Wednesday, 31 July 2019

Aerion AS2 Specs, Interior, Cockpit, and Price

01:00
Aerion AS2 Specs, Interior, Cockpit, and Price – Aerion AS2 is a Supersonic Business Jet (SBJ) which is being designed by Aerion Corporation together with Boeing, United States. This supersonic business jet will have the ability to fly up to 70 percent faster than today's business jets. Aerion AS2 will save about three hours of transatlantic flights while meeting environmental performance requirements.

Aerion AS2 was announced in May 2014 during the 2014 European Business Aviation Convention (EBACE), held in Geneva, Switzerland. AS2 is a redesigned version of Aerion SBJ, which was announced by Aerion in 2004. The first AS2 flight was scheduled for 2023, and the aircraft is expected to receive certification in 2023.

Aerion AS2 supersonic business jet

Aerion AS2 Specs

Aerion AS2 is designed to achieve maximum speed. It combines an oval shaped body with transverse and short wings. Wings, fuselage, empennage, and nacelle engines will be made of carbon fiber material, while the front end of the wing will be built using titanium alloy to protect from erosion.

Aerion AS2 will have a length of 49m, a width of 21m and a height of 8m. Long and narrow planes reduce the wave resistance, which is further reduced by narrowing the front of the aircraft and the center of the fuselage, where the wings, engine and fuselage meet.

The Aerion AS2 wing will have an area of ​​125m². The Aerion AS2 wing, which was not swept, resembled a modern fighter, especially designed to reduce obstacles above Mach 1 and display a relatively smaller aspect ratio. The supersonic natural laminar flow design (SNLF) reduces the total airframe resistance by 20%.

The wings are thin and smooth with relatively sharp edges and the upper and upper surfaces are slightly curved. They combine high-lift, low sweep, and strong flaps that allow approach and landing speeds to be similar to large subsonic jets.

Aerion AS2 engine

Aerion AS2 Engine

Aerion AS2 will be equipped with three engines of 15,000lb thrust class, supporting a low bypass configuration. The company launched the GE Affinity engine design for AS2 in 2018. Aerion is talking to all leading engine manufacturers to determine the optimal core engine that complies with AS2 requirements.

Compared to dual-engine business jets, tri-engine jets are more efficient because they require shorter runways for take-off. Failure of one machine can still allow two thirds of the power to be available and therefore lower power reserves will be needed. For the same reason, the engine can be sized more efficiently and optimized in terms of power output. Each tri-jet engine produces lower thrust compared to twin jet configurations.

The Aerion AS2 supersonic business jet is designed to fly at speeds up to Mach 1.4 or around 1,000 miles per hour. It will sail at speeds up to Mach 0.99 in geographical zones where supersonic flights are banned, and at speeds of Mach 1.1 to 1.2 above populated areas, without creating sonic explosions on land.

Its speed can be increased to Mach 1.6 on water and can fly on high, low supersonic and high speed supersonic cruises on one flight.

The maximum distance of the aircraft is 9,260 km. It takes a landing distance of less than 4,000 feet and a runway length of 7,500 feet to take off when fully charged. The basic working weight of AS2 is 22,588 kg, with a maximum takeoff weight of 52,163 kg.

The runway length can be 6,000 feet or shorter when carrying less fuel load, while the aircraft will not need additional land equipment and can achieve the same fuel efficiency in both subsonic and supersonic regimes.

Aerion AS2 interior

Aerion AS2 Cabin and Interior

The Aerion AS2 cabin is 9.1 m long, 1.87 m high, and 2.2 m wide. This will include a two-room layout, a four-step grouping club of individual chairs and four chairs around the conference or dining table at the back.

The cabin can be equipped with cots, increasing the total passenger capacity to 11. The seat can be configured as a bed for four passengers during an overnight flight. The cabin will also feature a kitchen, two laundry rooms, walking baggage, and a compartment.

Aerion AS2 cockpit

Aerion AS2 Cockpit and Avionics

The Aerion AS2 cockpit will feature a modified version of Primus Epic Honeywell's integrated cockpit. Honeywell will utilize the design work that has been carried out on flight control systems on supersonic fighter jets. Together with NASA, Honeywell will display an intuitive cockpit and touch screen controls, as well as several technological innovations for this supersonic aircraft.

Aerion AS2 Price and Orders

The Aerion AS2 price is around US $ 120 Million. In November 2015, Flexjet confirmed that it had ordered $ 2.4 Billion for 20 Aerion AS2, with shipments starting in 2023.

Monday, 29 July 2019

Airbus ACJ320neo Specs, Interior, Cockpit, and Price

01:00
Airbus ACJ320neo Specs, Interior, Cockpit, and Price – Airbus ACJ320neo is the longest single-aisle business jet in the A320 family produced by Airbus. ACJ320neo is developed based on the popular A320neo aircraft. The development of the company's jets includes features such as additional fuel tanks in the cargo space that will provide more intercontinental range, plus greater cabin pressure for better passenger comfort. ACJ320neo successfully completed the first flight for two hours and 40 minutes from Hamburg on November 16, 2018.

Airbus ACJ320neo

Airbus ACJ320neo Specs

Airbus ACJ320neo is based on the commercial variant of the Airbus A320neo. It has an overall length of 37.57m, a height of 11.76m and a wingspan of 35.8m. This aircraft has Sharklets with 2.4m high wing tips that save fuel by reducing drag and increasing take-off and landing performance. Sharklets reduces fuel combustion by 4%, which corresponds to an annual reduction of 900 tons of CO2 emissions per aircraft.

Airbus ACJ320neo Engine

ACJ320neo is powered by two Pratt & Whitney PW1000G or CFM Leap-1A engines. Wing-mounted Sharklets to produce 15 percent fuel savings, which also means a forward leap for business jet operators. This business jet can fly as far as 6,897 miles at speeds of up to Mach 0.82 (around 614 mph).

It consists of ACJ320neo which can fly 25 passengers 13 hours or 6,000 nm / 11,100 km, and ACJ319neo which can carry eight passengers 15 hours or 6,750 nm / 12,500 km, giving it the ability to connect London to Beijing or Moscow to Los Angeles.

Airbus ACJ320neo melody interior

Airbus ACJ320neo Interior and Cabin

The Airbus ACJ320neo cabin has a length of 27.74 m, has a width of 3.7 m and a height of 2.25 m. The cabin's dirty floor area is 96m². The average cabin height of the aircraft is 6,400 feet. With the large cabin, the Airbus ACJ320neo can accommodate up to 25 passengers. This aircraft contains heavy-duty carbon fiber on the desk and cupboard and includes a 650ft bagasi of luggage space to accommodate up to 138 large suitcases.

