Ilyushin IL-96-300 Specs, Cockpit, Cabin Interior, and Price – Ilyushin IL-96-300 is a wide body long-distance passenger aircraft. Designed by Russian aircraft designer Sergey V ILyushin, this aircraft was produced by the Voronezh Aircraft Production Association. Aerodynamic configuration, design and systems use the latest solutions, ensuring high security and economic efficiency in operations. Ilyushin IL-96-300 complies with all international ecological requirements and thus can be operated in all regions of the world. This aircraft is recognized for operating from high altitude aerodynamics and can land in the IIIA and IIIB ICAO airfield categories.
The first flight was conducted on September 28, 1988. The pilot was S.G. Blizniuk. Certificate Type No. 22-96-300 AR by IAC was granted in December 1992. Ilyushin IL-96-300 began operations in July 1993 with Aeroflot Russian International Airlines. There are around 19 Ilyushin IL-96-300 which have been produced where 6 units are operated by Aeroflot and 3 units are operated by Domodedovo Civil Aviation Enterprise, 2 for AiRUnion (KrasAir) 1 for Atlant-Soyuz Airlines, 3 for Cubana de Aviacion, and 4 for Rossiya Airlines (VIP flight unit, used for presidential flights).
The cabin layout of the Ilyushin IL-96-300 holds 262 passengers, with 18 54in pitch seats and 244 32in pitch seats. The galley is positioned on the upper deck, 16 LD-3 containers and the crew toilet are located on the lower deck. Another 289 seat layout specification is done by increasing seats in the business class section from 18 to 44 with pitch 34in. The flight crew consisted of only 3 people. This is possible because of the use of a modern system and glass cockpit. In terms of reliability, security and cost effectiveness, Ilyushin IL-96-300 is the same as its foreign counterparts.
Cruising distance with a maximum load of 37.5 tin (82,675 lb) and 9000 km (4850 nm) of reserves, with 30 tons (66,140 lb) 10,000 km (5400 nm (nautical miles)), with 15 tons (33,070 lb) 12000 km ( 6500 nm).
Operating empty weight 121,500 kg (267,860 lb), max take off weight 250,000 kg (551,160 lb), max landing 183,000 kg (403,450 lb), fuel tank capacity of 150,000 liters (39,625 gallons).
Wingspan (end to end) 60.11 m (197 ft (feet) 3 in (Inches), body length 55.35 m (181 feet 7 inches), height 17. 17.55 meters (57 feet 7 inches), wingspan 391.6m2 (4215.0 square foot (sq ft)).
Russia. Aircraft with PS-90A engines and 2nd generation sound absorbing structures (ZPK-2) comply with ICAO requirements regarding emissions and noise
The PS-90A engine was certified in 1992 and in accordance with the noise limit of ICAO stage 3. The fuel consumption of this engine is 0.595kg / kgf per hour. Flight height is supported up to 13,100 m. Cruising speed 850 to 900 km / h (460-485 knots). Long distance roaming speed of 0.78 Mach, high speed roaming 0.80 Mach and maximum speed of 0.84 mach.
Ilyushin IL-96-300M and Ilyushin IL-96-300T variants are driven by the Pratt & Whitney PW 2337 engine with a thrust rating of 165kN (37,000 lbf). Modern turbofan engines include fans, compressors, turbines, combustion chambers and exhaust nozzles. All components play an important role and develop thrust that in turn pushes the aircraft forward.
The six-screen electronic flight instrument system (EFIS) serves as a flightdeck instrument display system that incorporates the initial proximity warning system (GPWS) and also displays weather radar data. Communication and navigation on Ilyushin IL-96-300 is carried out with the help of the KPRTS-95М-1 control panel, which is incorporated in the aircraft.
This aircraft is managed with the help of VSS-95-1V flight management system. This system meets RNP-1 requirements while database loading is carried out in accordance with ARINC-424. Ilyushin IL-96-300 electronic indication system is SEI-85М and KISS-1-2МA. This aircraft is equipped with SRPBZ field assistance system. Ilyushin IL-96-300 has a CAS-81A (or SPS-2000) air impact avoidance system and Aero mini M or Aero I. satellite communication system.
The first flight was conducted on September 28, 1988. The pilot was S.G. Blizniuk. Certificate Type No. 22-96-300 AR by IAC was granted in December 1992. Ilyushin IL-96-300 began operations in July 1993 with Aeroflot Russian International Airlines. There are around 19 Ilyushin IL-96-300 which have been produced where 6 units are operated by Aeroflot and 3 units are operated by Domodedovo Civil Aviation Enterprise, 2 for AiRUnion (KrasAir) 1 for Atlant-Soyuz Airlines, 3 for Cubana de Aviacion, and 4 for Rossiya Airlines (VIP flight unit, used for presidential flights).
