| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Sukhoi |
| Model | Sukhoi Su-80 |
| Country | Russia |
| Manufactured from | 2006 year |
| Manufactured to | Add |
| Type | Passenger Turbo Props |
| Icao | SU80 |
| Performance | |
| Engine | 2x 2 X General Electric GE CT7-9B Turboprop |
| Power, hp | 1,750 hp |
| Power, lbf | Add |
| Avionics | SBKV-P strapdown heading and altitude system, VIM-95C (VOR/ILS/SP/MRK) navigation and landing systems |
| Max cruise speed | 463 km/h |
| Approach speed | Add |
| Travel range | 1,408 km |
| Fuel economy | 0.597 km/l |
| Service ceiling | 7,590 m |
| Rate of climb | Add |
| Take off distance | 840 m |
| Landing distance | 460 m |
| Weights | |
| Max take off weight | 13,500 kg |
| Max landing weight | 13,550 kg |
| Max payload | 2,730 kg |
| Fuel tank capacity | 2,498 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 3 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | 1.82 m |
| Cabin width | 2.17 m |
| Cabin length | 7.75 m |
| Exterior length | 18.26 m |
| Tail height | 5.74 m |
| Fuselage diameter | 2.4 m |
| Wing span | 23.18 m |
| Wing tips | Blended Tips |