| Manufacturer |
Ilyushin |
| Description |
The Ilyushin Il-114 (Russian Илью́шин Ил-114) is a twin-engine turboprop, short-haul regional airliner developed by the Ilyushin design bureau. |
| ICAO Code |
I114 |
| First Flight |
1990-03-29 |
| Entry Into service |
1998-08-27 |
| Designer |
Ilyushin |
| Type |
Turboprop Regional airliner |
| Length (m) |
26.88 |
| Height (m) |
9.19 |
| Max Seating |
64 |
| Max Speed (km/h) |
500 |
| Cruise Speed (km/h) |
470 |
| Max Ceiling (m) |
8000 |
| Capacity Description |
64 |
| National Origin |
Soviet Union |
| Number Built |
22 |
| Powerplant Description |
TV7-117S |
| Primary Users |
Uzbekistan Airways (former), Vyborg Airlines (former) |
| Status |
Retired; to be reintroduced in Russia |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Ilyushin_Il-114 |
| Flat Wing Span (m) |
30 |
| Flat Wing Area (m²) |
81.9 |
| Wake Category |
M |
| Aircraft Engine |
TV7-117 |
| Number of Engines |
2 |