Il-96T  
Initial Operational Capability (IOC): 1998
Maiden Flight: 16 May 1997
Total Production: ?
Origin: Russia
Corporations: Ilyushin Aviaton Complex
Parent System: Il-96
Initial Operational Capability (IOC): July 1993
Maiden Flight: 28 September 1988
Total Production: 83
Family Members: Il-96-300, Il-96-400, Il-96-400M, Il-96-400T, Il-96-400TZ and Il-96M
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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-96T is a long-range, wide-body freighter derived from Il-96-300 airliner and featuring a stretched fuselage equipped with Pratt & Whitney engines and Rockwell Collins avionics. The aircraft maximum payload capacity is 92 tons distributed inside 32 international containers, but typically carries a 58-ton payload on routes of up to 9,700 kilometers. The Il-96T freighter is powered by four US-built PW2037 engines rated at 37,000 pounds of thrust. These engines are far more reliable and fuel efficient than Russian-built PS90A turbofans. The maiden flight was carried out on May 16, 2007. Russian type certification was awarded in March 1998 and FAA type certification in June 1999.

Il-96T Specifications

Crew: 2
Number of Engines: 4
Service Life Flight Hours: 60,000
Service Life Flights: 20,000
Area
Wing Area: 350 square meter
Dimensions
Cargo Compartment Length: 45 meter
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: 9,700 kilometer (5,238 nautical mile)
Take Off Run Distance: 2,500 meter
Speed
Cruise Speed: 870 kph (0.73 mach)
Top Speed at High Altitude: 273 mps (983 kph)
Time
Service Life: 20 year
Volume
Fuel Tank Capacity: 152,620 liter
Payload Capacity: 776 metric ton
Weight
Cargo: 92 ton (202,822 pound)
Empty Weight: 132 ton
Max Takeoff Thrust: 148,000 pound
Max Takeoff Weight: 270 ton (595,238 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)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
PW2037x4
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