Il-114-300  
Initial Operational Capability (IOC): 2018
Total Production: ?
Origin: Russia
Corporations: Ilyushin Aviaton Complex
Parent System: Il-114
Initial Operational Capability (IOC): April 1997
Maiden Flight: 29 March 1990
Total Production: 20
Family Members: Il-114, Il-114MP and Il-114T
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Description: The Ilyushin IL-114 is a twin-engine turboprop aircraft suitable for commercial and military applications such as regional airliner and patrol aircraft respectively. Ilyushin Aviation Complex carried out the maiden flight on March 29, 1990. The Il-114 is suitable for regional routes operating from small unpaved runways and flying at day/night in all-weather conditions. An auxiliary power system allows for autonomous operation at ill-equipped airports. Flight data was unified into a central multifunctional display system based on color LCDs. The Russian aviation authorities certified the aircraft type in April 1997. Two Klimov TV7-117S engines rated at 2,500-hp each provide power to six-bladed propellers with a 3.6-m diameter.

The Ilyushin Il-114-300 turboprop airplane is intended to cover regional routes of up to 2,100 kilometers carrying up to 52 passengers. This version features two TV7-117SM turboprops each rated at 2,650-hp and designed with increased fuel efficiency compared with other TV7-117 engines. The new power plants allow for greater flight range while improving the landing and take off characteristics. Besides, a built-in air-stairs and an auxiliary power unit enable Il-114-300 operations in poorly-equipped airfields.

Il-114-300 Specifications

Crew: 2
Number of Engines: 2
Passengers: 52
Propeller Blades: 6
Service Life Flight Hours: 30,000
Service Life Flights: 30,000
Area
Wing Area: 82 square meter
Dimensions
Fuselage Diameter: 2.86 meter
Height: 9.32 meter
Length: 26.9 meter
Wingspan: 30 meter
Performance
Landing Run Distance: 610 meter
Max Range: 2,100 kilometer (1,134 nautical mile)
Operational Altitude: 7,600 meter (24,934 foot)
Take Off Run Distance: 1,160 meter
Power
Max Power at TakeOff: 5,300 hp
Speed
Cruise Speed: 500 kph (0.42 mach)
Time
Service Life: 30 year
Volume
Fuel Tank Capacity: 8,360 liter
Weight
Max Takeoff Weight: 23.5 ton (51,808 pound)
Payload: 6.50 ton
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
TV7-117SMx2
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