Comparison of Bell 210 and Bell 222 [S]ave
| Attribute |  Bell 210 × |  Bell 222 × |
|---|---|---|
| General | ||
| Manufacturer | Bell Helicopter | Bell Helicopter |
| Model | Bell 210 | Bell 222 |
| Country | United States | United States |
| Manufactured from (year) | 1959 | 1975 |
| Manufactured to (year) | 1980 | 1991 |
| Type | Mid Size Helicopters | Light Helicopters |
| Icao | B210 | B222 |
| Performance | ||
| Engine | 1x 1 × Lycoming T53-L-11A turboshaft | 2x Lycoming LTS101-650C-3 |
| Power, hp (hp) | 1,100 | 620 |
| Max cruise speed (km/h) | 206 | 257 |
| Travel range (km) | 417 | 604 |
| Fuel economy (km/l) | 0.523 | - |
| Service ceiling (m) | 5,910 | 6,096 |
| Rate of climb (m/sec) | 8.92 | 8.13 |
| Weights | ||
| Max take off weight (kg) | 4,309 | 3,670 |
| Max landing weight (kg) | - | 3,670 |
| Max payload (kg) | 1,135 | 1,100 |
| Fuel tank capacity (l) | 795 | 893 |
| Baggage volume (m³) | 2.1 | - |
| Dimensions | ||
| Seats | 15 | 9 |
| Cabin height (m) | 1.25 | 1.46 |
| Cabin width (m) | 2.44 | 1.46 |
| Cabin length (m) | 3.45 | 2.1 |
| Exterior length (m) | 12.7 | 15.1 |
| Tail height (m) | 4.5 | 3.5 |
| Fuselage diameter (m) | 2.6 | 1.6 |
| Wing span (m) | 14.63 | 12.1 |
| Wing tips | No Winglets | No Winglets |
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