Comparison of Bell Agusta BA609 and Kamov Ka-226 “Hoodlum” [S]ave
| Attribute |  Bell Agusta BA609 × |  Kamov Ka-226 “Hoodlum” × |
|---|---|---|
| General | ||
| Manufacturer | Bell Helicopter | Kamov |
| Model | Bell Agusta BA609 | Kamov Ka-226 “Hoodlum” |
| Country | United States | Russia |
| Manufactured from (year) | 2011 | 2006 |
| Type | Tilt Rotors | Mid Size Helicopters |
| Icao | B609 | KA26 |
| Performance | ||
| Engine | 2x Pratt & Whitney PT6C-67A | 2x 2 × Rolls-Royce Allison 250-C20R |
| Power, hp (hp) | 1,940 | 450 |
| Avionics | Rockwell Collins Pro-line 21 | - |
| Max cruise speed (km/h) | 509 | 220 |
| Travel range (km) | 1,852 | 965 |
| Fuel economy (km/l) | 0.978 | 1.438 |
| Service ceiling (m) | 7,620 | 6,203 |
| Rate of climb (m/sec) | 7.62 | 10.3 |
| Weights | ||
| Max take off weight (kg) | 7,620 | 7,500 |
| Max payload (kg) | 2,500 | 1,400 |
| Fuel tank capacity (l) | 1,401 | 768 |
| Baggage volume (m³) | 1.4 | 1 |
| Dimensions | ||
| Seats | 9 | 9 |
| Seats - business class | 6 | - |
| Cabin height (m) | 1.42 | 1.4 |
| Cabin width (m) | 1.52 | 1.54 |
| Cabin length (m) | 5.33 | 2.35 |
| Exterior length (m) | 13.3 | 8.1 |
| Tail height (m) | 4.5 | 4.15 |
| Fuselage diameter (m) | 1.6 | 1.7 |
| Wing span (m) | 18.3 | 13 |
| Wing tips | No Winglets | No Winglets |
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