Il-96-400  
Initial Operational Capability (IOC): 2007
Total Production: ?
Origin: Russia
Corporations: Ilyushin Aviaton Complex and VASO
Parent System: Il-96
Initial Operational Capability (IOC): July 1993
Maiden Flight: 28 September 1988
Total Production: 83
Family Members: Il-96-300, Il-96-400M, Il-96-400T, Il-96-400TZ, Il-96M and Il-96T
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Description: The Ilyushin Il-96 is a four-engine, wide-body, longer range passenger and freighter aircraft based upon the Il-86 airliner. The Il-96 aircraft features a fuselage shortened approx. 4 meters, a new wing layout, a seating capacity between 235 and 436 passengers, and fly-by-wire controls. The Il-96 wide-body aircraft family includes the Il-96-300 and Il-96-400 airliners and the Il-96T and Il-96-400T freighters. The Il-96 powered by western engines and the Il-98 twin-engine airliners were cancelled. The Il-96 maiden flight was carried out on September 28, 1988. In July 1993 the first Il-96-300 airliner entered into service.

The Il-96-400 is a stretched version of the Il-96-300 airliner and features improved aerodynamics, fuel efficient PS-90A turbojet engines, increased payload capacity, improved frame design, and updated onboard avionics. The Il-96-400 is less expensive than its western counterparts such as the Boeing 777 and Airbus A340 aircraft. In a single-class cabin layout the Il-96-400 airliner is capable of accommodating up to 436 passengers over ranges of up to 10,000 km. In August 2006, two Il-96-400 airliners were under construction at Voronezh aircraft plant. The four PS-90A engines are rated at 16,000 kg/35,000-lb of thrust each.

Il-96-400 Applications


Support Aircraft Il-80M

Il-96-400 Specifications

Crew: 3
Number of Engines: 4
Passengers: 436
Service Life Flight Hours: 60,000
Service Life Flights: 20,000
Area
Wing Area: 350 square meter
Dimensions
Fuselage Diameter: 6.08 meter
Height: 15.7 meter
Length: 64 meter
Wingspan: 60 meter
Performance
Ceiling: 12,000 meter
Landing Run Distance: 1,650 meter
Max Range: 10,000 kilometer (5,400 nautical mile)
Take Off Run Distance: 2,700 meter
Speed
Cruise Speed: 870 kph (0.73 mach)
Time
Service Life: 20 year
Volume
Fuel Tank Capacity: 152,620 liter
Weight
Max Takeoff Weight: 265 ton (584,215 pound)
Payload: 58 ton
Thrust: 141,000 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)

Il-96-400 News

There is 1 news
on 28 Jul 2016
Thursday, July 28, 2016Russian Ministry of Defense Takes Delivery of Il-96-400 Airborne Command System

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
PS-90Ax4
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