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IL96
ILyushin IL-96-300 is developed by Russian Aviation Industry . This aircraft was developed from ILyushin IL-86 ,medium range, wide body. ILyushin IL-96-300 is a long range airliner with features new wings (with winglets), fuselage shortened by 4 meters compared to the IL-86, a digital EFIS flight deck and fly-by-wire control. The initial model IL-96-300 equipped with Soviet Perm PS-90A engines , most of aicraft that were built delivered to Aeroflot. The first IL-96-300 flew on September 1988 , received Russian Certification in December 1992 and entering service with Aeroflot the following year. IL-96-300 resembles the Airbus A-340. Both began development and test flight the planes at about the same time.      ILyushin IL-96M, IL-96T(Cargo version), both use foreign made engines. IL-96M/T derivertives from IL-96-300. They have a stretched fuselage (4.76 m.) and equipped with Pratt & Whittney PW2337 engines which increasing fuel economy and reliability and Rockwell Collins flightdeck avionics. IL-96M took a first flight on April 1992.       The cost of PS-90A engine is about 4 times cheaper than PW 2337.
SPECIFICATIONS ILYUSHIN IL-96
	IL-96-300	IL-96M
Typical passenger load	350 basic single class 235 (three classes arrangement)	375 basic single class 312 (three classes arrangement)
Cargo loading version	40,000 kg.	58,000 kg.
Range	8,890 km. (4,800 nm.)	10,371 km. (5,600 nm.)
Number of engine	4	4
Engine (Turbofan)	Soloviev PS-90A	Pratt & Whittney PW2237
Engine Thrust	Soloviev PS-90A = 16,110 kgs	Pratt & Whittney PW2237=170.1 kN
Wing span	60.10 m.	60.10 m.
Length	59.94 m.	64.70 m.
Operating speed	900 km/h	870 km/h
Ceiling	12,100 m.	12,100 m.
Empty weight	117,000 kg.	132,400 kg.
Max.take off weight	216,000 kg.	270,000 kg.
Crew	3 (2 pilots and 1 flight engr.)	2
		Cockpit ILYUSHIN IL-96
		Cockpit ILYUSHIN IL-96M
1 nm.(nautical mile) = 1.15155 miles, 1 kt (knot) = 1.15155 mile / hr. 1 mach = 761 mph.(SL,ISA)