Wednesday, 13 March 2019

Sukhoi Superjet 100 Specs, Cabin, Cockpit, and Price

20:00
Sukhoi Superjet 100 Specs, Cabin, Cockpit, and Price – Sukhoi Civil Aircraft Company (AVPK Sukhoi) announced the Russian Regional Jet program (RRJ) in June 2001. Sukhoi was responsible for the design and manufacture of aircraft. The Russian Aeronautics and Space Administration (Rosaviakosmos) and Boeing Company agreed to jointly develop and market Russian Regional Jet and Sukhoi, Ilyushin and Boeing to sign a joint industrial agreement in July 2001.

In June 2001, the Sukhoi Civil Aircraft Company (AVPK Sukhoi) announced the Russian Regional Jet (RRJ) program. In March 2003, Rosaviakosmos announced the election of Sukhoi RRJ by the Russian Government to fulfill initial construction for 200 regional jets. Ilyushin is responsible for aircraft certification. Boeing is responsible for marketing activities (including sales and rentals) and after sales support (including operational, maintenance and spare parts logistics support). The aircraft was renamed the Sukhoi Superjet 100 in July 2006. Sukhoi Superjet 100 variant consists of the Superjet 100-75 and the Superjet 100-95, both variants must be built in the standard and remote versions.

Sukhoi Superjet 100

Sukhoi Superjet 100 First Flight

Sukhoi Superjet 100 with 95 seats was launched in September 2007 at the KnAAPO assembly plant in Komsolmosk-on-Amur, Siberia. The first flight was carried out in May 2008. The second aircraft entered the flight test program with the first flight in December 2008. The third aircraft carried out its flight test in July 2009.

On September 10, 2009, the aircraft began a high-altitude test and successfully completed it on September 23, 2009. The aircraft achieved initial Russian certification in April 2009 and received official certification from the Russian Inter-national Aviation Aviation Committee Registration in February 2011. The type of certificate from the Aviation Security Agency Europe (EASA) was received in 2012.

Sukhoi Superjet 100 specs

Sukhoi Superjet 100 Specs

Sukhoi Superjet 100 has a maximum cruise speed of Mach 0.81 and a maximum height of 12,500 m. Sukhoi Superjet 100-95 range is 3,279 km and 4,620km in the Sukhoi Superjet 100-95LR version.

Sukhoi Superjet 100-95, a total length of 30m, is an outline version of Sukhoi Superjet 100-75 base with two additional plugs in the fuselage for the forward and rear wing. There is also room for future development of the VIP version and Sukhoi Superjet 100 cargo.

The Novosibirsk Aircraft Production Association (NAPO), a member of Sukhoi Holding, produces around 40% of RRJ, including the nose, vertical and horizontal tail surfaces and additional power units. The Komsomolsk-on-Amur Aircraft Production Association (KnAAPO), which is also a member of Sukhoi Holding, produces low-swept rear wings. The RRJ final meeting took place at Komsomolsk-on-Amur.

In March 2005, Sogitech from France and Sukhoi Civil Aircraft signed an agreement to jointly develop specifications to create interactive electronic technical publications through lifelong after-sales support. Intertechnique, based in France, supplies fuel systems. This aircraft has a fuel capacity of 13.135l.

Additional aircraft power supplies were designed by Honeywell and MMPP Salyut. The aircraft is equipped with the Hamilton Sundstrand electrical system and Curtiss Wright's fire suppressor.

Sukhoi Superjet 100 is equipped with a three-wheeled tricycle landing gear that can be pulled from Messier-Dowty with the Sukhoi braking system and Goodrich wheels and brakes. Four wheels are offered as an option for the main landing gear unit.

Sukhoi Superjet 100 Engine

Sukhoi RRJ is powered by two pod machines mounted under the wing. Snecma Moteurs and NPO Saturn have established a joint venture, Powerjet, to produce the SaM146 turbofan engine. Each SaM146 engine has a rating of 62kN to 71kN and is equipped with digital electronic controls (FADEC) full authority Snecma. The engine low pressure system was developed by NPO Saturn.

The Gromov Aviation Research Institute signed an agreement with the Snecma Moteurs to develop the Ilyushin Il-76 flight test for the SaM146 turbofan engine. Engine flight testing began in December 2007. Sukhoi Superjet 100 aircraft meets the requirements of ground noise levels based on ICAO standards Chapter 4 and FAR 36.

