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IL-96 family
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General information
The IL-96-300 aircraft designed by Ilyushin Aviation Complex (city of Moscow, Russia) and manufactured by Voronezh Aircraft Manufacturing Company (city of Voronezh, Russia).
The IL-96-300 is a long-range wide-body aircraft, which successfully incorporates advanced achievements in Russian and foreign aerospace technology, experience of the designer’s and producer’s and highly qualified specialists. The aircraft is powered by four turbofan two-shaft PS-90A engines, produced by Perm Motors (city of Perm, Russia).
| IL-96-300 airplane life time: |
| years |
20 |
| landings |
20000 |
| flying hours |
60000 |
IL-96-300CU (Control Unit) is a special airplane was made for the President of the Russian Federation.
The board equipment of the aircraft gives an opportunity to use it not only as transport facility, but also as working office of the President.
Aircraft performances
| OPERATING WEIGHTS & FUEL CAPACITY |
| Max takeoff weight, t |
|
250 |
| Max payload, t |
|
40 |
| Max landing weight, t |
|
183 |
| Max fuel, t |
|
116,3 |
| Max passenger capacity |
262 |
289 |
| economy class |
244 |
289 |
| business class |
18 |
- |
| first class |
- |
- |
| Center of gravity |
|
19-34% ÑÀÕ |
| DIMENSIONS |
| Overall length, m |
|
55,35 |
| Wing span, m |
|
57,66 |
| Fuselage diameter, m |
|
6,08 |
| Overall height, m |
|
17,57 |
| ENGINE |
| Quantity x type |
4xPS-90À |
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| Maximum engine thrust, kg |
|
57,66 |
| Fuselage diameter, m |
16000 |
|
| Aircraft average fuel rate, t/h |
7,2-7,5 |
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| AIRCRAFT PERFORMANCE CHARACTERISTICS (ISA) |
| Cruising speed, km/h |
|
850-870 |
| Flight altitude, km |
|
9-12 |
| Takeoff roll, m |
|
2700 |
| Required takeoff distance, m |
|
3300 |
| Landing distance, m |
|
1260 |
| Required landing distance, m |
|
2100 |
| RANGE with fuel reserve, km |
|
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| with maximum load |
9000 |
9000 |
| with maximum number of passengers |
11000 |
10800 |
| with maximum fuel |
13500 |
13500 |
| RANGE OF OPERATIONAL TEMPERATURES, °Ñ |
-54…+45 |
Payload – range
Engine PS-90À
Main characteristics
- takeoff thrust (ÌÑÀ, H=0) - 16000 kg
- cruise thrust (ÌÑÀ+10C, Í=11 km, M=0,8) – 3340 kg
- by-pass ratio at maximum continuous power – 4,4
- pressure ratio at maximum continuous power – 31,1
- specific fuel consumption at cruise mode (Í=11 km, M=0,8, ÌÑÀ+10C) – 0.595 kg/kgfxh
- fan diameter – 1,90 m
- engine length – 5,533 m
- engine length inlet – 6.184 m
- engine weight – 2950 kg
Cabin equipment
LATEST ICAO RECOMENDATIONS
The crew and passenger cabins correspond to protection requirements of the aircraft against the illegal intervention of terrorists (the Amendment 27 to a Part 1 of the Appendix 6 to ICAO). Also both cabins correspond to safety requirements (Chapter 11 of the Appendix 8 to ICAO).
AVIONOICS
The IL-96-300 aircraft equipped with modern Russian made avionics which includes six multifunctional color-LCD displays, electro remote management system, inertial navigation system, collision air avoidance system (including mode “S”) and satellite navigation equipment, VHF communication with grid of 8,33/25 kHz frequencies, and equipment permitting executes flights in RVSM conditions. 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 allows to navigate and land under ICAO CAT IIIA conditions.
Avionics
On the airplane are installed the following systems providing ICAO recommendations and Eurocontrol requirements:
- Integrated control panel of communication and navigation KPRTS-95Ì-1 and Flight management system VSS-95-1V
- Upgraded Electronic Indication systems SEI-85Ì and KISS-1-2ÌA (redaction 6) with LCD indicators
- Inertial system NSI-2000MT or BINS-85
- Ground approximation system EGPWS with the terrain relief information or SRPBZ (or MARK V)
- Collision air avoidance system CAS-81A (or SPS-2000)
- System BRIK-324
- Domestic system of selective calling of crew on radio communication (Selcal) – ÀSV-324
- Weather locator Buran-À, or MN RLS – without wind shear (or RDR-4B with functions of wind shear warning and turbulence detection)
- MV-range radio station «Orlan-85STD» with maintenance of VDL Mode 2
- Crew satellite communication system Aero Mini M or Aero I (telephone and data exchange with UVD and airline)
- Sound information solid-state registrar RZBN-1, ensuring crew members negotiation recording and cabin sound situation (4 channels) with record conservation of 2 hours of flight information
- System MSRP-A-02 with solid-state protected and operational storage devices
Passenger cabin layout
Economy class
Business class
Passenger cabin layout for 262 seats
/18 seats with pitch 54 inches + 244 seats with pitch 32 inches/
Galleys are positioned on the upper deck. 18 containers LD-3 and crew rest room are positioned on the lower deck.
There is also stipulated a converting of this layout to the 289 seats layout by changing seats in the business class section from 18 to 44 with seats pitch 34".
Technical maintenance
Qualitative implementation of the Program provides flight safety and low-cost operation.
Form «T» (transit): performed after each landing to prepare for the next flight;
Form «D» (base): performed daily principally at the base airport;
Form «S» performed not less than once in 10 days at the base airport.
Form «A»: performed after each 500±50 flight hours;
Form «B»: performed after each 1500±50 flight hours;
Form «C»: performed after each 3000±50 flight hours;
Form «D»: performed after each 20000±1000 flight hours.
As the Buyer gets more experienced in maintenance, the program may be modified/corrected to be more acceptable under certain operation conditions. This encompasses further maintenance optimization (decrease in work load and increase in periodicity).
Customer support
The IL-96-300 product support program is based on the IAC and VASO experience in international and domestic product support of Ilyushin aircraft. To provide an adequate service to the Buyer after the sale of the aircraft IFC has established by ”IFC Technik” to provide the following aspects of product support:
- technical maintenance
- spares
- crew training
- personnel training
- customer service
- engineering support
- technical library
- ground equipment
- overhaul.
Service life and warranties
Airframe
Service life of the airframe is not less than 20 years or 60000 flight hours.
With each aircraft, the Buyer will be provided with a package of product warranty on the basis of VASO’s standard Technical Delivery Terms, consisting of:
- 24 months or 4000 flight hours or 800 cycles (whatsoever shall occur first) coverage for proprietary parts of the aircraft manufactured by VASO;
- the appropriate warranty documentation from VASO’s suppliers covering the quality of their own parts.
Engines
Service life of the engines is not less than 60000 flight hours and 10000 cycles in case technical maintenance is performed properly.
With each engine, the Buyer will be provided with a package of product warranty on the basis of PMZ’s standard Technical Delivery Terms consisting of:
- 2 years or 1000 flight hours or 500 cycles (whatsoever shall occur first) coverage for proprietary parts of the aircraft manufactured by PMZ;
- the appropriate warranty documentation from PMZ’s suppliers covering the quality of their own parts.
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