Iljuschin / Ilyushin Il-114
Regional Airliner
The Ilyushin Il-114 is a twin-engined regional airliner for max. 64 passengers developed by the Russian manufacturer JSC Ilyushin Aviation Complex.
| Propulsion | 2 Turboprop Engines |
| Engine Model | Klimov TW7-117S / TV7-117S |
| Engine Power (each) | 1840 kW | 2468 shp |
| Speed | 500 km/h | 270 kts 311 mph |
| Service Ceiling | 7.620 m | 25.000 ft |
| Range | 1.000 km | 540 NM 621 mi. |
| Empty Weight | 13.700 kg | 30.203 lbs |
| max. Takeoff Weight | 23.500 kg | 51.809 lbs |
| Wing Span | 30,00 m | 98 ft 5 in |
| Wing Area | 81,9 m² | 882 ft² |
| Length | 26,30 m | 86 ft 3 in |
| Height | 9,32 m | 30 ft 7 in |
| First Flight | 29.03.1990 |
| Production Status | in production |
| ICAO Code | I114 |
| IATA Code | I14 |
| Data for (Version) | Iljuschin / Ilyushin Il-114 |