Attribute | Short 360 × | Fokker 50 × |
---|---|---|
General | ||
Manufacturer | Short Brothers | Fokker |
Model | Short 360 | Fokker 50 |
Country | United Kingdom | Netherlands |
Manufactured from (year) | 1980 | 1987 |
Manufactured to (year) | 1991 | 1997 |
Type | Passenger Turbo Props | Passenger Turbo Props |
Icao | SH36 | F50 |
Performance | ||
Engine | 2x Pratt & Whitney Canada PT6A-65AR | 2x Pratt & Whitney PW125B turboprops |
Power, hp (hp) | 1,424 | 2,500 |
Avionics | - | EFIS and Automatic Flight Control System |
Max cruise speed (km/h) | 404 | 530 |
Approach speed (km/h) | 185 | 180 |
Travel range (km) | 1,056 | 2,056 |
Fuel economy (km/l) | - | 0.44 |
Service ceiling (m) | 6,096 | 7,620 |
Rate of climb (m/sec) | 4.84 | 7.62 |
Take off distance (m) | 1,300 | 1,350 |
Landing distance (m) | 1,100 | 1,130 |
Weights | ||
Max take off weight (kg) | 12,300 | 20,820 |
Max landing weight (kg) | 12,020 | 20,030 |
Max payload (kg) | 3,500 | 5,500 |
Fuel tank capacity (l) | 2,180 | 5,137 |
1↑Baggage volume (m³) | - | 16.72 |
Dimensions | ||
Seats | 39 | 62 |
Cabin height (m) | 1.88 | 1.96 |
Cabin width (m) | 1.85 | 2.5 |
Cabin length (m) | 8.4 | 15.63 |
Exterior length (m) | 21.6 | 25.25 |
Tail height (m) | 7.27 | 8.32 |
Fuselage diameter (m) | 2.2 | 2.7 |
Wing span (m) | 22.8 | 29 |
Wing tips | No Winglets | No Winglets |