The Ilyushin Il-96 (Russian: Илью́шин Ил-96) is a Russian four-engined jet long-haul wide-body airliner designed by Ilyushin in the former Soviet Union and manufactured by the Voronezh Aircraft Production Association in Russia. It is powered by four high-bypass Aviadvigatel PS-90 two-shaft turbofan engines.
It is used as the main Russian presidential aircraft. The type's only commercial operator in passenger service is Cubana de Aviación.
Despite its usefulness on domestic routes in the Soviet Union, the serviceable but ultimately disappointing performance of the Il-86, especially in regards to range caused Ilyushin to begin planning to produce the long range Il-86D variant and the design was completed in 1976. The main changes from the base Il-86 included slightly longer wings and increased fuel capacity. The Il-86D project was eventually cancelled, but it laid the foundation for the Il-96, and the new design has a strong resemblance to the older Il-86. The new Il-96 featured larger wings, a shorter fuselage, new modern avionics and systems, and, perhaps most important, the new PS-90A high-bypass turbofan, which greatly decreased fuel consumption and increased overall performance. The prototype was first flown 20 September 1988 and the aircraft was certified in 1992. Aeroflot began passenger service in 1993. In June 2005, the Volga-Dnepr Group signed a 15-year financial agreement with Ilyushin Finance Corporation (IFC) to take delivery of two new-build Il-96-400T aircraft, to be operated by Volga-Dnepr's subsidiary AirBridge Cargo. The first was due to have been delivered in late 2006.[1]
The Cuban Government newspaper Granma announced on 3 January 2006 the first official flight of the Cubana Il-96-300, from Havana to Buenos Aires, Argentina.[2]
On 11 August 2009 Russian Minister of Industry and Trade Viktor Khristenko announced that manufacturing of the Il-96-300 would cease. In particular, the Il-96-300 had been deemed inferior to counterparts from Boeing and Airbus, and the manufacturer could not arrange commercially viable mass production, making only one aircraft per year.[3] The Il-96-400T cargo version was to remain in production.
On 9 October 2015, it was announced that an updated version of the Il-96 may be produced. This decision was taken due to the current diplomatic situation between Russia and the West, and the dependency of the Russian aerospace industry on Airbus and Boeing.[4] In September 2017, the Vice President of Russia's United Aircraft Corporation Aleksandr Tulyakov announced the start of development of the 250–280 seat, wide-body long-haul aircraft in partnership with Chinese builders. The aircraft is to be a development of the Russian-designed IL-96 and will be assembled in China. A new engineering center will be built in Russia to undertake technical and electronics production.
In March 2022, after International sanctions during the Russo-Ukrainian War, the CEO of Rostec Sergey Chemezov announced a large scale production relaunch of the Il-96.[5]
The Ilyushin Il-96 is a shortened, long-range, and advanced technology development of the Soviet Union'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. The basic Il-96-300 is equipped with modern Russian avionics integrating six multi-function colour LCD displays, inertial and satellite navigation systems, and a Traffic Collision Avoidance System (including mode "S"). It allows the airplane to be operated 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.
The Il-96-300 has a standard passenger capacity of 262 seats in a two-class configuration with 18 seats with a seat pitch of 54inches and 244 seats with a pitch of 32inches, of which typical seating is 3–3–3 (layout), but low density seating is possible with 2–4–2 (layout). Galleys are positioned on the upper deck, and the lower deck can accommodate 18 LD-3 containers and crew rest areas.
There are two variants of the Il-96. The Il-96-300 was launched in 1985 with introduction into service in 1993. The Il-96M was launched in 1993 with introduction into service in 2000.
The Il-96-300 is the initial variant and is fitted with Aviadvigatel (Soloviev) PS-90A turbofans with a thrust rating of 16,000 kgf (157 kN, 35,300 lbf). Development started in the mid-80s while the first prototype flew on 28 September 1988. The first Il-96 entered service with Aeroflot in 1993. Range with 262 passengers and fuel reserves (for holding 75 minutes at an altitude of 450 m) in a two-class configuration is about 11,000 km (5,940 nmi), allowing flights from Moscow to US west coast cities, a great improvement over the Ilyushin Il-86.
The Il-96M 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 165 kN (37,000 lbf). Range with 312 passengers in a three-class configuration or 92 tonne (203,000 lb) payload is about 10,400 km (5,600 nmi). This turned it into a true—but vastly more capable—Il-86 successor. Development on the M/T variant stalled when the US Export–Import Bank suspended talks on financing the engines and avionics, following pressure from Boeing. The dispute was later settled following an Aeroflot order for ten Boeing 737-400s—placed in April 1997 in a deal worth US$440 million that were granted a tax exemption by the Russian government. Nevertheless, the financing was blocked again when four Boeing 767-300ERs also ordered by Aeroflot were not included in the accorded exemption. The deal was never realised.
