Wednesday, December 03, 2008

Il-114

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

Also Known As
Il-114-100 (Version powered by Pratt & Whitney PW-127H engines)

Origin
Russia

Contractor/s
Ilyushin Aviaton Complex

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

Power plant:
PW-127H (2)
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-114 turboprop airplane is intended to cover regional routes of up to 1,000 kilometers carrying up to 64 passengers. This variant features a built-in passenger-boarding ramp as well as buffet table, wardrobe and toilet facility. The Il-114-100 builds on the Il-114 passenger airplane replacing TV7-117 turboprops by the more powerful Pratt & Whitney Canada PW127H engines developing 2,645-hp each. The new power plants allow for greater flight range while improving the landing and take off characteristics. The Il-114-100's propeller diameter is 3.72 meters. The maiden flight was carried out on January 26, 1999, followed by type certification in December 1999.

Specifications
Accommodation: Crew 2, Passengers 64

Dimensions: Fuel Tank Capacity 8,360 l (2,200 gl), Fuselage Diameter 2.9 m, Height 9.3 m, Length 26.9 m, Wing Area 82 square meter, Wingspan 30 m

Weights: Max Weight 23.5 t, Payload 6.5 t

Performance: Ceiling 7,600 m (24,934 ft), Cruise Speed 500 kph (311 mph), Landing Run Distance 900 m (2,953 ft) 550 meters powered by PW127Hs, Max Range 1,000 km (540 nm) carrying max passengers or 1,400 km with max passengers and powered by PW127H engines, Service Life 30 yr, Take Off Run Distance 1,100 m (3,609 ft) 750 meters powered by PW127Hs

Power: Power 5,000 hp Both engines at take off

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

Operators

Russia

Internet Resources
ilyushin.org, 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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