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Ilyushin Il-96




The Ilyushin Il-96 is a four-engined long-range Russia n Widebody airliner.

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 Winglet s, a Glass Cockpit , and a Fly-by-wire control system. It was first flown in 1988 and certificated in 1992. The Il-96 comes in three main variants: the Il-96-300, Il-96M/T and Il-96-400.


IL-96-300

The Il-96-300 is the initial variant and is fitted with Aviadvigatel (Soloviev) PS90A turbofans with a thrust rating of 16,000 Kgf (157 KN , 35,300 Lbf ). Development started in mid-80s while first prototype flew on 28 September 1988 , with Russian certification was obtained on 29 December 1992 . The first Il-96 entered service with Aeroflot in 1993 .

Range with 235 passengers in a three-class configuration is about 4,850 nautical miles (9,000 km), allowing flights from Moscow to US west coast cities, a far improvement over the Ilyushin Il-86 , but still inferior to the performance of the Airbus A340 and the later versions of the Boeing 777 . It is used by Russian President Vladimir Putin as a VIP plane. The aircraft, however, has a nickname of "Poor man's Boeing 767 " by Russian Media.

Although its list price is more than 30% lower than the equivalent western types, Russian airlines are not particularly eager to buy it. As Of February 2006 , there are only 17 Il-96-300s in operation with Aeroflot (6 of the 17), KrasAir (3), Domodedovo Airlines (3; actually operated by Krasair on behalf of AiRUnion alliance), Atlant-Soyuz Airlines (1; cargo version), Cubana De Aviacion (2) and President Putin's airwing (2). Two more aircrafts are being readied at the plant in Voronezh for shipment to the government of Cuba . Both Aeroflot and Transaero received tax exemption when importing Western-built aircraft in exchange for their promising to buy a few Il-96's each. So far, neither airline made good on that promise.

Meanwhile, Air Zimbabwe is planning to purchase 5 Il-96-300, making airline largest carrier of the type outside Russia and second largest carrier to operate the planes after Aeroflot .

Following a series of incidents, one of which embarrassingly involved President Putin's jet in Turku , Finland , Russian civil aviation authorities grounded all the Ilyushin-96-300's from 22 August to 3 October 2005 to examine the braking gear.

The Cuban official newspaper Granma announced on 3 January 2006 the first official flight of the first Cubana IL-96-300, from Havana, Cuba to Buenos Aires, Argentina {Link without Title} .


IL-96M/T

This is a stretched variant of the Il-96-300. It features a 10 m (30 ft) fuselage stretch, is 15 tonnes (33,000 lb) heavier, is fitted with Western-style avionics, and is powered by four Pratt & Whitney PW2337 engines with a thrust rating of 37,000 lbf (165 kN). Range with 312 passengers in a three-class configuration or 92 tonne (203,000 lb) payload is about 5,600 nautical miles (10,400 km). This turned it into a true—but vastly more capable—Il-86 successor. The Il-96M/T is broadly comparable with the Airbus A330-300 and Boeing 777-200A , but is much cheaper. Development on the M/T variant stalled when the US Export-Import Bank suspended talks on financing the engines and avionics, due to Russia's economic problems {Link without Title} .

The Il-96M/T dispenses with the Flight Engineer , making it a two-pilot airliner.


IL-96-400

The Il-96-400 was developed with Russian avionics and engines. It is based on the Il-96M/T fuselage and is powered by four less-powerful Aviadvigatel (Soloviev) PS90A turbofans; consequently its performance was affected. Range with 235 passengers in a three-class configuration is about 4,800 nautical miles (8,900 km). The newer Aviadvigatel PS90-A2 restores the original Il-96-M/T design range and overcomes this performance deficit.


Other versions

  • Il-96PU : VIP transport version for the Russian President.

  • Il-96-300V : Long-range version with increased fuel.



SPECIFICATIONS (IL-96-300)


  plane Or Copter plane
  jet Or Prop jet
  crew 3
  capacity <br>
  length Main 5535 m
  length Alt 181 ft 7 in
  span Main 6011 m
  span Alt 197 ft 3 in
  height Main 1755 m
  height Alt 57 ft 7 in
  area Main 3916 m&sup2
  area Alt 4,215 ft&sup2
  empty Weight Main 121,500 kg
  empty Weight Alt 267,900 lb
  loaded Weight Main kg
  loaded Weight Alt lb
  useful Load Main 183,000 kg
  useful Load Alt 403,000 lb
  max Takeoff Weight Main 250,000 kg
  max Takeoff Weight Alt 551,000 lb
  number Of Jets 4
  engine (jet) Aviadvigatel PS-90 A
  type Of Jet Turbofan s
  thrust Main 160 kN
  thrust Alt 36,000 lbf
  max Speed Main 940 km/h
  max Speed Alt 510 kt, 580 mph
  range Main 9,000 km
  range Alt 4,900 nm, 5,600 mi
  ceiling Main m
  ceiling Alt ft
  climb Rate Main m/s
  climb Rate Alt ft/min
  loading Main kg/m&sup2
  loading Alt lb/ft&sup2



REFERENCES AND EXTERNAL LINKS



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