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 |