Attribute | Vickers VC.1 Viking × | Bombardier Q100 (Dash 8-100) × |
---|---|---|
General | ||
Manufacturer | Vickers-Armstrongs | Bombardier Aerospace |
Model | Vickers VC.1 Viking | Bombardier Q100 (Dash 8-100) |
Country | United Kingdom | Canada |
Manufactured from (year) | 1945 | 1983 |
Manufactured to (year) | 1954 | - |
Type | Passenger Turbo Props | Light Passenger Jets |
Icao | VC1 | Q100 |
Performance | ||
1↑Engine | 2x Bristol Hercules 634 | Pratt & Whitney Canada PW120 |
Power, hp (hp) | 1,690 | 2,000 |
Avionics | - | UNS-1Ew FMS, EFI-890R |
Max cruise speed (km/h) | 424 | 535 |
Approach speed (km/h) | - | 250 |
Travel range (km) | 2,778 | 2,084 |
Service ceiling (m) | 7,620 | 7,620 |
Rate of climb (m/sec) | 7.62 | 7.49 |
Take off distance (m) | 780 | 1,000 |
Landing distance (m) | 1,200 | 780 |
Weights | ||
Max take off weight (kg) | 15,422 | 15,650 |
Max payload (kg) | 2,500 | 4,536 |
Fuel tank capacity (l) | 3,369 | 3,161 |
Baggage volume (m³) | - | 8.5 |
Dimensions | ||
Seats | 26 | 4 |
Cabin height (m) | - | 1.95 |
Cabin width (m) | - | 2.5 |
Cabin length (m) | - | 9.16 |
Exterior length (m) | 19.86 | 22.25 |
Tail height (m) | 5.97 | 7.5 |
Fuselage diameter (m) | 2.6 | 2.69 |
Wing span (m) | 27.2 | 25.9 |
Wing tips | No Winglets | No Winglets |