Sukhoi Superjet 100 cabin

Sukhoi Superjet 100 Cabin

Aerospace B / E in Florida has designed cabin layout including sidewall and ceiling configurations, luggage baskets, passenger service panels, reading lights, crew and passenger oxygen systems, seats, services, and cabin management systems. Normal seating configuration is three plus two in economy class and two plus two in business class. There is a luggage compartment under the floor at the bottom of the fuselage under the rear and front cabin. The volume of the luggage compartment at RRJ-75 is 16.1m³.

Sukhoi Superjet 100-75 can accommodate up to 78 first class passengers. For airlines with two-class passenger requirements, the alternative configuration provides eight passenger seats on the front of the first class cabin and 62 tourist class seats in the main passenger cabin. The cabin has two passenger doors at the port side and three service doors for embarkation and fast landing and fast turnaround at the airport terminal.

Sukhoi Superjet 100-95 is the first aircraft made and can accommodate up to 98 passengers. The aircraft variant has maximum similarity in design, for example in structural design, system suitability, avionics, landing gear, electrical systems and power systems.

Sukhoi Superjet 100 cockpit

Sukhoi Superjet 100 Cockpit

In June 2005, Thales announced his election by Sukhoi and awarded a contract to provide an avionics package for the new Sukhoi Superjet 100 aircraft. The flight deck has a design similar to the one on an Airbus A380. The avionics suite includes cockpit display, communication, navigation and surveillance systems. CMC Electronics is a supplier for the CMA-9000 flight management system (FMS).

Leibherr Aerospace, based in Toulouse, and the Voscod Design Center in Russia are responsible for the RRJ flight control system. Leibherr also developed air conditioning and control systems.

Sukhoi Superjet 100 Price and Orders

The price of a Sukhoi Superjet 100 aircraft is US $ 35 million in 2012 and US $ 50.1 million in 2018. Firm orders have been received for 122 aircraft plus 56 choices from customers including: Aeroflot (30 plus 15 options), Kartika Airlines (15 plus 15 choices), Sibir Airlines (50), Concord Aviation (20 plus 20), Dalavia Far East Airways (six), AirUnion (30), Interjet (15 plus five options), Armavia (two plus two), ItAli Airlines (10 plus 10) and Avialeasing Aviation Company (24 plus 16 options). In July 2008, Superjet International announced firm orders for five aircraft from Asset Management Advisors (AMA) from Switzerland. Avialeasing ordered 24 aircraft in July 2009.

At the 2009 Paris Air Show, where the aircraft made its first flight, the Hungarian national airline Malev Airlines signed a statement of intention to buy 30 Sukhoi Superjet 100 for € 710 million.

In September 2007, Sukhoi and Alenia Aeronautica established a joint venture company, Superjet International. The company is 51% owned by Alenia and 49% by Sukhoi and is responsible for aircraft marketing and support in the West. The settlement and shipping center is located in Venice, Italy.

In July 2012, Interjet changed five options based on a contract signed in January 2011 to become a company order. All five aircraft were sent in February 2014. The first aircraft was sent to Armavia in April 2011. In June 2011, the aircraft entered commercial operations with Aeroflot. Aeroflot received the sixth complete specification of the Sukhoi Superjet aircraft in February 2014.

In June 2011, Italian Blue Panorama Airlines ordered $ 370 million for 12 Sukhoi Superjet100 aircraft. And PT Sky Aviation ordered $ 379.2 million for 12 Sukhoi Superjet 100 / 95B aircraft.

In October 2011, SuperJet International received an order of $ 200 million from Comlux The Aviation Group for two Sukhoi Business Jets (SBJ) plus two options. Deliveries are scheduled to take place in 2014. In June 2012, Transaero Airlines installed a $ 566.4 million contract for six Sukhoi Superjet 100 / 95B aircraft plus 10 options.

Tuesday, 12 March 2019

Ilyushin IL-96-300 Specs, Cockpit, Cabin Interior, and Price

20:41
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).

Ilyushin IL-96-300

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 specs

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 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

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.

