Il-96
Maiden Flight: Wednesday, September 28, 1988
IOC: July 1993
Total Production: 80
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)
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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.
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
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