The interior of the Airbus ACJ320neo cabin is equipped with a harmonious melody curve feature, designed for a quiet and comfortable environment. It has a simple kitchen, lounge and 65in curved television screen on the front of the plane. The entertainment facilities in the cabin include a modern home cinema with a large screen television, featuring ceiling speakers for the best acoustics. Wi-Fi is also available.

The spacious cabin has a private main bathroom with separate bathroom, shower and sink. Has a spacious bedroom with a large double bed and a sofa, while also has a conference room and dining room in the main lounge, which can hold up to six passengers.

Airbus ACJ320neo cockpit

Airbus ACJ320neo Cockpit and Avionics

Airbus ACJ320neo cockpit is equipped with a digital glass cockpit. It also features improved fly-by-wire control protection, a 3B automatic landing category and runway runway prevention, and an airport navigation system on board.

Airbus ACJ320neo Price and Orders

The latest Airbus ACJ320neo price is US $ 115 Million. ACJ received the first order from Acropolis Aviation, Farnborough, in May 2015 for 19 seats Airbus ACJ320neo aircraft. The business unit also arranged to supply six aircraft with the Melody cabin in December 2016. The first Airbus ACJ320neo aircraft, with a newly designed cabin melody, was sent in January 2019. The Aviomlux Aviation group booked three aircraft in February 2016 and the first aircraft shipments were in 2019.

Saturday, 27 July 2019

Airbus ACJ319neo Specs, Interior, Cockpit, and Price

01:00
Airbus ACJ319neo Specs, Interior, Cockpit, and Price – Airbus ACJ319neo is a VIP business jet configuration, within the family of Airbus Corporate Jets (ACJ) developed by Airbus. With new engines and Sharklets, the ACJ319neo provides better ratings and better comfort. In addition, it offers a lower cabin height, equivalent to an average of less than 6,400 feet - providing comfort that is closer to the one visited on the field to increase passenger comfort.

The ACJ319neo launched by Comlux on the VVIP charters in Dubai, is certified to carry 19 passengers in imitated comfort, and is equipped with cabins with lounges and two private rooms - each of which can be arranged to function as a lounge / office or bedroom.

Airbus ACJ319neo

Airbus ACJ319neo Specs

Airbus ACJ319neo has an overall length of 33.84 m, a height of 11.76 m and a wing span of 35.80 m. It features structural fuselage reinforcements and includes heated floor panels to the front. It is also equipped with Satcom Aero I / H +, supply and installation of emergency locator transmitters and the supply and installation of multiple HF systems.

It has wind-slide protection, and a head-up display (HUD) to operate in adverse weather conditions. This can be loaded without land support, and includes airstairs, an additional power unit (APU) and a GPS landing system, which allows it to operate at a remote airport.

This aircraft has a wheelbase of 11.04 m (36ft 3in), a maximum ramp weight of 76.9t (169.5lb) and zero fuel weight of 58.5t (129lb). The takeoff weight is 76.5t (168.6lb) and the landing weight is 62.5t (137.8lb).

Airbus ACJ319neo Engine

The Airbus ACJ319neo is powered by two CFM56-5B7 or CFM LEAP engines, which provide a thrust of 98kN to 120kN (22,000 lbs to 27,000 lbs respectively), while six additional fuel tanks (ACT) provide a maximum fuel capacity of 40.990l.

The jet can fly with a maximum operating speed of 0.82 mach, and can rise to 12,500 m (41,000 feet). It has a range of around 11,100 km, while landing and landing distances are 1,850 m (6,080 ft) and 1,360 m (4,450 ft), respectively.

Airbus ACJ319neo interior

Airbus ACJ319neo Interior and Cabin

The Airbus ACJ319neo cabin can accommodate up to 19 passengers. It has a bathroom and kitchen in the front and a bedroom with a bathroom on the back. These jets can be configured with a series of lounge, office, dining room and conference modules based on customer requirements.

Its length is 24.01 m (78 feet 9 inches), width 3.7 feet (12 feet 1 inch) and is 2.25 meters (7 feet 4 inches) high, and has a gross floor area of ​​82.70 m² (890 feet²).

Airbus ACJ319neo cockpit

Airbus ACJ319neo Cockpit and Avionics

Airbus ACJ319neo has the same cockpit and the same layout of instruments and controls - with the same quality and handling procedures - with other Airbus company jets. This makes it easy for pilots to change from one type to another.

A liquid crystal display (LCD), rather than a cathode ray tube (CRT), can be found on the flight deck. Avionics includes fly-by-wire controls and side-controller for fingertip maneuverability. This controller also activates the pull-out table, while navigation aids such as satellite navigation and category 3B autoland capabilities are included.

Airbus ACJ319neo Price and Orders

The latest Airbus ACJ319neo price is US $ 105 Million. Customers in China submitted their first order to Airbus to supply one aircraft in November 2012, and are expected to be delivered as early as 2015.

Friday, 26 July 2019

Lockheed Martin LM-100J Super Hercules Specs, Cockpit, Cargo, and Price

01:00
Lockheed Martin LM-100J Super Hercules Specs, Cockpit, and Price – LM-100J Super Hercules is a commercial freighter aircraft manufactured by the Lockheed Martin Corporation at the Marietta, Georgia, US. This aircraft is a variant of a commercial multipurpose transport aircraft from the C-130J Super Hercules military transport aircraft. Lockheed Martin submitted an application to the Federal Aviation Administration (FAA) for the LM100J aircraft type certification in February 2014.

The first flight of LM-100J Super Hercules was completed in Marietta in May 2017. It was exhibited for the first time at the International Paris Air Show in June 2017.

Lockheed Martin LM-100J Super Hercules

Lockheed Martin LM-100J Specs

The LM-100J freighter aircraft is the latest version of the L-100 Hercules. This aircraft has a length of 34.37m (112ft 9in), height of 11.81m (38ft 9in), wingspan of 40.38m (132ft 7in) and horizontal tail span of 16.05m (52ft 8in). The broad LM-100J airframe allows aircraft to provide many missions, including cargo, oil and gas, mining logistics, air fire, air shipping, air ambulance, humanitarian assistance operations, personnel transportation, search-and-rescue, and field operations the hard one.