Ilyushin IL-96-300 Price and Orders

The price of one unit of Ilyushin IL-96-300 aircraft is US $ 86 Million. Since June 2009, 21 Ilyushin IL-96-300 aircraft have operated with 12 more aircraft. Airlines using the aircraft are Rossiya (four in service, one according to order), ILyushin Design Bureau (one in service), KrasAir (two in service), Iran Air (six in order), Atlant-Soyuz Airlines (two in order)) , Aeroflot (six in service), Cubana (three in services, one in order), Clean Air (two in order), Polet (two in service, one on order), Conviasa (two on orders) and other Russian airlines (five in service). In addition, the Ilyushin IL-96-300 aircraft was also used as a presidential aircraft, previously used by Vladimir Putin and currently used by Russian President Dmitri Medvedev.

Monday, 11 March 2019

Ilyushin IL-62 Specs, Jet Engine, Cockpit, and Price

22:24
Ilyushin IL-62 Specs, Jet Engine, Cockpit, and Price – Ilyushin IL-62 is the first intercontinental intercontinental jet produced by the Russian Flight Complex Ilyushin. Over the years, it has become a mainstay of the Soviet civil air fleet. This aircraft is capable of flying in adverse weather conditions, at any latitude and anytime day or night. The airline has completed 8,500 flight hours since it was founded in 1967 with regional and intercontinental flights on the Aeroflot route.

The first flight of Ilyushin IL-62 was carried out on January 2, 1963 with the pilot test being V.K. Kokkinaki. Ilyushin IL-62 has undergone flight certification in accordance with ICAO international airworthiness requirements for civil aircraft and has been operating regularly on Aeroflot's local and international flights since 1967. Ilyushin IL-62 aircraft broke five world speed and reach records in 1977. Ilyushin production IL-62 ended in 1990, when 292 aircraft were produced.

This aircraft has two variants, Ilyushin IL-62M and Ilyushin IL-62MK. Ilyushin IL-62MK is a medium-range passenger aircraft that has strong wings and landing gear to operate with greater gross weight. And Ilyushin IL-62M is a plane equipped with four Soloviev D-30KU turbofan engines. This aircraft can carry five crew and 174 passengers. It features luggage and containerized transport systems, which are damaged wing spoilers and modern flight decks.

Ilyushin IL-62

Ilyushin IL-62 Specs

Ilyushin IL-62 has a loading room, dual mechanical flight control, tail support actuation and wheel brake. It also consists of an electric motor for incident tailplane control and a hydraulic nosewheel steering.

The aerodynamic design of the Ilyushin IL-62 wing and T-shaped tail reduces mass. The design is based on the British VC-10 aircraft. Ilyushin IL-62 is equipped with flight control navigation equipment that includes an automatic control system, manual control system and the main parameter control system.

Ilyushin IL-62's main landing gear is positioned before the aircraft's center of gravity when empty, which allows to reduce the horizontal tail surface area. For parking and land transportation operations from empty aircraft, the designer introduces a retractable tail landing gear, which makes loading and unloading of the aerodrome easier, and can be done in any order.

Ilyushin IL-62 can reach heights varying between 8,000 m and 12,000 m. It has a service ceiling of 13,000 m and a maximum durability of 35,000 hours. This aircraft weighs around 67,500 kg and the maximum takeoff weight is 161,000 kg.

Ilyushin IL-62 specs

Ilyushin IL-62 Engine

The aircraft is powered by four Kuznetsov NK-8-4 turbojet by-pass engines. Each machine can produce a thrust of 10,500kg. Four engines on the rear of the aircraft reduce the noise level in the cabin, increase passenger comfort, and reduce the possibility of fire on the boat due to the remoteness of the engine from the fuel tank. With the engine Ilyushin IL-62 can go up at a speed of 5.3 m / s. It has a maximum speed of 900 km / h and cruising speed of 850 km / hour. The normal range is 7,550 km and has a maximum range of 9,200 km.

Ilyushin IL-62 cabin

Ilyushin IL-62 Cabin

The Ilyushin IL-62 aircraft consists of two pressurized cabins separated by a lobby and cabin crew rest area. The cabin has three toilets, a buffet and a bar. This can accommodate 186 passengers. This aircraft has a semi-monocoque cross section of the passenger body and an ergonomic passenger door. It also comes with a six-parallel seating arrangement for standard international flights.

Ilyushin IL-62 cockpit

Ilyushin IL-62 Cockpit and Avionics

Ilyushin IL-62 uses Automatic Direction Finder and Doppler navigation radar to monitor its position and speed. Other avionics include dual radio altimeters, automatic radio transponders, tannoy cabin systems and intercoms, friend identification or enemy transponders, emergency evacuation systems, automatic flight control systems, instrument landing system receivers, global positioning systems, and vertical receiver omni-directional radio range .

