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