Attribute | Bombardier Q200 × | Fokker 50 × |
---|---|---|
General | ||
Manufacturer | Bombardier Aerospace | Fokker |
Model | Bombardier Q200 | Fokker 50 |
Country | Canada | Netherlands |
Manufactured from (year) | 1995 | 1987 |
Manufactured to (year) | 2009 | 1997 |
Type | Passenger Turbo Props | Passenger Turbo Props |
Icao | DH8B | F50 |
Performance | ||
Engine | 2x 2 X Pratt & Whitney PW123C/D | 2x Pratt & Whitney PW125B turboprops |
Power, hp (hp) | 2,150 | 2,500 |
Avionics | Honeywell SPZ-8000 | EFIS and Automatic Flight Control System |
Max cruise speed (km/h) | 537 | 530 |
Approach speed (km/h) | 137 | 180 |
Travel range (km) | 2,084 | 2,056 |
Fuel economy (km/l) | 0.426 | 0.44 |
Service ceiling (m) | 7,620 | 7,620 |
Rate of climb (m/sec) | 9.14 | 7.62 |
Take off distance (m) | 1,000 | 1,350 |
Landing distance (m) | 780 | 1,130 |
Weights | ||
Max take off weight (kg) | 16,466 | 20,820 |
Max landing weight (kg) | 15,649 | 20,030 |
Max payload (kg) | 4,647 | 5,500 |
Fuel tank capacity (l) | 3,161 | 5,137 |
Baggage volume (m³) | 8.5 | 16.72 |
Dimensions | ||
1↑Seats | 4 | 62 |
Seats - business class | 37 | - |
Cabin height (m) | 1.95 | 1.96 |
Cabin width (m) | 2.52 | 2.5 |
Cabin length (m) | 9.16 | 15.63 |
Exterior length (m) | 22.25 | 25.25 |
Tail height (m) | 7.49 | 8.32 |
Fuselage diameter (m) | 2.69 | 2.7 |
Wing span (m) | 25.89 | 29 |
Wing tips | No Winglets | No Winglets |