It can operate in short and unprepared airfields without ground support equipment and can be loaded or disassembled with minimal material handling equipment. It can fly in all weather conditions and can provide fast or loose loads at the height of the truck bed. The aircraft also includes a central wing box and increased ice cover protection.

LM-100J Super Hercules specs

Lockheed Martin LM-100J Engine

The LM-100J Super Hercules is supported by four Rolls-Royce AE2100D3 turboprop engines, which produce a power output of 4,591pshp respectively. This engine drives a propeller of six all-composite Dowty R39 blades. This freighter aircraft has a cruising speed of 660km / h and a maximum range of 2.450nm. It offers an additional 50% range of L-100 aircraft.

The LM-100J aircraft can take off with a maximum weight of up to 74,389 kg (164,000 lb), including a maximum payload weight of 21,863 kg (48,200 lb). It has an operating weight of 36,650kg (80,800 lb) and zero weight of fuel 8,513kg (129,000 lb). This freighter aircraft requires a landing distance of 3,100 feet.

LM-100J Super Hercules cargo

Lockheed Martin LM-100J Cargo Transport

LM-100J is designed to serve bulk and oversized markets, especially to developing countries. It can also support oil and gas operations, mining logistics, air firefighting, air shipping, medevac / air ambulances, humanitarian assistance operations, personnel transportation, harsh field operations, and search and rescue.

The LM-100J is capable of carrying 33 percent more cargo than the L-100, which was last marketed in the 1990s. The LM-100J has a range of 4,000 kilometers with a load of 18 tons and can operate with two crew instead of three L-100s.

LM-100J Super Hercules cockpit

Lockheed Martin LM-100J Cockpit and Avionics

The LM-100J freighter aircraft has two cockpit pilots that integrate communication, navigation, air traffic monitoring / management (CNS / ATM) that are compatible with digital avionics with two head-up displays and four head-down displays.

The cockpit includes weather radar and Northrop Grumman land mapping, and a commercial traffic warning system (TCAS). It also features digital autopilot and automatic maintenance and error reporting systems.

Lockheed Martin LM-100J Price and Orders

The latest LM-100J price is around US $ 65 Million. Ireland-based flight group ASL Aviation made an order with Lockheed Martin for ten LM-100J aircraft in July 2014. Bravo Industries agreed to buy ten LM-100J aircraft from Lockheed Martin in July 2016.

Thursday, 25 July 2019

Flaris LAR 1 Specs, Interior, Cockpit, and Price

01:00
Flaris LAR 1 Specs, Interior, Cockpit, and Price – Flaris LAR 1 is a very lightweight, four-seat single-engine business jet developed by Metal Master, a company based in Podgórzyn, Poland. This business jet is intended for customers who need to travel quickly for business or leisure. Flaris LAR 1 debuted at the 2013 Paris Air Show. The first prototype flew on April 5, 2019. The development of this business jet was jointly funded by the European Union.

Flaris LAR 1

Flaris LAR 1 Specs

The Flaris LAR 1 aircraft is built with lightweight carbon fiber material. The fuselage features a geometric design and includes a safety parachute system located in the nose area. It features a semi-elliptical removable wing, which allows the aircraft to be parked in a large garage. The structure of the middle part of the fuselage is supported by two forms of duraluminium integral, which function as fuel tanks. The aircraft's external dimensions are 8,32 m, height 2,43 m, with a wingspan of 8,68 m and a wingspan of 10 m².

Flaris LAR 1 has a range of 2,200 km (1,200 nm) with a maximum load and range of 2,600 km (1,400 nm) with two people and luggage. In addition, the aircraft has an empty weight of 700kg (1,543lb) and a takeoff mass of 1,500kg.

Flaris LAR 1 can take off or land on a 250 m short runway or small airport. It takes 250 m for take-off run and can glide 18 km without encouragement for every 1 km drop in altitude.

Flaris LAR 1 Engine

The Flaris LAR 1 is powered by a single FJ33-5A turbofan engine manufactured by Williams International, with a thrust of 8.2kN. These business jets can fly with a cruising speed of 700 km / h (380 kt) and stop speeds of 115 km / h (62 kt). It has a maximum range of 3,200 km (1,730nm), a maximum climbing rate of 30m / s, and a service ceiling of 14,000 m (46,000 feet).

Flaris LAR 1 cockpit

Flaris LAR 1 Cockpit and Avionics

The Flaris LAR 1 cockpit is equipped with Garmin G600 avionics with a choice of integrated glass Garmin G3000 touch screen. It is equipped with an instrument landing system (ILS) and a field awareness and warning system (TAWS), which will provide guidance to the pilot, while landing under conditions of zero visibility.

Avionics also includes the GTN-750 module with the addition of the GTN-650 receiver that is right below it. This also includes the MPV-50T unit, air speed indicator, altimeter, flap, switch and fuse panel position control switches.

The Flaris LAR 1 aircraft is designed to be operated by a single pilot. This includes the radio and Garmin G600 navigation system that will function as co-pilots. A private pilot license (PPL) is needed to fly aircraft.

Flaris LAR 1 interior

Flaris LAR 1 Cabin and Interior

The Flaris LAR 1 cabin can accommodate four passengers. The cabin has one door on each side and has a multi-bolt door locking system with 11 bolts, which ensures proper air fit to the minimum door mass.

Flaris LAR 1 Price

The latest Flaris LAR 1 price is US $ 2 Million.

Wednesday, 24 July 2019

Cirrus Vision SF50 Specs, Interior, Cockpit, and Price

01:00
Cirrus Vision SF50 Specs, Interior, Cockpit, and Price – Cirrus Vision SF50 is a very lightweight single-engine business jet with seven seats designed and manufactured by Cirrus Design Corporation (CDC), United States. This business jet made its first flight on July 3, 2008. The SF50 was developed with the requirements of a lightweight private jet intended for the single pilot operating market.

In 2011, Cirrus was purchased by CAIGA, a Chinese company that funded the project a year later. The first adjustment prototype then flew on March 24, 2014, followed by two other prototypes that same year. On October 28, 2016, Cirrus Vision SF50 obtained a type certificate from the US Federal Aviation Administration.

Cirrus Vision SF50

Cirrus Vision SF50 Specs

Cirrus Vision SF50 has a low wing monoplane design and consists of carbon fiber composite material. The aircraft can operate day and night, and in an environment that is not friendly.

