Il-114T  
Initial Operational Capability (IOC): 1998
Maiden Flight: 14 September 1996
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-114-300 and Il-114MP
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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 Il-114T is a cargo aircraft suitable for regional routes based upon the Il-114 passenger airplane. This cargo aircraft can operate from small unpaved runways in a variety of conditions carrying up to 7 tons. A quick-detachable floor-mounted mechanization and wide cargo door (3250x1715mm) was provided for the rapid and effective handling of cargoes carried in standard containers, on trays or in bulk. The Il-114T maiden flight was carried out on September 14, 1996.

Il-114T Specifications

Crew: 2
Number of Engines: 2
Service Life Flight Hours: 30,000
Service Life Flights: 30,000
Area
Wing Area: 82 square meter
Dimensions
Cargo Compartment Height: 1.92 meter
Cargo Compartment Length: 18.9 meter
Cargo Compartment Width: 2.28 meter
Fuselage Diameter: 2.86 meter
Height: 9.32 meter
Length: 26.9 meter
Wingspan: 30 meter
Performance
Ceiling: 7,600 meter
Landing Run Distance: 900 meter
Max Range: 1,000 kilometer (540 nautical mile)
Take Off Run Distance: 1,100 meter
Power
Max Power at TakeOff: 5,000 hp
Speed
Cruise Speed: 500 kph (0.42 mach)
Time
Service Life: 30 year
Volume
Fuel Tank Capacity: 8,360 liter
Payload Capacity: 76 metric ton
Weight
Cargo: 7 ton (15,432 pound)
Max Takeoff Weight: 23.5 ton (51,808 pound)
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
TV7-117Sx2
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