Jump to content

Ilyushin Il-96

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by BilCat (talk | contribs) at 04:49, 14 October 2018 (Undid revision 863945286 by 2601:181:C381:73E0:C44B:82E2:F044:9FD2 (talk)). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Il-96
An Aeroflot Il-96-300 at Sheremetyevo International Airport in 2011
Role Widebody jet airliner
Manufacturer Voronezh Aircraft Production Association
Design group Ilyushin
First flight 28 September 1988; 36 years ago (1988-09-28)
Introduction 29 December 1992 with Aeroflot
Status In low-rate production, In service
Primary user Cubana
Produced 1992–present[1]
Number built 30[2][3]
Developed from Ilyushin Il-86

The Ilyushin Il-96 (Template:Lang-ru) is a Russian four-engined 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 Aviadvigatel PS-90 two-shaft turbofan engines.

Design and development

Inside an Ilyushin Il-96 operated by Cubana de Aviación

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. 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 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.[citation needed]

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 54 inches (140 cm) and 244 seats with a pitch of 32 inches (81 cm), 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.

Cockpit of an Aeroflot Il-96-300

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.[4]

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.[5]

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.[6] 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.[1] 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.[7] 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.

Variants

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.

Il-96-300

Cubana de Aviación Ilyushin Il-96-300

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.[citation needed]

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. A highly customized version of the Il-96-300, called Il-96-300PU is used as the primary aircraft in the Russian presidential aircraft fleet. Four were used by Russian president Vladimir Putin, and by Dmitry Medvedev as VIP planes. The VIP aircraft is operated by Russia State Transport Company.[8] The Cuban leadership use the IL-96-300.

There were plans to produce a variant dubbed Il-96-300V which would include two sets of Airstairs in it.[9]

Il-96M

Il-96T in Atlant-Soyuz Airlines livery at the MAKS Airshow, August 2007

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. The Il-96M/T is broadly comparable with the Airbus A330-300 and McDonnell Douglas MD-11CF, 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, 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.

Il-96T

This is the freighter version of the Il-96-400. It is powered by four Aviadvigatel PS-90A1 engines.[10]

Il-96-400

The Il-96-400 is similar to the Il-96M, but features Russian avionics and engines. It is powered by four Aviadvigatel PS-90A1 turbofans and can carry up to 436 passengers. Typical two-class configuration will have 386 passengers. Range with 315 passengers in a three-class configuration is about 10,000 km.[11] A special version, dubbed Il-96-400VT, was reported on Friday 19 March 2010 by the Wall Street Journal to bid on the US $40 billion Air Force Tanker Program contract.[12] In February 2013, Cubana signed a deal for the order of three 350-seater Ilyushin Il-96-400s.[13]

Il-96-400M

In February 2017, it was announced that Russia’s United Aircraft Corporation had signed a contract with its subsidiary Ilyushin Aviation Complex for the development of a new version of Ilyushin Il-96-400 wide-body passenger airliner. The first flight of the new aircraft is scheduled for 2019. Il-96-400M is the passenger version of the Il-96-400T cargo aircraft. Its fuselage is 9.65 m longer than the existing Il-96-300 passenger variant. The planned seating capacity is 390 passengers.[14][15] In 2017, the Kremlin injected ₽3.6 billion ($57.4 million) into the Ilyushin Il-96-400M.[16]

Il-96-400TZ

In January 2015, a new tanker variant of the Il-96, designated the Il-96-400TZ, was proposed, with an initial order for two aircraft placed by the Russian Ministry of Defense.[17] The new tanker would have been able to transfer more than 65 tons (IL-78M 40 tons) of fuel at a distance of up to 3500 km (Il-78M 3000 km). Universal aviation refueling systems ORM-1, proven on existing combat aircraft tankers Il-78/78М, would have been installed on the aircraft.[18][19] In May 2018, the Russian Ministry of Defence cancelled the contract citing that the cost "has significantly exceeded that initially expected".[20]

Twin engine

To reduce fuel consumption and maintenance costs, Ilyushin is studying a twin-engined development, powered by over 340 kN (76,000 lbf) Aviadvigatel PD-35s developed by 2025 from the PD-14, or foreign powerplants.[21]

Operators

Current operators

As of December 2016, current operators of the Ilyushin Il-96 are:[22]

Operator Aircraft Type In Service On Order Stored
Cuba Cubana de Aviación Il-96-300 4 3 1
Russia Ilyushin Il-96-300 1 — —
Russia Rossiya (government fleet) Il-96-300 10 — —
Russia VASO Il-96-400T — — 1
Russia Russian Ministry of Defence Il-96-400TZ — 2 —
Total 15 5 2

Production by year

Year 1988 1989 1990 1991 1992 1993 1994 1995 1996 1997 1998 1999 2000 2001 2002
Prod 1 1 2 1 2 1 3 2 0 1 0 1 0 0 0
Year 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017
Prod 1 2 1 2 2 0 2 0 1 1 1 0 1 1 1