These business jets are equipped with Cirrus airframe parachute system (CAPS) features, ice protection systems, large abdominal parts, double pelvic fins, steam cycle cooling systems, onboard oxygen generating systems, optional toilets, satellite telephones, lightning detection and ski tubes.

Cirrus Vision SF50 is equipped with a ballistic recovery system, emergency exits, retractable landing gear, dark windows, pusher sticks, single cabin pressure vessels, environmental control systems, and parachutes on large pointed noses.

Cirrus Vision SF50 Engine

Cirrus Vision SF50 is powered by a single William FJ33 turbofan engine with a maximum thrust of 8.5kN. This machine was designed and manufactured by US-based engine manufacturer William International. The length and diameter of the machines are 0.97 m and 0.53 m, respectively. The dry weight is 140kg. The time between repairs (TBO) of the engine is 4,000 hours.

The FJ33 engine is equipped with two stage low pressure turbines, centrifugal high pressure compressors, one stage high pressure turbines, one stage fan and annular combustion.

Cirrus Vision SF50 can fly with a maximum speed of 555 km / hour. The stall speed is 111 km / hour. The service ceiling is 8,500 m. Airplane takeoff and landing distances are 492m and 379m.

Cirrus Vision SF50 interior

Cirrus Vision SF50 Cabin and Interior

Cirrus Vision SF50 has a pressurized cabin in a single carbon shell. The cabin can accommodate six passengers in three rows in a parallel seating configuration. It has an optional seat between the second and third rows.

The cabin is 3.33 m long, 1.56 m wide and 1.24 m high. It features a luggage compartment of 0.88m3 on the back of the aircraft to place passenger luggage. The length, width and height of the luggage compartment are 0.91mX1.22mX0.79m.

Cirrus Vision SF50 cockpit

Cirrus Vision SF50 Cockpit and Avionics

Cirrus Vision SF50 digital cockpit can accommodate a stwo pilots. SF50 was initially integrated with the L-3 SmartDeck avionics suite which was later replaced with the Garmin G1000 avionics package. Garmin Avionics was selected as the main contractor for the avionics package by the CDC in March 2009.

Cirrus Vision SF50 avionics suite includes a 12-inch dual heading heading system (AHRS), dual wide area augmentation system (WAAS), global positioning system (GPS), active traffic system, GPS, XM radio, twin air data computer ( ADC)), Transponder Mode S, audio and telephone input, digital data processing A / P, ADL and SD 3-axis.

Other avionics installed include the second S Mode transponder, automatic direction finder (ADF), distance measuring equipment (DME), enhanced vision system (EVS) and warning and terrain systems (TAWS) to alert pilots of potential conflicts with obstacles and terrain.

Cirrus Vision SF50 Price and Orders

The latest Cirrus Vision SF50 price is around US $ 2-2.3 Million. Cirrus Vision SF50 has 431 orders with the first shipment taking place in 2012.

Tuesday, 23 July 2019

Daher TBM 930 Specs, Interior, Cockpit, and Price

01:00
Daher TBM 930 Specs, Interior, Cockpit, and Price – TBM 930 is a single turboprop engine business jet, designed and manufactured by Daher. This business jet was launched in Tarbes, France, in April 2016 and was first shown at the International Sun-Fun Fun Fly-In Expo at Lakeland Airport, Florida. In the same year the European Aviation Safety Agency (EASA) and the US Federal Aviation Administration (FAA) gave a certificate of type of airworthiness to TBM 930.

Daher TBM 930

Daher TBM 930 Specs

TBM 930 is an enhanced version of the TBM 900 business jet, which was introduced in March 2014. The external dimensions of the aircraft are 10.73 m long, 4.35 m high, and a wingspan of 12.83 m. The wheelbase is 2.91m and the tailplane range is 4.98m. The aircraft is equipped with pilot access doors, large access doors with retractable ladders, and emergency and maintenance doors providing access.

The TBM 930 aircraft was built using various aluminum and steel alloys, as well as titanium and sophisticated composite materials. It is also equipped with new anti-corrosion, soundproof, thermal insulation and gear door protection treatments. The aircraft has an empty weight of 2,097kg, a maximum takeoff weight of 3,354kg, and a maximum payload capacity of 636kg. 726m runway distance is required, and the landing distance is 741m.

With the aim of improving aerodynamics and reducing resistance, the aircraft has 2-foot wings, which are attached to the aileron. Winglets help improve handling at low speeds and high attack angles.

The jet has a tail cone that has been restructured and has additional light at the tail end. It is equipped with a retractable landing gear with electro-hydraulic actuation.

Daher TBM 930 Engine

The TBM 930 is powered by a PT6A-66D turboprop engine, produced by Pratt & Whitney (P & W) Canada. Driven by Hartzell's five-blade constant speed propeller, the engine has a thermodynamic power of 1.825hp, and a nominal power of 850shp. The capacity of fuel that can be used from the aircraft is 1,100l.

The TBM 930 can travel at a speed of 467 km / h in remote settings, while the maximum cruising speed is 611 km / h at an altitude of 28,000 feet. The maximum distance of the aircraft is 3,304 km at cruising speeds of 467 km / h This aircraft has a certified ceiling of 9,449 m, which can rise in 18 minutes and 45 seconds.

Daher TBM 930 cockpit

Daher TBM 930 Cockpit and Avionics

The TBM 930 cockpit features a reconfigured Garmin G3000 touch screen glass, and has enhanced interior decoration, along with the new bespoke e-co-pilot safety system.

Avionics TBM 930 aircraft include dual flight controls, control wheels with seven integrated functions, autopilot, electric pitch trim and steering trim, center console including single lever power control, adjustable steering pedal, landing gear handle, two-wheel brake and parking brake . Automatic environment and pressure control systems, alternative static source control, and alternative ram air source control are also provided.

Daher TBM 930 interior

Daher TBM 930 Cabin and Interior

The spacious cabin of the TBM 930 can accommodate six passengers. The cabin dimensions are 4.05m long, 1.21m wide, 1.22m high, and 3.5m3 volume. The interior of the cabin includes easily stretched seats with leather armrests. And also along with storage cabinet configuration, and luggage space.

Daher TBM 930 Price

The latest TBM 930 price is US $ 4.3 Million.

Monday, 22 July 2019

Daher TBM 900 Specs, Interior, Cockpit, and Price

01:00
Daher TBM 900 Specs, Interior, Cockpit, and Price – TBM 900 is a single turboprop engine business jet produced by Daher company in Tarbes, France. The aircraft was first launched in March 2014. The TBM 900 was modified based on the design of its predecessor, the TBM 850. This business aircraft presents the latest aerodynamic profile of the fuselage to improve aircraft performance. In addition, updates are also made to electrical systems to provide alternative electrical input in emergency.