Ilyushin IL-62 Prices and Orders

The price of one Ilyushin IL-62 aircraft is US $ 51.2 Million.

Sunday, 10 March 2019

Ilyushin IL-114 Specs, Cabin, Cockpit, and Price

21:15
Ilyushin IL-114 Specs, Cabin, Cockpit, and Price – Ilyushin IL-114 is a middle-class passenger jet designed and manufactured by the Russian Ilyushin Aviation Complex (IAC). It was built to replace the old fleet of IL-14 and An-24 aircraft deployed in Russia. 14 Ilyushin IL-114 currently operates worldwide. Ilyushin IL-114 turboprop aircraft was designed for local routes. Ilyushin IL-114 made its inaugural flight from the Gromov Flight Research Institute airport on March 29, 1990. The aircraft was flown by a crew under the pilot-test command V. Belousov.

The development of Ilyushin IL-114 began in the 1980s. Production began in 1992. Four prototypes were built with the aim of achieving certification in 1993. However, the test program was delayed when one of the prototypes that underwent a flight path crashed in July 1993 due to a technical error in the engine or propeller. The cargo version, Ilyushin IL-114T, also suffered an accident in 1999 during flight testing. The aircraft received Russian certification in April 1997.

Ilyushin IL-114

Ilyushin IL-114 Specs and Design

Ilyushin IL-114 is based on a free monoplane lift design. This aircraft is made of a sophisticated composite metal mixture, including titanium, to reduce its overall weight. It was designed to take off and land from an unpaved airfield or a short runway even in poor climatic conditions.

Ilyushin IL-114 is equipped with modern technology to maintain the aerodynamics and efficiency of the required weight of the aircraft and power units, thus providing high fuel efficiency.

Ilyushin IL-114 is equipped with a conventional tricycle type landing gear. Retractable wheels are combined with a telescopic shock absorption system that provides stability to the aircraft when landing on synthetic or non-paved runways.

The landing gear wheel allows it to land on aerodromes that are not ready with concrete or ground runways that contribute to the expansion of Ilyushin IL-114 use in various regions. In addition, this aircraft is designed for independent operations at airports that are not equipped. Ilyushin IL-114 has an integrated air passenger. Access to all structural elements and units, inspections required by the maintenance program, fast and easy.

Ilyushin IL-114 can fly at a maximum speed of 500 km / hr. The normal range and ferries are 1,000 km and 4,800 km respectively. The service ceiling is 7,600 m. The take-off and landing rates are 1,500 m and 1,300 m respectively.

Ilyushin IL-114 specs

Ilyushin IL-114 Engine

Ilyushin IL-114 is powered by two TV7-117S turboprop engines, each worth 1,900kW. The engine is driven by a six-bladed SV-34 propeller provided by Aerosila. Produced by Klimov Corporation, the TV7-117S consumes 500kg to 550kg of fuel per hour. The TV7-117S engine maximizes fuel efficiency and reduces noise and gas emissions. The length and diameter of the machines are 2.1 m and 0.94 m, respectively. The dry weight is 530kg.

Ilyushin IL-114 cabin

Ilyushin IL-114 Cabin 

Ilyushin IL-114 cabin with a length of 18.9 m and a width of 2.64 m accommodates 64 passengers in a two-seat configuration. The cabin height is 1.92 m. The ergonomically designed cabin is equipped with a luggage compartment, air conditioning system and a digital engine control system. The overhead panel is also included to provide blurry light which creates a comfortable atmosphere for passengers on the plane. The passenger cabin of the aircraft ensures comfortable flight within the overall height range.

Ilyushin IL-114 cockpit

Ilyushin IL-114 Cockpit and Avionics 

Ilyushin IL-114 crew consisted of a pilot-in-command and co-pilot. For successful flight crew performance, all flight data display devices and warning systems, as well as aircraft system controls, are combined in a single information and control system by sending data to a digital display, which is located in the pilot panel instrument.

Ilyushin IL-114 has an all-digital glass cockpit that can accommodate two crew members. The flight deck is equipped with five color displays including head to top (HUD), main flight display (PFD), multifunction display (MFD), navigation display, and warning display.

The screen allows pilots to analyze and prevent failures caused by engines, power supply systems, air conditioners, antifreeze systems, cabin air pressure, position of landing gear, doors and other systems.

