Comparison of Bell 222 and Bristol Sycamore [S]ave
| Attribute |  Bell 222 × |  Bristol Sycamore × |
|---|---|---|
| General | ||
| Manufacturer | Bell Helicopter | Bristol Aeroplane Company |
| Model | Bell 222 | Bristol Sycamore |
| Country | United States | United Kingdom |
| Manufactured from (year) | 1975 | 1947 |
| Manufactured to (year) | 1991 | 1959 |
| Type | Light Helicopters | Military Helicopters |
| Icao | B222 | SYCA |
| Performance | ||
| Engine | 2x Lycoming LTS101-650C-3 | 1x Alvis Leonides 73 |
| Power, hp (hp) | 620 | 550 |
| Max cruise speed (km/h) | 257 | 204 |
| Travel range (km) | 604 | 537 |
| Service ceiling (m) | 6,096 | 4,877 |
| Rate of climb (m/sec) | 8.13 | 5.84 |
| Weights | ||
| Max take off weight (kg) | 3,670 | 2,540 |
| Max landing weight (kg) | 3,670 | - |
| Max payload (kg) | 1,100 | 454 |
| Fuel tank capacity (l) | 893 | 405 |
| Dimensions | ||
| Seats | 9 | 5 |
| Cabin height (m) | 1.46 | - |
| Cabin width (m) | 1.46 | - |
| Cabin length (m) | 2.1 | - |
| Exterior length (m) | 15.1 | 18.62 |
| Tail height (m) | 3.5 | 4.2 |
| Fuselage diameter (m) | 1.6 | - |
| Wing span (m) | 12.1 | 14.8 |
| Wing tips | No Winglets | No Winglets |
Help · Contact us · Disclaimer · Contributors · Developers · Donate