Ilyushin Il-96

The Ilyushin Il-96 (Russian: Ил-96) is a four-engined long-haul widebody airliner designed by Ilyushin in the Russian Federation and manufactured by the Voronezh Aircraft Production Association in Voronezh. It is powered by four Aviadvigatel PS-90 two-shaft turbofan engines

Design and development

The Ilyushin Il-96 is a shortened, long-range, and advanced technology development of Russia's first widebody airliner, the Ilyushin Il-86. It features supercritical wings fitted with winglets, a glass cockpit, and a fly-by-wire control system. It was first flown in 1988 and certified in 1992. The basic IL-96-300 is equipped with modern Russian avionics integrating six multi-function color LCD displays, inertial and satellite navigation systems, and a Traffic Collision Avoidance System (including mode "S"). It allows operating the airplane with two crew members. The avionics correspond to modern requirements on international routes in Europe and North America (RNP-1) and allow navigation and landing under ICAO CAT III/A conditions. The Il-96 is offered in three main variants: the Il-96-300, Il-96M/T and Il-96-400.

Specifications
Measurement Il-96-300
Length 55.3 m (181 ft 7 in)
Span 60.11 m (197 ft 3 in)
Height 17.5 m (57 ft 7 in)
Zero Fuel Weight 183,000 kg (403,000 lb
Maximum take-off weight 250,000 kg (551,000 lb)
Takeoff Run at MTOW 2,600 m (8,530 ft)
Cruising speed .83 Mach (1,037.5 km/h)
Maximum speed .86 Mach (1075 km/h)
Range fully loaded 11,000 km (5,939 nmi
Max. fuel capacity 150,000 l (39,625 US gal)
Engines (example) Aviadvigatel PS-90A
Cockpit crew Three
3-class Seating 259