Daher TBM 900

Daher TBM 900 Specs

The Daher TBM 900 airframe is made of aluminum alloy, high strength steel and advanced composite materials, which maximize durability and structural strength while minimizing overall aircraft weight.

New carbon fiber winglets, vertical fin strakes and new tail cones are added to optimize aircraft aerodynamic profiles. Wing spars, track flaps, and windshield frames are made of solid aluminum rods.

The Daher TBM 900 propulsion system is equipped with five new blade propellers that are integrated with the aircraft's new inlet, which results in more thrust and increased take-off, climbing and cruising distances. The inner gear door reduces obstacles and helps deal with low speed and high angle attacks in a better way.

The sound level at takeoff is 76.4 decibels, of which three decibels are quieter than the previous TBM aircraft version. Therefore, aircraft meet the latest European and US noise standards in the quiet category.

It is also equipped with a fully modified electrical system with a 300A starter generator, as well as an additional 100A stand-by generator to provide alternative electrical input in an emergency.

Daher TBM 900 Engine

TBM 900 is powered by a single PT6A turboprop engine produced by Pratt & Whitney Canada. The engine has a thermodynamic rating of 1,825 hp with an average output of 850 hp. It was designed to provide low efficiency and operating costs, and easy maintenance. This jet has the highest cruise speed of 467km / h at 28,000 feet above sea level, a range of 1,730nm, and a climbing rate of 31,000 feet.

Daher TBM 900 interior

Daher TBM 900 Cabin and Interior

The TBM 900 cabin provides comfortable seating for six passengers, with interior leather seats with a top grain leather surface, adjustable backrest and folding armrests. A large folding executive desk is placed in the center, and passengers can enter the cabin through large electric doors, stairs and roads.

The TBM 900 cabin is 14.96 feet long and 4 feet tall. The maximum volume is 13ft³ (0.4m³), the baggage area is 19.2in (0.487m), and the height is 35.8in (0.910m).

Inside are seven rectangular windows with a pull down sun shade and an automatic dual zone environmental control system. The lighting system is well regulated with dome lights, luggage compartment lights and stair lighting access. Individual reading lights are also provided on all seats.

The TBM 900 cabin is equipped with entertainment facilities including iPods, XM satellite music, and radio, while passengers can keep their personal electronics fully charged with 14 / 24V and USB power jacks. Storage cabinets are provided optionally.

Daher TBM 900 cockpit

Daher TBM 900 Cockpit and Avionics

The TBM 900 glass cockpit is equipped with a Garmin G1000 avionics suite can be found on the plane. The cockpit has extensive legroom for the pilot and a revised central cockpit that combines a single control throttle operation. It also has the latest flight instrumentation systems, including a new ergonomic yoke with remote command buttons, a single lever control, a new landing gear control system, and a redesigned control panel.

The TBM 900 avionics suite has a high resolution 10.4in and 15in glass screen, which displays main flight data, navigation, communication, terrain, traffic, weather and machinery. It also has other advanced avionics equipment such as two digital audio controllers, two solid state position-reference systems, two digital air data computers, and two WAAS and GPS receivers.

Also includes two tri-axial magnetometers, an integrated digital automatic flight control system, color weather radar, field avoidance system, and in-flight traffic avoidance system (TCAS). In addition, it comes with a Garmin GDL69A, GSR 56, and optional datalink receiver that provides XM WX satellite weather to the navigation system.

Daher TBM 900 Price and Orders

The latest TBM 900 price is US $ 3.9 Million. Daher delivered the first three production versions of the TBM 900 in March 2014. The launch customer was Larry Glazer, Chair of the Owner Association and Pilot TBM (TBMOPA).

Daher handed over the TBM 900 aircraft to Badenwings in May 2014, while Jean-Jacques Bely, founder and CEO of Singapore's Franco-Asian Enterprises (FAE), accepted the new aircraft in June 2014.

Saturday, 20 July 2019

Stratos 714 Specs, Interior, Cockpit, and Price

01:00
Stratos 714 Specs, Interior, Cockpit, and Price – Stratos 714 is a single-engine lightweight business jet designed and manufactured by Stratos Aircraft based in the United States. The jet can fly from Miami to Seattle in seven hours using a single refueling stop. The wind tunnel test at Stratos 714 was conducted at the University of Washington Kirsten Wind Tunnel in August 2011. The business jet was first launched at the European Business Aviation Convention and Exhibition (EBACE) held in May 2008. The first flight of the Stratos 714 jet was completed in November 2016.

Stratos 714 business jet

Stratos 714 Specs

The slim and aerodynamic design of Stratos 714 achieves more fuel efficiency compared to conventional business jets. The fuselage is built with sophisticated carbon fiber composite material to increase the strength-to-weight ratio, avoid corrosion, and optimize obstacles during flight.

This business jet has been designed to maintain extensive laminar flow in cruising speeds. It can operate day and night from unprepared runways and grass runways.

The Stratos 714 landing gear is a tricycle undercarriage that can be pulled from being hydraulically driven by a gear switch. It is equipped with one wheel nose wheels and two main wheel legs. The main gear shortens to the wing while the nose wheel turns into the front wheel after takeoff.

Stratos 714 specs

Stratos 714 Engine

The Stratos 714 is powered by a single Williams International FJ44-3AP two-shaft turbofan engine with a thrust of 13.5kN. The engine is installed in the rear of the cabin to produce a high thrust-to-weight ratio and minimize fuel consumption and operating costs. The engine has a length of 1.58m and a diameter of 0.58m. The dry weight is 239kg. The time between repairs (TBO) is 4,000 hours.

The FADEC compatible engine is equipped with a one-stage fan with an integral single stage low pressure axial compressor, annular burner and one-stage high pressure, and two-stage low pressure turbine.

Stratos 714 can fly at a maximum speed of 769km / hour. The kiosk speed is 117 km / hour. The maximum range and service ceiling of the aircraft are 2,779 km and 12,500 m respectively. The take-off distance is 600m and the landing distance is 683m.

Stratos 714 interior

Stratos 714 Cabin and Interior

Stratos 714 has a low wing monoplane design. The pressurized Stratos 714 cabin measures 2.9 m in length, 1.43 m in width and 1.46 m in height. This accommodates two passengers providing 0.76m of leg space. The cabin provides in-flight access to 160 cubic feet of volume available in two external baggage compartments.

