Attribute | Sukhoi Su-80 × | Yakovlev Yak-40 × |
---|---|---|
General | ||
Manufacturer | Sukhoi | Yakovlev |
Model | Sukhoi Su-80 | Yakovlev Yak-40 |
Country | Russia | Russia |
Manufactured from (year) | 2006 | 1967 |
Manufactured to (year) | - | 1981 |
1↓Type | Passenger Turbo Props | Light Passenger Jets |
Icao | SU80 | YK40 |
Performance | ||
Engine | 2x 2 X General Electric GE CT7-9B Turboprop | 3x Ivchenko AI-25 |
Power, hp (hp) | 1,750 | 3,300 |
Avionics | SBKV-P strapdown heading and altitude system, VIM-95C (VOR/ILS/SP/MRK) navigation and landing systems | - |
Max cruise speed (km/h) | 463 | 556 |
Approach speed (km/h) | - | 222 |
Travel range (km) | 1,408 | 1,796 |
Fuel economy (km/l) | 0.597 | - |
Service ceiling (m) | 7,590 | 7,925 |
Rate of climb (m/sec) | - | 8 |
Take off distance (m) | 840 | 1,000 |
Landing distance (m) | 460 | 640 |
Weights | ||
Max take off weight (kg) | 13,500 | 16,000 |
Max landing weight (kg) | 13,550 | 15,500 |
Max payload (kg) | 2,730 | 2,700 |
Fuel tank capacity (l) | 2,498 | 3,899 |
Dimensions | ||
Seats | 3 | 32 |
Cabin height (m) | 1.82 | 1.85 |
Cabin width (m) | 2.17 | 2.15 |
Cabin length (m) | 7.75 | 7.7 |
Exterior length (m) | 18.26 | 20.36 |
Tail height (m) | 5.74 | 6.5 |
Fuselage diameter (m) | 2.4 | 2.25 |
Wing span (m) | 23.18 | 25 |
Wing tips | Blended Tips | No Winglets |