The Ilyushin Il-96 is built by Ilyushin in the Soviet Union as a four-engined jet capable of long-haul flights. It was a wide-body airliner introduced on December 29, 1992, with Aeroflot, and was produced by the Russian manufacturer Voronezh Aircraft Production Association (VASO) on the same year up to the present.

Manufacturer:
Ilyushin
Country:
Russia
Manufactured:
1992 to: Present
ICAO:
IL96
Price:
US$50 million (2019)
Avionics:
Engine:
4x Aviadvigatel PS90-A1
Turbofan
Power:
38,326 pound-force
Max Cruise Speed:
469 knots
869 Km/h
Approach Speed (Vref):
Travel range:
5,400 Nautical Miles
10,001 Kilometers
Fuel Economy:
Service Ceiling:
43,000 feet
Rate of Climb:

Take Off Distance:
2700 metre - 8,858.16 feet
Landing Distance:
1650 metre - 5,413.32 feet
Max Take Off Weight:
265,000 Kg
584,219 lbs
Max Landing Weight:
Max Payload:
58,000 Kg
127,867 lbs
Fuel Tank Capacity:
40,322 gallon
152,635 litre
Baggage Volume:
Seats - Economy / General:
436 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
2.86 metre - 9.38 feet
Cabin Width:
5.7 metre - 18.70 feet
Cabin Length:
44.4 metre - 145.67 feet
Exterior Length:
63.9 metre - 209.64 feet
Tail height:
15.7 metre - 51.51 feet
Fuselage Diameter:
6.08 metre - 19.95 feet
Wing Span / Rotor Diameter:
60.1 metre - 197.18 feet
Wing Tips:
Canted Winglets

Blog Mentions

Blog posts that mention the Ilyushin Il-96 400:

The Ilyushin II-96 is a derivative of the first widebody airliner of the Soviet Union, the Ilyushin II-86. Unlike its antecedent, the II-96 is capable of flying on longer ranges, and equipped with more innovative technology. It is fitted with supercritical wings incorporating winglets, as well as a glass cockpit with electronic flight instrument displays, and fly-by-wire technology. In 1988, the aircraft made its first flight. In 1992, the Il-96 was awarded its type certification. The airliner has three major versions namely the Il-96-300, Il-96M/T, and Il-96-400.

The Il-96-400 is the same as the Il-96M. However, unlike the Il-96M that features Pratt and Whitney engines, the Il-96-400 is fitted with engines and avionics systems from Russia. The aircraft is a quadjet- it is powered by four Aviadvigatel PS-90A1 high-bypass commercial engines rated at 38,326 lbf thrust. Its engine is a twin-spool high-bypass turbofan with a single-stage fan, four-stage low-pressure and thirteen-stage high-pressure compressor, fully annular combustors, and two-stage high-pressure and four-stage low-pressure turbine.

The aircraft can accommodate a maximum of 436 passengers on board and the standard two-class layout can seat 386 passengers. It has a travel range of 5,400 nautical miles while carrying 315 passengers in a three-class layout. The aircraft has a service ceiling of 43000 feet and a cruise speed of 459 to 469 knots. It has a takeoff and landing distance of,2700 meters and 1,650 meters, respectively. The Il-96-400 has a maximum takeoff weight of 265,000 kg, a maximum payload of 58,000 kg, and a fuel tank capacity of 40,322 US gallons.

The Il-96-400 has an exterior length of 63.9 meters, an exterior height of 7 meters, a tail height of 15.7 meters, and a fuselage diameter of 6.08 meters. The aircraft cabin is 2.86-meter-high, 5.7-meter-wide, and 44.4-meter-long. It has a wheelbase of 26 meters, a wingspan of 60.1 meters, and a wing area of 350 square meters.
In February 2013, the Cuban Aviation Corporation signed a contract with Ilyushin for the three Il-96-400 aircraft orders.

All Ilyushin Aircraft

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