |
Fuselage diameter (m) | 1.6 | 2.6 |
Wing span (m) | 18.3 | 14.02 |
Wing tips | No Winglets | No Winglets |