Cabin is available in six different configurations, which include four standard seating, club seating, five seats, training, toilets and cargo. The five-seat model will feature the fifth seat behind the co-pilot's seat.

The Stratos 714 cabin is equipped with an air conditioning system, ice protection system, interior LED lights, reading lights for the rear seats, plus front and rear luggage compartment lights. 0.6 m and 1.2 m wide cabin doors are available on the left side for passenger entry and exit. It is equipped with an emergency exit on the right side of the fuselage.

Stratos 714 cockpit

Stratos 714 Cockpit and Avionics

The glass enclosure of the Stratos 714 aircraft is integrated with two main flight displays and a single multifunction display to show data related to navigation, instrumentation of flight, fuel and engines to the flight crew.

Stratos 714 cockpit is equipped with side-stick flight controls, removable winglets, removable horizontal stabilizer, fuel system, electrical system, environmental control system and fuel management system. This business jet was built according to FAR 23 rules for visual flight rules (VFR), international flight rules (IFR) and reduced minimum vertical separation (RVSM).

The avionics suite installed at Stratos 714 includes attitude and canopy reference systems, colored weather radars, wide area augmentation systems, flight data recorders, field awareness and warning systems, S mode transponders, air data computers, dual VHF radios, voice over recorders, autopilot and emergency locator transmitters.

Stratos 714 Price

The latest Stratos 714 price is around US $ 3-3.5 Million.

Friday, 19 July 2019

Piper M600 Specs, Interior, Cockpit, and Price

01:00
Piper M600 Specs, Interior, Cockpit, and Price – Piper M600 is a new M-Class line aircraft, a single turboprop engine manufactured by Piper Aircraft, United States. The aircraft was introduced in Vero Beach, Florida in April 2015. This enhanced aircraft is the first single turboprop engine equipped with G3000 avionics integrated with the glass flight deck.

Piper M600 received a type certification from the Federal Aviation Administration (FAA) in June 2016. The Directorate General of Mexican Civil Aviation (DGAC) also provided type validation certificates for aircraft. in September 2016.

Piper M600

Piper M600 Specs

Piper M600 aircraft was developed and upgraded from the M500 aircraft. It features a new wing design, more power than the engine, and an interior that is enhanced with the Garmin G3000 avionics. The exterior dimensions of the aircraft include a length of 9.1 m (29 feet 10 inches), a height of 3.5 meters (11 feet 4 inches) and a wingspan of 13.2 meters (43 feet 2 inches).

Safety equipment installed on the aircraft include electronic stability protection (ESP), low speed protection (USP), and main warnings, main warnings, gear position and gear warning. Other security features include go-around clutches, expanded engagement envelopes, level mode, autopilot, auto-engagement, hypoxic recognition, and emergency drop mode.

Piper M600 has a maximum takeoff weight of 2,722 kg (6,000 lb) and a useful standard load carrying capacity of up to 1,089kg (2,400 lb). The maximum ramp weight is 2,744kg (6,050lb) and the standard weight is 1,656kg (3,650lb).

Piper M600 Engine

Piper M600 is powered by the Pratt and Whitney Canada PT6A-42A engines, which produce 600 hp of power. The engine is driven by the four-blade Hartzell constant speed propeller, which is 208cm (82in) in diameter. The aircraft fuel capacity is 984l (260gal) and the time between overhauls (TBO) is 3,600 hours. The aircraft requires 803 m (2,635 ft) take-off distance and 810 m (2,659 ft) landing distance above the 50-foot hurdle.

This aircraft has a cruising speed of 507 km / h (274 kt) and Vmo speed of 463 km / h. The maximum distance of the aircraft is 1.484nm (2,748 km) at 184kt and the maximum height agreed to is 9,144 m (30,000 feet).

Piper M600 cockpit

Piper M600 Cockpit and Avionics

Piper M600 is equipped with a Garmin G3000 avionics suite that integrates with a glass flight deck that includes enhanced autopilot and 12.1 dual synthetic vision in a primary flight display (PFD), single 12.1in multi-function display (MFD), and a GTC touch screen cockpit management unit 570 dual screen. Avionics also include dual GIA 63W NAV / COM / GPS, GEA 71 engine and fuselage interfaces, and GWX 70 digital weather radar.

The aircraft is equipped with an improved GFC 700 automatic flight control system, which offers flight automation enhanced by multiple AHRS based systems. The SurfaceWatch feature provides pilots with aural and visual warnings to help maintain situational awareness and avoid potential runway attacks or visits.

Piper M600 can also be equipped with an optional GTS 855 traffic advisory system, which offers a traffic collision warning system (TCAS) I, and Garmin GSR 56 Iridium Satellite Transceiver Datalink Global Satellite for additional connectivity.

Enhanced avionics features on the aircraft include the GMC 710 AP controller, dual 44 GMU magnetometer units, and dual GRS 77 AHRS computers. Further avionics include GMA 36 digital audio panels, dual 74 GDC air data computers, GTX 33 ES Mode transponders, GAE 43 altitude encoders, Garmin FliteCharts, Garmin SafeTaxi, and EFD1000 Aspen flight flight instruments.

Piper M600 interior

Piper M600 Cabin and Interior

Piper M600 cabin can accommodate 6 passengers. The interior of the aircraft can be configured with premium leather seats from Calais, Sedona or Florence. It also features an electroluminescent placard, chrome, wooden accents and four USB charging ports.

Piper M600 Price and Orders

The latest Piper M60 price is US $ 2.9 Million. The first aircraft was sent to Jerry and Jack Wardlaw in July 2016.

Wednesday, 17 July 2019

Hondajet HA-420 Specs, Interior, Cockpit, and Price

01:00
Hondajet HA-420 Specs, Interior, Cockpit, and Price – Hondajet HA-420 is a twin-engine business jet designed and manufactured by the Honda Aircraft Company (HAC) based in the US to operate on domestic and international air routes. This is the first public flight aircraft built by HAC. The first production aircraft made its first flight with a GE Honda HF120 engine in June 2014.

Hondajet HA-420 business jet received a type certification from the US Federal Aviation Administration (FAA) in December 2015. The aircraft was given type certification by the Mexican Civil Aviation Safety Authority in March 2016. The European Aviation Safety Agency (EASA) certified the Hondajet HA-420 Business Jet in May 2016.

