Wednesday, December 03, 2008

Il-114

Maiden Flight: Thursday, March 29, 1990
IOC: April 1997

Il-114T

Maiden Flight: Saturday, September 14, 1996

Origin
Russia

Contractor/s
Ilyushin Aviaton Complex

Family Members
Il-114
Il-114-300
Il-114MP

Power plant:
TV7-117S (2)

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 (3250?1715mm) 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.

Specifications
Accommodation: Crew 2

Dimensions: Cargo Compartment Height 1.9 m, Cargo Compartment Length 18.9 m, Cargo Compartment Width 2.3 m, Fuel Tank Capacity 8,360 l (2,200 gl), Fuselage Diameter 2.9 m, Height 9.3 m, Length 26.9 m, Payload Capacity 76 metric ton, Wing Area 82 square meter, Wingspan 30 m

Weights: Max Weight 23.5 t, Payload 7 t

Performance: Ceiling 7,600 m (24,934 ft), Cruise Speed 500 kph (311 mph), Landing Run Distance 900 m (2,953 ft), Max Range 1,000 km (540 nm) carrying a 6.5t payload, Service Life 30 yr, Take Off Run Distance 1,100 m (3,609 ft)

Power: Power 5,000 hp

Other: Number of Engines 2, Service Life (Flight Hours) 30,000, Service Life (Flights) 30,000

Operators

Russia

Internet Resources
ilyushin.org

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)

Last Updated: Saturday, November 22, 2008

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