Attribute | Antonov An-140 × | de Havilland DHC-8-200 × |
---|---|---|
General | ||
Manufacturer | Antonov | de Havilland |
Model | Antonov An-140 | de Havilland DHC-8-200 |
Country | Ukraine | United Kingdom |
Manufactured from (year) | 1997 | 1983 |
Type | Passenger Turbo Props | Passenger Turbo Props |
Icao | A140 | DH8B |
Performance | ||
Engine | 2x 2 × Pratt & Whitney PW127A or Klimov TV3-117WMA-SBM1 | 2x Pratt & Whitney Canada PW123 |
Power, hp (hp) | 2,465 | 2,150 |
Avionics | Buran weather radar | Honeywell SPZ-8000 dual-channel digital AFCS, Primus P660 weather radar, Collins nav/comm systems |
Max cruise speed (km/h) | 574 | 537 |
Travel range (km) | 3,704 | 2,084 |
Fuel economy (km/l) | 1.208 | - |
Service ceiling (m) | 7,590 | 7,620 |
Rate of climb (m/sec) | 6.83 | 7.49 |
Take off distance (m) | 1,750 | 1,000 |
Landing distance (m) | 1,360 | 780 |
Weights | ||
Max take off weight (kg) | 21,500 | 16,466 |
Max landing weight (kg) | 21,000 | 15,649 |
Max payload (kg) | 6,000 | 4,647 |
Fuel tank capacity (l) | 5,413 | 3,161 |
Baggage volume (m³) | 0.2 | 8.5 |
Dimensions | ||
Seats | 52 | 4 |
Cabin height (m) | - | 1.95 |
Cabin width (m) | 2.6 | 2.5 |
Cabin length (m) | - | 9.16 |
Exterior length (m) | 22.6 | 22.25 |
Tail height (m) | 8.2 | 7.5 |
Fuselage diameter (m) | 2.8 | 2.69 |
Wing span (m) | 24.5 | 25.9 |
Wing tips | No Winglets | No Winglets |