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