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