Friday, March 19, 2010

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Il-96


Maiden Flight: Wednesday, September 28, 1988
IOC: July 1993
Total Production: 83

Il-96-400


IOC: 2007


Origin
Russia


Contractor/s
Ilyushin Aviaton Complex
VASO

Family Members
Il-96-300
Il-96-400T
Il-96M
Il-96T

Power plant:
PS-90A (4)

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.

Specifications
Accommodation: Crew 3, Passengers 436 in three-class layout; 386 in two-class layout; 315 in three-class cabin layout

Dimensions: Fuel Tank Capacity 152,620 l (40,163 gl), Fuselage Diameter 6 m, Height 15.7 m, Length 63.9 m, Wing Area 350 square meter, Wingspan 60.1 m

Weights: Max Takeoff Weight 265 t, Payload 58 t

Engine/s Performance: Thrust 141,000 lb (63,958 kg)

Performance: Ceiling 12,000 m (39,370 ft), Cruise Speed 870 kph (541 mph), Landing Run Distance 1,650 m (5,413 ft), Max Range 10,000 km (5,400 nm) with max passenger, Service Life 20 yr, Take Off Run Distance 2,700 m (8,858 ft)

Other: Number of Engines 4, Service Life (Flight Hours) 60,000, Service Life (Flights) 20,000

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: Sunday, March 07, 2010

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