Comparison of Bell 222 and Hughes OH-6 Cayuse [S]ave
| Attribute |  Bell 222 × |  Hughes OH-6 Cayuse × |
|---|---|---|
| General | ||
| Manufacturer | Bell Helicopter | McDonnell Douglas |
| Model | Bell 222 | Hughes OH-6 Cayuse |
| Country | United States | United States |
| Manufactured from (year) | 1975 | 1965 |
| Manufactured to (year) | 1991 | - |
| Type | Light Helicopters | Military Helicopters |
| Icao | B222 | OH6A |
| Performance | ||
| Engine | 2x Lycoming LTS101-650C-3 | 1x Allison T63-A-5A |
| Power, hp (hp) | 620 | 317 |
| Max cruise speed (km/h) | 257 | 241 |
| Travel range (km) | 604 | 611 |
| Service ceiling (m) | 6,096 | 4,816 |
| Rate of climb (m/sec) | 8.13 | 10.5 |
| Weights | ||
| Max take off weight (kg) | 3,670 | 1,610 |
| Max landing weight (kg) | 3,670 | 1,440 |
| Max payload (kg) | 1,100 | 713 |
| Fuel tank capacity (l) | 893 | 233 |
| Dimensions | ||
| Seats | 9 | 2 |
| Cabin height (m) | 1.46 | 1.5 |
| Cabin width (m) | 1.46 | 1.3 |
| Cabin length (m) | 2.1 | 2.4 |
| Exterior length (m) | 15.1 | 9.4 |
| Tail height (m) | 3.5 | - |
| Fuselage diameter (m) | 1.6 | 1.45 |
| Wing span (m) | 12.1 | 8.03 |
| Wing tips | No Winglets | No Winglets |
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