This is the freighter version of the Il-96-400. It is powered by four Aviadvigatel PS-90A1 engines.[8]
Only a handful of Il-96-400T aircraft were built and most of them were in storage until recently. Sanctions on Russia by Boeing and Airbus have changed the situation though and in December 2023, Sky Gates who are owned by Red Wings leased an IL-96-400T and started using it to carry cargo to and from Russia.[9] The plane received an overhaul prior to being leased in order to make sure it met air worthiness standards. Russian media suggest a second Il-96-400T is currently being overhauled and it too will be leased to Sky Gates in early 2024, once the overhaul is complete.[10] [11]
By January 2020, the first test-flight airframe was in final assembly and the wing and fuselage were joined, to be finished at the end of 2020 before a first flight in 2021,[19] but by April 2021 it was announced that the aircraft will not enter mass production as expected because of "lack of interest from the airlines and the worldwide idling of the long-range fleet due to the pandemic".[20] Still, due to sanctions, on 15 August 2022, it was announced that the first flight of the Il-96-400M was planned.[21] On 7 June 2023, the United Aircraft Corporation rolled out Russia's future wide-body passenger airliner. It made its first flight on 1 November 2023.[22] [23] [24]
Projected freighter version of Il-96 with an enlarged fuselage to transport oversize cargo.
Projected double-deck version of Il-96 for 550-600 passengers and powered by Kuznetsov NK-93 propfan engines. Following flight tests in 2007 the engines were removed and the aircraft was not developed further.
, Ilyushin is studying a new variant of airliner based on Il-96, powered by two Aviadvigatel PD-35s rated at, developed by 2025 from the PD-14, or powered by foreign powerplants. The goal would be to reduce fuel consumption and maintenance costs.[29]
As of December 2023, current operators of the Ilyushin Il-96 are:[30]
| Operator | Aircraft type | In service | On order | Stored | |
|---|---|---|---|---|---|
| Il-96-300 | 1 | – | 2 | ||
| Il-96-400T | 1 | 1 | – | ||
| Il-96-300 | 1 | – | – | ||
| Rossiya (operated for the Government of Russia) | Il-96-300 | 10 | – | 1 | |
| Il-96-300 | 2 | 3 | – | ||
| Il-96-400M | 1 | – | |||
| Il-96-400T | – | 1 | |||
| Il-96-400TZ | 1 | – | – | ||
| Total | 16 | 3 | 6 |
The following sheet lists the number of finished aircraft per year since the start of its production:[31] [32]
| Year | 1988 | 1989 | 1990 | 1991 | 1992 | 1993 | 1994 | 1995 | 1996 | 1997 | 1998 | 1999 | 2000 | 2001 | 2002 | 2003 | 2004 | 2005 | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Prod | 1 | 2 | 1 | 1 | 2 | 1 | 3 | 2 | 0 | 1 | 0 | 1 | 0 | 0 | 0 | 1 | 2 | 1 | |
| Year | 2006 | 2007 | 2008 | 2009 | 2010 | 2011 | 2012 | 2013 | 2014 | 2015 | 2016 | 2017 | 2018 | 2019 | 2020 | 2021 | 2022 | 2023 | |
| Prod | 2 | 2 | 0 | 2 | 0 | 1 | 1 | 1 | 0 | 1 | 1 | 0 | 0 | 0 | 0 | 2 | 0 | 1 |
In the entire history of operation with the Il-96, there have been no accidents causing the deaths of passengers or crew.
| Variant | Il-96-300 | Il-96M | Il-96T | Il-96-400 | |
|---|---|---|---|---|---|
| Cockpit crew | 3 | 2 | 2/3 | ||
| Seats (1/2/3-class) | 237/263/300 | 307/340/420 | 315/386/436 | ||
| Cargo capacity | t | m3 | m3 | ||
| LD3 capacity | |||||
| Length | 55.35m (181 ft 7 in) | 64.69m (212 ft 3 in) | 63.93m (209 ft 9 in) | ||
| Wing | 60.12m (197 ft 3 in) span, 350m2 (3767.9 ft²), 30° sweep | ||||
| Fuselage | 6.08 m (19.94 ft) diameter, 5.70 m (18.70 ft) cabin width[36] | ||||
| Height | 17.55m (57ft 7in) | ||||
| OEW | 120.4 t (265,198 lb) | 132.4 t (291,630 lb) | 116.4 t (256,387 lb) | 122.3 t (269,383 lb) | |
| MTOW | 250 t (551,000 lb) | 270 t (595,000 lb) | 270 t (594,713 lb) | 265 t (583,700 lb) | |
| Max. payload | 40 t (88,105 lb) | 58 t (127,753 lb) | 92 t (202,643 lb) | 58 t (127,753 lb) | |
| Fuel capacity | 152,620l (40,322US gal) | ||||
| Engines (×4) | Aviadvigatel PS-90A | PW2037 | PW2337 or PS-90A1 | PS-90A1 | |
| Thrust (×4) | 156.9 kN (35,242 lbf) | 170.1 kN (38,250 lbf) | 166.8 kN (37,500 lbf) | 170.7 kN (38,326 lbf) | |
| Cruise | 0.78–0.84Mach / 850–870 km/h / 459–469kn TAS; 13,100m (43,000ft) Ceiling | ||||
| Range | 10,000 km (5,400nmi)[37] | 11,482 km (6,195nmi)[38] | 9,700 km (5,237nmi) | 10,000 km (5,400nmi)[39] | |
| Takeoff run (MTOW) | 2,340m (7,677 ft) | 3,000m (9,843 ft) | 2,700m (8,858 ft) | 2,700m (8,858 ft) | |
| Landing run | 860m (2,821 ft) | 1,800m (5,906 ft) | 1,650m (5,511 ft) | 1,650m (5,511 ft) | |
The airplane has the following systems installed, providing compliance with ICAO recommendations and Eurocontrol requirements: