| Manufacturer |
Ilyushin |
Antonov |
| Description |
The Ilyushin Il-114 (Russian Илью́шин Ил-114) is a twin-engine turboprop, short-haul regional airliner developed by the Ilyushin design bureau. |
AI-24VT |
| ICAO Code |
I114 |
AN26 |
| EASA TCDSN |
|
EASA.IM.A.351 |
| First Flight |
1990-03-29 |
1969-05-21 |
| Entry Into service |
1998-08-27 |
1972-01-01 |
| Designer |
Ilyushin |
|
| Type |
Turboprop Regional airliner |
Transport aircraft / regional airliner |
| Length (m) |
26.88 |
23.8 |
| Height (m) |
9.19 |
8.58 |
| Max Seating |
64 |
40 |
| Max Speed (km/h) |
500 |
|
| Cruise Speed (km/h) |
470 |
440 |
| Max Ceiling (m) |
8000 |
7500 |
| Rate of Climb (m/s) |
|
8 |
| Capacity Description |
64 |
40 passengers / 5500 kg |
| National Origin |
Soviet Union |
Soviet Union |
| Number Built |
22 |
1403 |
| Powerplant Description |
TV7-117S |
2 × Progress AI-24VT Turboprop engines, 2103 kW (2820 hp) each |
| Primary Users |
Uzbekistan Airways (former), Vyborg Airlines (former) |
Soviet Air Forces (former), Russian Aerospace Forces , Ukrainian Air Force , People's Liberation Army Air Force |
| Status |
Retired; to be reintroduced in Russia |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Ilyushin_Il-114 |
en.wikipedia.org/wiki/Antonov_An-26 |
| Flat Wing Span (m) |
30 |
29.3 |
| Flat Wing Area (m²) |
81.9 |
74.98 |
| Flat Wing Aspect Ratio |
|
11.7 |
| Wake Category |
M |
M |
| Aircraft Engine |
TV7-117 |
|
| Number of Engines |
2 |
2 |