The flight navigation package of this aircraft allows the operation of Ilyushin IL-114 in the day and night, in visual weather conditions and instruments, in storms, and ensures takeoff and landing in the ICAO II standard weather conditions.

The system is configured in such a way that the failure of one system does not affect the performance of the other. The system requires a level of redundancy and uses proven material.

Ilyushin IL-114 Price and Orders 

One unit of Ilyushin IL-114 had an estimated price of US $ 11 Million in 2008. Vyborg Airlines purchased two IL-114 aircraft from IAC in the MAKS Airshow held in 2005. Venezuela signed an agreement with IAC during the 2007 MAKS Airshow to hold 98 IL-114 , but the agreement was canceled. Uzbekistan Airways acquired five Ilyushin IL-114 in July 2010.

Saturday, 9 March 2019

Embraer E195-E2 Specs, Cabin, Range, and Price

16:59
Embraer E195-E2 Specs, Cabin, Range, and Price – Embraer E195-E2 is the second generation aircraft from the commercial jet Embraer E-Jet. With travel costs 22% lower than Airbus A320neo (154 seats) and 24% under Boeing 737 MAX 8 (160 seats), Embraer E195-E2 is expected to open new markets and spur strong demand from airlines. Embraer E195-E2 starts operating in the first half of 2019.

Since the Embraer E195-E2 aircraft prototype was launched at the Paris Air Show in June 2017. Embraer plans to invest around $ 1.7 billion for the development of three aircraft over the next eight years. International Lease Finance Corporation (ILFC) has now ordered 25 Embraer E195-E2 aircraft at the Paris Air Show.

Embraer E195-E2

Embraer E195-E2 Specs

The Embraer E195-E2 wing has a high aspect ratio and features a sophisticated aerodynamic design. New generation aircraft will be designed to reduce fuel consumption, emissions, noise and maintenance costs.

The length of Embraer E195-E2 is 41.5m (136ft) and has a height of 10.9 m (36 feet). The maximum takeoff weight of Embraer E195-E2 is 59,400 kg. The maximum landing weight is 53,750kg.

The main components for the E2 aircraft are being supplied by Liebherr (control systems for flaps and blades), Moog (fly-by-wire system) and Rockwell Collins (horizontal stabilizer control system).

Wheels, brakes, auxiliary units (APU) and electrical systems are provided by UTC Aerospace Systems. Crane Aerospace & Electronics will provide electronic control modules for landing gear, brake control systems and proximity sensors. Triumph will supply the aircraft segment, steering and elevators. Aernnova Aerospace was chosen to provide vertical and horizontal stabilizers. Intertechnique will supply engines and feed APU fuel, pressure refueling, fuel transfers and ventilation systems.

Embraer E195-E2 is equipped with the advanced Primus EpicTM 2 integrated avionics system developed by Honeywell. Avionics will include a large landscape display with the Next Generation Flight Management System (NGFMS). This will also include advanced graphics capabilities, and 4th generation fly-by-wire flight controls. The avionics suite will provide situational pilot awareness and flexibility for innovation on the flight deck.

Embraer E195-E2 specs

Embraer E195-E2 Engine

The E2 aircraft will be equipped with two directed turbofan engines developed by Pratt & Whitney. Embraer E195-E2 each is equipped with two PW1900G engines, with each engine producing thrusts up to 22,000 lbf. The maximum speed of the aircraft is 870 km / hour. The service ceiling will be 41,000 feet (12,500 m). The Embraer E195-E2 range will be 3,704km (2,000nm).

Embraer E195-E2 cabin

Embraer E195-E2 Cabin

The cabin interior design will be enhanced to provide more comfort and a flexible environment for passengers. The aircraft will feature a spacious cabin without a central seat. The aircraft cabin design contract was given to Priestman Goode, a company based in the UK. In a unique single classroom layout, Embraer E195-E2 will have seating capacity for 132 passengers.

Embraer E195-E2 Price and Orders

One Embraer E195-E2 unit is sold at a price of US $ 60.4 Million. Currently Embraer has sold more than 435 type units to the North American market since 2013, which is equivalent to 80% of all orders on the 76 seat market. The E2 family has been a significant success for Embraer, with the transition of smooth delivery to Wideroe in April 2018 where it now operates longer flights.

Horizon Air is a big customer for Embraer with the airline because it has 26 E195-E2 in its fleet at the end of the year and four additional schedules for shipping during 2019.