Attribute | Fokker 50 × | ATR 42-500 × |
---|---|---|
General | ||
Manufacturer | Fokker | ATR Aircraft |
Model | Fokker 50 | ATR 42-500 |
Country | Netherlands | France |
Manufactured from (year) | 1987 | 1994 |
Manufactured to (year) | 1997 | - |
Type | Passenger Turbo Props | Passenger Turbo Props |
Icao | F50 | AT45 |
Performance | ||
Engine | 2x Pratt & Whitney PW125B turboprops | 2x 2 X Pratt & Whitney PW127E |
Power, hp (hp) | 2,500 | 2,400 |
Avionics | EFIS and Automatic Flight Control System | Dual Honeywell HT1000 FMS |
Max cruise speed (km/h) | 530 | 556 |
Approach speed (km/h) | 180 | 193 |
Travel range (km) | 2,056 | 1,326 |
Fuel economy (km/l) | 0.44 | 1.243 |
Service ceiling (m) | 7,620 | 7,620 |
Rate of climb (m/sec) | 7.62 | 9.4 |
Take off distance (m) | 1,350 | 1,165 |
Landing distance (m) | 1,130 | 964 |
Weights | ||
Max take off weight (kg) | 20,820 | 18,600 |
Max landing weight (kg) | 20,030 | 18,300 |
Max payload (kg) | 5,500 | 5,450 |
Fuel tank capacity (l) | 5,137 | 5,602 |
Baggage volume (m³) | 16.72 | 10.8 |
Dimensions | ||
Seats | 62 | 48 |
Cabin height (m) | 1.96 | 1.9 |
Cabin width (m) | 2.5 | 2.57 |
Cabin length (m) | 15.63 | 9.5 |
Exterior length (m) | 25.25 | 22.67 |
Tail height (m) | 8.32 | 7.59 |
Fuselage diameter (m) | 2.7 | 2.7 |
Wing span (m) | 29 | 24.57 |
Wing tips | No Winglets | No Winglets |