Attribute | Fokker 50 × | Bombardier Q300 × |
---|---|---|
General | ||
Manufacturer | Fokker | Bombardier Aerospace |
Model | Fokker 50 | Bombardier Q300 |
Country | Netherlands | Canada |
Manufactured from (year) | 1987 | 1998 |
Manufactured to (year) | 1997 | 2009 |
Type | Passenger Turbo Props | Passenger Turbo Props |
Icao | F50 | DH8C |
Performance | ||
Engine | 2x Pratt & Whitney PW125B turboprops | 2x 2 X Pratt & Whitney Canada PW123B |
Power, hp (hp) | 2,500 | 2,500 |
Avionics | EFIS and Automatic Flight Control System | Honeywell Avionics Suite |
Max cruise speed (km/h) | 530 | 532 |
Approach speed (km/h) | 180 | 204 |
Travel range (km) | 2,056 | 1,711 |
Fuel economy (km/l) | 0.44 | 0.499 |
Service ceiling (m) | 7,620 | 7,620 |
Rate of climb (m/sec) | 7.62 | 9.14 |
Take off distance (m) | 1,350 | 1,180 |
Landing distance (m) | 1,130 | 1,040 |
Weights | ||
Max take off weight (kg) | 20,820 | 19,505 |
Max landing weight (kg) | 20,030 | 19,050 |
Max payload (kg) | 5,500 | 6,124 |
Fuel tank capacity (l) | 5,137 | 3,161 |
Baggage volume (m³) | 16.72 | 9.1 |
Dimensions | ||
Seats | 62 | 56 |
Seats - business class | - | 5 |
Cabin height (m) | 1.96 | 1.95 |
Cabin width (m) | 2.5 | 2.51 |
Cabin length (m) | 15.63 | 12.6 |
Exterior length (m) | 25.25 | 25.7 |
Tail height (m) | 8.32 | 7.49 |
Fuselage diameter (m) | 2.7 | 2.69 |
Wing span (m) | 29 | 27.4 |
Wing tips | No Winglets | No Winglets |