[citation needed]

Accidents and incidents

  • In 2005, Russia indefinitely grounded Ilyushin 96-300 passenger aircraft after transport inspectors pointed out malfunctions in the jets’ braking systems. The decision came just weeks after a technical glitch in an Ilyushin 96-300 forced Russian President Vladimir Putin to fly in a back-up plane during a visit to Finland.[23]
  • On 3 June 2014, RA-96010 of Aeroflot, which had been retired from service, was damaged beyond economical repair in a fire while parked in storage at Sheremetyevo International Airport, Moscow.[24]

Specifications

Measurement Il-96-300 Il-96M Il-96T Il-96-400
Length 55.3 m (181 ft 7 in) 64.7 m (212 ft 3 in) 63.939 m (209 ft 9.28 in)
Span 60.11 m (197 ft 3 in)
Wing area 350 m² (3767.9 ft²)
Wing sweep 30°
Flaps/Slats I – 2°/3° (275 KIAS), II 3°/25° (264 KIAS), III – 10°/25° (243 KIAS),
IV – 25°/25° (210 KIAS) for Takeoff, V – 40°/25° (189 KIAS) for Landing
Cabin width 5.70 m (18.70 ft)[25]
Fuselage Diameter 6.08 m (19.94 ft)
Height 15.7 m (57 ft 7 in)
Operating Empty Weight 120,400 kg (265,198 lb) 132,400 kg (291,630 lb) 116,400 kg (256,387 lb) 122,300 kg (269,383 lb)
Max. Zero Fuel Weight 180,000 kg (403,000 lb) 208,400 kg (459,030 lb)
Max. Landing Weight 183,000 kg (403,083 lb) 220,000 kg (484,581 lb) 220,000 kg (484,581 lb) 220,000 kg (484,581 lb)
Max. Take-off Weight 250,000 kg (551,000 lb) 270,000 kg (595,000 lb) 270,000 kg (594,713 lb) 265,000 kg (583,700 lb)
Max. Payload 40,000 kg (88,105 lb) 58,000 kg (127,753 lb) 92,000 kg (202,643 lb) 58,000 kg (127,753 lb)
Takeoff Run at MTOW 2,340 m (7,677 ft) 3,000 m (9,843 ft) 2,700 m (8,858 ft) 2,700 m (8,858 ft)
Landing Run 860 m (2,821 ft) 1,800 m (5,906 ft) 1,650 m (5,511 ft) 1,650 m (5,511 ft)
Cruising speed 0.78 to 0.84 Mach or 850 to 870 km/h TAS (459 to 469 KTAS)
Maximum speed (Vmo) 0.84 Mach or 900 km/h IAS (485 KIAS)[26]
Service ceiling 13,100 m (43,000 Ft)
Cruise Altitude 9,000 to 12,000 m (29,527 to 39,370 Ft)
Range with max. payload 11,500 km (6,209 nmi) 12,800 km (6,907 nmi) 5,000 km (2,699 nmi) 10,000 km (5,400 nmi)
Range with max. fuel 13,500 km (7,289 nmi) 15,000 km (8,100 nmi) 12,000 km (6,479 nmi) 12,000 km (6,479 nmi)
Max. Fuel capacity 152,620 l (40,322 US gal)
Engines (x4) Aviadvigatel PS-90A[27] Pratt & Whitney
PW2037		 Pratt & Whitney PW2337
or
Aviadvigatel PS-90A1		 Aviadvigatel PS-90A1[28]
Thrust (x4) PS-90A: 156.9 kN
(35,242 lb)
N2:10,425 RPM		 170.1 kN
(38,250 lb)
N2:12,360 RPM		 PW2337: 166.8 kN
(37,500 lb)
N2:12,360 RPM		 PS-90A1: 170.7 kN
(38,326 lb)
Engine Dry Weight (x4) 2,950 kg
(6,497 lb)		 3,314 kg
(7,300 lb)		 PW2337: 3,314 kg
(7,300 lb)		 2,950 kg
(6,497 lb)
Cockpit crew Three Two Two (op. Three)
3-class Seating capacity 237 307 315
2-class Seating capacity 263 340 386
1-class Seating capacity 300 420 436
Cargo Capacity F.H.1: 9,000 kg (Front)
F.H.2: 15,000 kg (Back)
F.H.3: 1,000 kg (Back)
6 LD3 (front)
10 LD3 (Rear)		 580 m³ main deck
114 m³ front lower deck
82 m³ rear lower deck
18 LD3 (Front)
14 LD3 (Rear)		 114 m³ front lower deck
82 m³ rear lower deck

18 LD3 (Front)
14 LD3 (Rear)

Data from Ilyushin Aviation Complex,[29] FAA Certification Document A54NM and Il-96-300 Pilot Manual

Avionics

PS-90A engine

The airplane has the following systems installed, providing compliance with ICAO recommendations and Eurocontrol requirements:

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

  1. ^ a b "В России воссоздадут конкурента Boeing и Airbus". Новости Mail.Ru. Archived from the original on 2015-12-24. Retrieved 2015-11-09. {{cite web}}: Unknown parameter |dead-url= ignored (|url-status= suggested) (help)
  2. ^ "✈ russianplanes.net ✈ наша авиация". Archived from the original on 2015-12-11. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  3. ^ Стрюк, Игорь. "22.07.2016: Новый Ил-96 передан специальному летному отряду "Россия"". Retrieved 14 August 2016.
  4. ^ "Volga-Dnepr Group signs up for two new Il-96-400T aircraft". VOLGA-DNEPR GROUP. 27 March 2005. Archived from the original on October 16, 2007. Retrieved 29 March 2014. {{cite news}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  5. ^ Gómez Lluciá, Julio (January 3, 2006). "Realiza su primer vuelo oficial IL 96-300 de" (in Spanish). Granma. Archived from the original on March 4, 2008. {{cite news}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  6. ^ Kolobkov, Sergei (August 11, 2009). "The short-lived Il-96-300" (in Russian). RBC Daily. Archived from the original on August 14, 2009. Retrieved 2009-08-01. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  7. ^ "Russian-Chinese passenger jet to take on Boeing & Airbus".
  8. ^ "Ilyushin Il-96 Production List". Archived from the original on 1 April 2015. Retrieved 26 March 2015. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  9. ^ Александр, Артемьев. "ШИРОКОФЮЗЕЛЯЖНЫЙ ДАЛЬНЕМАГИСТРАЛЬНЫЙ ПАССАЖИРСКИЙ САМОЛЕТ ИЛ-96-300 - Крылья сверхдержавы". www.e-reading.club.
  10. ^ "Ил-96-400Т - ПАО «Ил»". www.ilyushin.org.
  11. ^ "Il-96-400". Ilyushin. Archived from the original on September 19, 2008. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  12. ^ John Pike. "Il-96-400VT Aerial Tanker". Retrieved 26 December 2014.
  13. ^ "Cubana buys Antonov An-158 and Il-96-400s". Archived from the original on 27 July 2013. Retrieved 26 December 2014. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  14. ^ http://www.rusaviainsider.com/improved-ilyushin-il-96-airliner-to-fly-in-2019/
  15. ^ "VASO to Build a Passenger Il-96-400M Prototype by 2019". 15 August 2016.
  16. ^ Vladimir Karnozov (July 9, 2018). "Kremlin Boosts Effort toward 'Indigenization' of SSJ100". AIN online.
  17. ^ "MAKS: Russia extends Il-96 production by several years". Flightglobal. 27 August 2015. Retrieved 31 August 2015.
  18. ^ "bmpd". livejournal.com. Archived from the original on 2016-02-09. {{cite web}}: Unknown parameter |dead-url= ignored (|url-status= suggested) (help)
  19. ^ "Минобороны России закупит новые самолеты-топливозаправщики". function.mil.ru. Retrieved 3 July 2015.
  20. ^ "Russian MoD Cancels Il-96-400TZ Aerial Tanker Contract". 9 May 2018.
  21. ^ David Kaminski-Morrow (9 Feb 2018). "Ilyushin studies twin-engined version of Il-96". Flightglobal.
  22. ^ "Archived copy". Archived from the original on 2015-12-11. Retrieved 2015-12-16. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)CS1 maint: archived copy as title (link)
  23. ^ "Russia: Ilyushin Planes Grounded After Putin Jet Suffers Glitch". RadioFreeEurope/RadioLiberty. Retrieved 2017-12-20.
  24. ^ Hradecky, Simon. "Accident: Aeroflot IL96 at Moscow on Jun 3rd 2014, caught fire while parked". The Aviation Herald. Retrieved 3 June 2014.
  25. ^ "Flight – Airline Industry news, aviation jobs & airline recruitment". Flightglobal.com. Archived from the original on 2012-03-13. Retrieved 2009-12-20. {{cite web}}: Unknown parameter |dead-url= ignored (|url-status= suggested) (help)
  26. ^ The Vmo values for military operation are higher
  27. ^ All the PS-90A turbofan can be upgraded to the new PS-90A2 version, with the latest generation FADEC of western design and many other improvements. The maintenance costs are reduced by 40%. The fuel consumption (SFC) of this version is equivalent to current Western turbofans. PS-90A2 variant meets the ETOPS-180 rules, ICAO-4 and AP-33 (equivalent to FAR-33/JAR-33). The Maximum thrust is 16,000 kg or 18,000 kg. [1]
  28. ^ Ilyushin has not ruled out the possibility to install other engines (PW, RR, or CFM), depending on the number of requests from customers.
  29. ^ "Il-96-300". ILYUSHIN a UAC company. Retrieved 29 March 2014.
Wikimedia Commons has media related to Ilyushin Il-96.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Ilyushin_Il-96&oldid=863954781"