Hondajet HA-420

Hondajet HA-420 Specs

Hondajet HA-420 jet body consists of a lightweight carbon composite material or honeycomb sandwich to reduce the overall weight of the aircraft. The wings are built with single reinforced aluminum sheets, which provide a smoother surface compared to conventional business jet wings.

The slim and aerodynamic design of the Hondajet HA-420 is claimed to achieve fuel efficiency 35% higher than conventional business jets. Configuring a podded over-the-wing engine from the aircraft reduces obstacles in flight and maximizes cabin space.

Hondajet HA-420 engine

Hondajet HA-420 Engine

Hondajet HA-420 is powered by two GE Honda HF120 turbofan engines, each worth 8.04kN. This machine was designed and developed by General Electric Honda Aero Engine at their factory in Burlington, North Carolina.

The GE Honda HF120 engine is equipped with a dual-controlled double-authority digital engine control system, single fan, two-stage compressor and two-stage turbine. The modern integration of reverse flow combustor and fuel nozzles in the engine reduces fuel consumption, noise detected on the ground, and harmful emissions, such as Nox, CO and HC.

The engine has a length of 1.1 m and a diameter of 0.53 m. The dry weight is 181kg. The time between repairing the engine is 5,000 hours.

Hondajet HA-420 business jet can rise at a speed of 20.27 m / s. The maximum speed is 778km / hour. The aircraft service range and ceiling are 2,593 km and 13,107 m. The take-off distance is 950m, while the landing distance is 762m.

Hondajet HA-420 interior

Hondajet HA-420 Cabin and Interior

The spacious cabin of the Hondajet HA-420 has a length of 5.43m, a width of 1.52m and a height of 1.47m. The total volume of external luggage is 1.87m³. The cabin can accommodate five passengers and offers extensive legroom. It features executive seating for four passengers in a classic club configuration and additional single seat cots.

It is equipped with a flexible leather club-style chair, a fashionable glass stand, a tray table, electrochromatic window curtains, and a rear private toilet.

Hondajet HA-420 cockpit

Hondajet HA-420 Cockpit and Avionics

The Hondajet HA-420 cockpit is integrated with the Garmin G3000 avionics system. The digital cockpit is equipped with two 14.1 primary LCD screens that are compatible with LCD screens and a central multifunction screen, two user-friendly infrared touch screen control panels, autopilot functions, and anti-icing equipment. Garmin SVT (synthetic vision technology) offers runway display, terrain, traffic, and virtual obstacles.

Hondajet HA-420 Price

The latest Hondajet HA-420 price is US $ 4.9 Million. Delivery of Hondajet HA-420 began in December 2015 and aircraft were delivered to customers in the US, Mexico and Europe.

Monday, 15 July 2019

Spectrum S-40 Freedom Specs, Interior, Cockpit, and Price

01:00
Spectrum S-40 Freedom Specs, Interior, Cockpit, and Price – Spectrum S-40 Freedom is a twin-engine medium-scale business jet designed and built by Spectrum Aeronautical based in the United States. This business jet was developed based on the S-33 Independence business jet. Spectrum Aeronautical gave a contract to GE Honda Aero Engine in October 2006 to supply Honda HF-120 engines for integration into S-40 jets. The first S-40 aircraft was produced in June 2009. This will be the second aircraft in the series to be developed by Spectrum Aeronautical.

Spectrum S-40 Freedom

Spectrum S-40 Freedom Specs

Spectrum S-40 Freedom has a sleek and aerodynamic airframe design, to achieve more fuel efficiency compared to conventional business jets. The design of the three-wheeled undercarriage allows planes to take off from and land on muddy runways and short runways.

The aircraft body will be built with carbon fiber carbon fiber technology to improve durability, avoid corrosion, and optimize obstacles in flight. The unique combination of carbon fiber and epoxy will reduce the empty weight of the S-40 Freedom jet by 40%, compared to conventional aircraft made of aluminum.

Spectrum S-40 Freedom Engine

Spectrum S-40 Freedom will be powered by two HF120 turbofan engines, each producing 8.04 kN. The engine was designed and developed by General Electric Honda Aero Engine at their factory in Burlington, North Carolina. The length and diameter of the machines are 1.1 m and 0.53 m, respectively. The dry weight is 181kg. The time between repairing the engine is 5,000 hours.

The HF-120 turbofan engine features a dual-controlled ultra compact FADEC system, one-stage fan, two-stage compressor and two-stage turbine. It is equipped with advanced backflow burners and fuel nozzles to minimize fuel consumption, noise detected in the ground, and harmful emissions, such as nitrogen oxides (NOx), carbon monoxide (CO) and hydrocarbons (HC).

The S-40 Freedom can go up at a speed of 15.2m / s. The maximum speed of the S-40 Freedom is 815km / hour. The maximum range and service ceiling of the aircraft will be 4,170 km and 13.7 km, respectively. The take-off distance will be 914m, while the landing distance will be 822m.

Spectrum S-40 Freedom interior

Spectrum S-40 Freedom Cabin and Interior

Spectrum S-40 Freedom cabin has 6.4 m length, 1.8 m wide and 1.8 m high. The cabin can accommodate seven to nine passengers with extensive legroom. This will provide flight access to 80 cubic feet of volume available in the external baggage compartment.

The cabin will combine refresher centers, electronically shaded windows, private rear toilets, plug-in stations for electronic equipment, air conditioning systems, in-flight entertainment systems and 15 cubic feet of interior storage cabinets.

Spectrum S-40 Freedom cockpit

Spectrum S-40 Freedom Cockpit and Avionics

Spectrum S-40 Freedom digital cockpit will feature four high-resolution screens, including two 15.6-inch main flight screens and two 10.4-inch multifunction screens to showcase navigation data, flight instrumentation, fuel and machine-related to the flight crew.

Spectrum S-40 Freedom uses Primus Apex Honeywell Aerospace avionics suite. The avionics suite will include the AH-1000 attitude reference system, KXP-2290 S transponder mode, KGS-200 global positioning system receiver, KMA-29 audio panel, AZ-200 air data module, KTR-2280 and KMC-2230 digital multimode radio cursor control device.

Other avionics will include automatic flight control systems, field collisions and avoidance systems, field awareness alert systems, crew warning system and engine indications, aural warning computers, flight management systems, wide area augmentation systems, flight data recorders, cockpit voice recorders, situation seekers emergency transmitter, automatic dependent surveillance system, XM satellite weather radar and central aircraft maintenance system.

