There are 11 images added between 20 April 2009 and 13 October 2016
1  2  
Il-96-300  
Initial Operational Capability (IOC): 1998
Maiden Flight: 12 October 1996
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-96-400, Il-96-400M, Il-96-400T, Il-96-400TZ, Il-96M and Il-96T
Reviews
There are no reviews so far

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-96-300 airliner entered service in July 1993 powered by four Soviet/Russian PS90A engines each developing 16,000 kg of thrust. It has been reported that less than 20 of such aircraft were delivered to Aeroflot. The Il-96-300's low efficient engines and its poor performance Russian avionics seem to be the main reason for the aircraft's cancellation favoring new models equipped with western avionics and engines. According to Russian press the Il-96-300 production terminated in the 2006/2007 timeframe.

Il-96-300 Applications


Support Aircraft Il-80

Il-96-300 Specifications

Crew: 3
Number of Engines: 4
Passengers: 300
Service Life Flight Hours: 60,000
Service Life Flights: 12,000
Area
Wing Area: 350 square meter
Dimensions
Fuselage Diameter: 6.08 meter
Height: 17.6 meter
Length: 55 meter
Wingspan: 58 meter
Performance
Ceiling: 12,000 meter
Landing Run Distance: 2,100 meter
Max Range: 9,000 kilometer (4,860 nautical mile)
Take Off Run Distance: 3,150 meter
Speed
Cruise Speed: 870 kph (0.73 mach)
Top Speed at High Altitude: 990 kph (0.83 mach)
Time
Service Life: 20 year
Volume
Fuel Tank Capacity: 152,620 liter
Weight
Max Takeoff Weight: 240 ton (529,101 pound)
Payload: 40 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-96-300 News

There are 2 news between
17 Apr 2009 and 23 Apr 2009
Thursday, April 23, 2009UAC Delivers an Il-96-300 Presidential Jet and an Il-96-400T Freighter
Friday, April 17, 2009Manufacturer Trials Complete on Presidential Il-96-300 Aircraft

Operators & Related Equipment


OperatorsItems
Russia?
Four aircraft used for presidential transport

Grand Total ?2
Propulsion Systems
PS90Ax4
Copyright © 2003-2017 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.