Ilyushin IL-96-300 Specs
The design of the Ilyushin IL-96-300 aircraft uses modern materials to reduce aircraft weight while ensuring the required rigidity and durability. A large-diameter aircraft gives passengers a new level of comfort during long flights. The new wing ensures reliable and safe flight in all operational speed ranges.The cabin layout of the Ilyushin IL-96-300 holds 262 passengers, with 18 54in pitch seats and 244 32in pitch seats. The galley is positioned on the upper deck, 16 LD-3 containers and the crew toilet are located on the lower deck. Another 289 seat layout specification is done by increasing seats in the business class section from 18 to 44 with pitch 34in. The flight crew consisted of only 3 people. This is possible because of the use of a modern system and glass cockpit. In terms of reliability, security and cost effectiveness, Ilyushin IL-96-300 is the same as its foreign counterparts.
Cruising distance with a maximum load of 37.5 tin (82,675 lb) and 9000 km (4850 nm) of reserves, with 30 tons (66,140 lb) 10,000 km (5400 nm (nautical miles)), with 15 tons (33,070 lb) 12000 km ( 6500 nm).
Operating empty weight 121,500 kg (267,860 lb), max take off weight 250,000 kg (551,160 lb), max landing 183,000 kg (403,450 lb), fuel tank capacity of 150,000 liters (39,625 gallons).
Wingspan (end to end) 60.11 m (197 ft (feet) 3 in (Inches), body length 55.35 m (181 feet 7 inches), height 17. 17.55 meters (57 feet 7 inches), wingspan 391.6m2 (4215.0 square foot (sq ft)).
Ilyushin IL-96-300 Engine
Ilyushin IL-96-300 aircraft uses four two-shaft PS-90A turbofan engines with a thrust rating of 16,000kgf (157kN, 35,300lbf) and was developed by Perm Motors Holding, Russia. The PS-90A design is a twin-spool, high-bypass-ratio turbofan with a fan and core air flow. The engine has 11 modules, a noise suppression system and thrust reversing on the fan duct. The aircraft also includes an additional VSU-10-02 power unit built by Baranov Manufacturing Union,Russia. Aircraft with PS-90A engines and 2nd generation sound absorbing structures (ZPK-2) comply with ICAO requirements regarding emissions and noise
The PS-90A engine was certified in 1992 and in accordance with the noise limit of ICAO stage 3. The fuel consumption of this engine is 0.595kg / kgf per hour. Flight height is supported up to 13,100 m. Cruising speed 850 to 900 km / h (460-485 knots). Long distance roaming speed of 0.78 Mach, high speed roaming 0.80 Mach and maximum speed of 0.84 mach.
Ilyushin IL-96-300M and Ilyushin IL-96-300T variants are driven by the Pratt & Whitney PW 2337 engine with a thrust rating of 165kN (37,000 lbf). Modern turbofan engines include fans, compressors, turbines, combustion chambers and exhaust nozzles. All components play an important role and develop thrust that in turn pushes the aircraft forward.
Ilyushin IL-96-300 Cabin
Ilyushin IL-96-300 can accommodate up to 300 passengers. Single class (Single Class) 300 seats in 9 rows with 2 cabins. The three classes consist of 235 seats with 22 first class seats in 6 lines with 102 cm (40 inch) seats, 40 business classes in 8 lines with 90 cm (35 in) distance, and 173 economic classes in 9 lines with 87 distance (34 in). Front lower trunk can carry LD3 type containers or pallet with a capacity of 9000 kg (19,840 lb) and rear luggage can carry 10 LD3 containers or pallet with a capacity of 15,000 kg (33,070 lb).Ilyushin IL-96-300 Cockpit and Avionics
Avionics systems at Ilyushin IL-96-300 are modern systems made in Russia and they comply with ICAO standards. This aircraft is equipped with Collins digital avionics. Ilyushin IL-96-300 features a flight management system (FMS), an inertial and satellite navigation system, and a collision air avoidance system (CAS) that contains an S. transponder mode. and navigation. Computer-assisted control that is supported by an electric-hydraulic system with an artificial reserve mechanical channel insuring the aircraft.The six-screen electronic flight instrument system (EFIS) serves as a flightdeck instrument display system that incorporates the initial proximity warning system (GPWS) and also displays weather radar data. Communication and navigation on Ilyushin IL-96-300 is carried out with the help of the KPRTS-95М-1 control panel, which is incorporated in the aircraft.
This aircraft is managed with the help of VSS-95-1V flight management system. This system meets RNP-1 requirements while database loading is carried out in accordance with ARINC-424. Ilyushin IL-96-300 electronic indication system is SEI-85М and KISS-1-2МA. This aircraft is equipped with SRPBZ field assistance system. Ilyushin IL-96-300 has a CAS-81A (or SPS-2000) air impact avoidance system and Aero mini M or Aero I. satellite communication system.
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