Spectrum S-40 Freedom Price and Orders

The latest Spectrum S-40 Freedom price is US $ 6.8 Million. Jet Pool ordered the S-40 Freedom jet fleet in February 2008. Other S-40 orders were received from Starfish Aviation in September 2008.

Saturday, 13 July 2019

Eclipse 500 Specs, Interior, Cockpit, and Price

17:06
Eclipse 500 Specs, Interior, Cockpit, and Price – Eclipse 500 is a very light business jet produced by Eclipse Aviation at its production facility in Albuquerque in New Mexico. Eclipse 500 is marketed for pilot / owner services, airplane charters and air taxis, as economical and luxurious six-seat twin turbofan jets.

Eclipse 500 made its maiden flight in August 2002, with the Williams EJ22 engine. In November 2002, Eclipse Aviation decided to replace the engine and the aircraft was now equipped with the Pratt & Whitney Canada PW615F engine. The first flight with the new engine was in December 2004. The aircraft received FAA production certification in April 2007. The European Aviation Safety Agency (EASA) certification was received in November 2008.

Eclipse 500

Eclipse 500 Specs

Eclipse 500 is made of conventional aluminum construction with traditional components (spars, stringers, rib frames and clips). All critical connections, such as leather joints, bulkheads and spar joints to the fuselage are bound mechanically.

The aircraft is equipped with horizontal and horizontal de-icing wing boots. The windshield and air data probe are equipped with an electric powered de-icing system.

UK-based Hampson Industries supplies stabilizers, steering and elevator empennage, vertical and horizontal. Saint Gobain supplies radome and Steico Industries all system tube assemblies.

The Macaer Group supplies trailing link landing gear. The single wheeled nose wheel pulls forward and the main unit pulls in. The landing gear is equipped with Parker Hannifin lightweight wheels and a multi-disc brake system and Michelin radial main tires.

Eclipse 500 can operate from runways, grass or land. Run-off is 700m. The kiosk speed of 124km / h (67kt) provides an easy and safe landing.

Eclipse 500 Engine

Eclipse 500 is powered by two Pratt & Whitney Canada PW615F medium turbofan engines, with a take-off rating of 4.00kN. The engine is equipped with digital engine control full authority of Hispano-Suiza SA (FADEC) including engine start, automatic restart in flight, over temperature, and more speed protection. Engine inlet holes are equipped with bleed engine air ice protection.

The PW615F twin turbofan engine provides a maximum height of 12,497 m (41,000 feet) which avoids the most severe weather systems. The aircraft provides a cruising speed of 685 km / h (370kt) and ranges from 2,408 km (1,496 miles) to four passengers.

The aircraft is equipped with a fuel tank that can hold 871l (699kg) of fuel. Argo-Tech Corporation supplies integrated fuel systems.

The unique thing about Eclipse 500 is the PhostrEx engine fire suppression system, which is not based on Halon and does not have ozone depletion potential. PhostrEx has been certified by the FAA and meets the Montreal Protocol standards, an agreement to protect the ozone layer.

Eclipse 500 interior

Eclipse 500 Interior and Cabin

The interior of Eclipse 500 cabin is equipped with four club-style leather seats, LED lights, wood trim and a desk and electrical outlet. The aircraft is equipped with a Dukes Inc interface digital cabin pressure control system and a Seamech air conditioning module containing steam coolers and heat exchangers.

Eclipse 500 cockpit

Eclipse 500 Cockpit and Avionics

Eclipse 500 is equipped with an all-glass cockpit with two main flight displays and a multifunctional screen, which provides system control and clearly shows the flight, engine, and system performance data parameters.

The multifunctional display unit provides controls for fuel, electricity, machinery, environmental control, ice cleaning, lighting and pressure systems. It is equipped with embedded backup instrumentation and a primary flight display and the multifunction screen has a reversal mode to allow transfer of information to other displays.

Eclipse 500 is integrated with the Avio NG avionic suite which has two main flight displays with a resolution of 768 × 1,024 and one 1,440 × 900 multi-function display supplied by IS & S. The new screen has a higher resolution and average time between failures (MTBF).

Avio NG owns Chelton Flight Systems RTCA / DO-229C which are integrated with flight management systems (FMS), which allow the creation of special waypoints, addition or removal of waypoints from active routes and specifications of parallel lane operations. This system has lateral lateral capability based on GPS and vertical navigation (VNAV).

Honeywell communication / navigation devices include the Primus Apex KTR 2280 multi-mode digital radio (MMDR), with a digital VHF navigation receiver (omni-directional VHF ranger, localiser and glideslope), and an optional automatic direction finder. Each radio has one transmitter and six receivers, which are capable of operating 8.33 / 25kHz channel distances and simultaneous monitoring of two VHF communication frequencies. The VHF communication system is displayed and controlled in the main flight display. Honeywell also supplies the optional KGP 560 terrain awareness system (TAWS).

Eclipse 500 navigation system has a Garmin GTX 33 and GTX 33D dual-mode transponders. The FreeFlight system is a double-area-wide augmentation system that is capable of a global positioning system certified for rules on the way in transit and in approach. EDO Corporation supplies antenna communications and aircraft navigation.

The Meggitt Avionics flight control and guidance system consists of three axis autopilot, dual Crossbow Technology AHRS500, heading and attitude reference system (AHRS) and automatic throttle. Curtiss-Wright controls, Novatronics throttle quadrant include dual engine throttle levers and auto-throttle motor assemblies for flap grip, speed brakes and steering trim functions.

The air data system, supplied by Harco Laboratories, Bradford, Connecticut, consists of dual air data computers with minimum vertical separation capabilities (RVSM), dual static ports, double outdoor air temperatures and pitot heat probes and static ports of multiple environmental control systems.

Eclipse 500 Price and Orders

The latest Eclipse 500 price is US $ 2 Million. DayJet was the first air taxi operator to receive the aircraft, three were sent in April 2007. Dayjet received 12 aircraft in September 2007 and in October 2007 launched operations using Eclipse 500 aircraft.

Eclipse Aviation has received Eclipse 500 orders for more than 2,600 aircraft, including 239 (plus 70 options) for DayJet, 25 (plus 25 options) for JetSet Air UK, 15 (plus 15 options) for Linear Air USA and 120 (plus 60 options) ) for Aviation Europe ETIRC. In July 2008, more than 200 aircraft were shipped and accumulated more than 20,000 flight hours.