Comparison of North American B-25 Mitchell and Vickers VC.1 Viking [S]ave
| Attribute |  North American B-25 Mitchell × |  Vickers VC.1 Viking × |
|---|---|---|
| General | ||
| Manufacturer | North American Aviation NAA | Vickers-Armstrongs |
| Model | North American B-25 Mitchell | Vickers VC.1 Viking |
| Country | United States | United Kingdom |
| Manufactured from (year) | 1940 | 1945 |
| Manufactured to (year) | 1945 | 1954 |
| Type | Military Propellor Planes | Passenger Turbo Props |
| Icao | B25 | VC1 |
| Performance | ||
| Engine | 2x Wright R-2600-92 Twin Cyclone | 2x Bristol Hercules 634 |
| Power, hp (hp) | 1,700 | 1,690 |
| Max cruise speed (km/h) | 437 | 424 |
| Approach speed (km/h) | 148 | - |
| Travel range (km) | 2,167 | 2,778 |
| Service ceiling (m) | 7,376 | 7,620 |
| Rate of climb (m/sec) | 5.08 | 7.62 |
| Take off distance (m) | - | 780 |
| Landing distance (m) | - | 1,200 |
| Weights | ||
| Max take off weight (kg) | 15,876 | 15,422 |
| Max payload (kg) | 3,060 | 2,500 |
| Fuel tank capacity (l) | 3,687 | 3,369 |
| Dimensions | ||
| Seats | 5 | 26 |
| 1↑Exterior length (m) | 16.13 | 19.86 |
| Tail height (m) | 4.98 | 5.97 |
| Fuselage diameter (m) | 1.4 | 2.6 |
| Wing span (m) | 20.6 | 27.2 |
| Wing tips | No Winglets | No Winglets |
Help · Contact us · Disclaimer · Contributors · Developers · Donate