Attribute | de Havilland DHC-8-200 × | Sukhoi Su-80 × |
---|---|---|
General | ||
Manufacturer | de Havilland | Sukhoi |
Model | de Havilland DHC-8-200 | Sukhoi Su-80 |
Country | United Kingdom | Russia |
Manufactured from (year) | 1983 | 2006 |
Type | Passenger Turbo Props | Passenger Turbo Props |
Icao | DH8B | SU80 |
Performance | ||
Engine | 2x Pratt & Whitney Canada PW123 | 2x 2 X General Electric GE CT7-9B Turboprop |
Power, hp (hp) | 2,150 | 1,750 |
Avionics | Honeywell SPZ-8000 dual-channel digital AFCS, Primus P660 weather radar, Collins nav/comm systems | SBKV-P strapdown heading and altitude system, VIM-95C (VOR/ILS/SP/MRK) navigation and landing systems |
Max cruise speed (km/h) | 537 | 463 |
Travel range (km) | 2,084 | 1,408 |
Fuel economy (km/l) | - | 0.597 |
Service ceiling (m) | 7,620 | 7,590 |
Rate of climb (m/sec) | 7.49 | - |
Take off distance (m) | 1,000 | 840 |
Landing distance (m) | 780 | 460 |
Weights | ||
Max take off weight (kg) | 16,466 | 13,500 |
Max landing weight (kg) | 15,649 | 13,550 |
Max payload (kg) | 4,647 | 2,730 |
Fuel tank capacity (l) | 3,161 | 2,498 |
Baggage volume (m³) | 8.5 | - |
Dimensions | ||
Seats | 4 | 3 |
Cabin height (m) | 1.95 | 1.82 |
Cabin width (m) | 2.5 | 2.17 |
Cabin length (m) | 9.16 | 7.75 |
Exterior length (m) | 22.25 | 18.26 |
Tail height (m) | 7.5 | 5.74 |
Fuselage diameter (m) | 2.69 | 2.4 |
Wing span (m) | 25.9 | 23.18 |
Wing tips | No Winglets | Blended Tips |