| Airbus ACJ | ||
An ACJ corporate jetliner operated by Aero Services of France. |
The Airbus Corporate Jetliner is based on the airframe of the A319, a twin-engine, single-aisle, medium-range airliner. |
The ACJ's spacious 24m-long cabin has a floor area of nearly 80m². |
Aero Services ACJ on the ground. |
Aero Services ACJ boarding. |
The ACJ can be operated to allow private or commercial flight – the interior can be easily converted for commercial passenger service. |
Interior view of one ACJ cabin arrangement. |
The cabin layout can be altered according to the needs of the individual client or corporate customer. |
A chair that converts easily to a bed. |
Alternative cabin arrangement. |
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| Beechcraft Baron G58 Advanced Business Aircraft | ||
Baron G58 taking off from the HBC service centre. |
Beechcraft Baron G58 performing its maiden flight. |
Baron G58 is equipped with the Garmin G1000 avionics suite. |
| Boeing Business Jet (BBJ) | ||
The Boeing long range business jet, the BBJ. |
The BBJ is a member of the successful 737 family of airliners. |
BBJ taking off, showing the optional winglets which provide increased range through a reduction in air turbulence. |
The BBJ glass cockpit is based on that of the Boeing 777. |
The BBJ coming in to land. |
The BBJ's spacious cabin can be customised to meet individual or business requirements. |
The BBJ's interior configuration is chosen by the customer in consultation with interior designers and completion centres. |
Interior designers can include an executive office, conference rooms, private offices and bedrooms in the BBJ design. |
Personal environments can be created within the Boeing business jet, for example with a living room, dining room, two bedrooms and two bathrooms. |
| Boeing Business Jet (BBJ) Convertible | ||
Boeing has launched the latest in its business jets range, the BBJ convertible. |
The jet can be turned from an all-passenger to all-cargo configuration in a matter of hours. |
The BBJ convertible is lightweight with lower emissions, yet with capacity for more than 16.6t of cargo or 149 passengers. |
BBJs are designed for corporate or VIP applications. |
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| Boeing Business Jet 2 (BBJ2) | ||
The Boeing business jet 2 (BBJ2) is a development of the BBJ family, with increased cabin volume and cargo volume. |
With BBJ 2, Boeing has increased the range of its business jet to over 10,000km. |
Aviation Partners Boeing winglets and CFM56-7 engines (offering 27,000lb of thrust) are standard equipment. |
The Boeing business jet flight deck includes leading-edge technology, including a head-up guidance system, integrated dual global positioning system (GPS), and what the maker claims is the most advanced flight management system in the world. |
The BBJ2 includes a dining room and executive offices. |
The interior design, completed by a number of US-based companies, incorporates divans for maximum passenger comfort. |
The BBJ2 can also incorporate an optional AJAC space-saving shower that provides an endless supply of purified, re-circulated hot water. |
Cutaway of the new Boeing business jet. |
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| Boeing Business Jet 3 (BBJ3) | ||
BBJ3, the newest member of the Boeing Business Jet flies at 41,000 feet altitude. |
The BBJ3 fuselage is an aluminium structure, which is manufactured and assembled by Spirit AeroSystems at Wichita, Kansas. |
Joining of the BBJ3 fuselage at workshop. |
Winglets construction at Renton facility. |
BBJ3 on its first flight. The aircraft was unveiled in November 2005 and officially launched in October 2006. |
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| Bombardier Challenger 300 | ||
The Bombardier Challenger 300 (formerly called the Continental) business jet entered service with Flexjet in January 2004. |
Interior of Bombardier's Challenger 300 business jet for executive and corporate business travel. |
The Bombardier Challenger 300 flight deck. Rockwell Collins was given the task of supplying the Pro Line 21 integrated avionics system. |
The third Bombardier Challenger 300 business jet successfully completed its first flight on 6 December 2001, shown here taking off from Wichita's Mid-Continent airport. |
The aircraft can carry up to eight passengers coast-to-coast across America. |
Bombadier's comprehensive flight test programme involved five aircraft. |
The aircraft has two Honeywell AS907 turbofan engines each providing 35.81kN (8,050lbs) thrust. |
The Challenger 300 requires a take-off airfield length of less than 5,000ft. |
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| Bombardier Challenger 604 | ||
The Challenger 605, the successor to the 604, first flew in January 2006. |
The cockpit of the Challenger 604 is fitted with Rockwell Collins Pro Line 4 integrated avionics suite. |
The Challenger 604 intercontinental business jet. |
The cabin can accommodate up to nine passengers in business-class seats or up to 19 passengers in higher-density seating. |
The aircraft is powered by two General Electric CF34-3B turbofan engines each providing 38.84kN (8,729lb) thrust at take-off. |
The Challenger 604 provides a range of 7,551km (4,077nm) and a long-range cruise speed of 787km/h. |
| Bombardier Global 5000 | ||
The first Bombardier Global 5000 business jet (serial number 9127) successfully completed its first flight on 7 March 2003. |
The first Global 5000 business jet takes off from Bombardier's Tucson completion centre, en route to its public debut in White Plains, New York, on 11 June 2003. |
The Global 5000 super-large business jet landing at Orlando Executive Airport for its debut at the National Business Aviation Association (NBAA) Convention in October 2003. |
The Global 5000 is capable of flying non-stop from continental Europe to central North America at Mach 0.85 with eight passengers. |
The Global 5000 has a take-off field length of 1,525m, enabling it to operate from smaller airfields. |
The Global 5000 is a development of the proven Global Express business jet. |
The Global 5000 has a spacious maximum cabin width of 2.49m (8.17ft). |
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| Bombardier Global Express | ||
The Bombardier Global Express ultra long-range, high-speed business jet. |
The Global Express has a range of 11,130km with eight passengers and four crew. |
The Global Express cockpit features a six-tube EFIS/EICAS (electronic flight information system / engine instrument and crew advisory system) with 8in×7in cathode ray tube displays for processing, fault warning, flight management and a fail-operational automatic flight control system. |
The first Bombardier Global Express featuring a customised interior made its first appearance at the National Business Aviation Association (NBAA), in Dallas. The interior was completed at the de Havilland facility in Toronto. |
A Global Express business jet landed at Plettenberg Bay, South Africa, landing in less than 3,000ft after taking off from the airfield in under 2,000ft from a standing start. |
The first flight of a Global Express jet configured as an ASTOR platform took place in August 2001. |
| Bombardier Learjet 31A | ||
The Learjet 31A light business jet entered service in 1994. |
The Learjet 31A can carry seven passengers at a cruise speed of 845km/h. |
The Learjet 31A cockpit is fitted with a Honeywell digital avionics suite. |
The Learjet 31A |
The cabin of the Learjet 31A. |
Four Learjet 31A light jets on the ground. |
Learjet 31A, operated by Düsseldorf-based Air Traffic. |
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| Bombardier Learjet 45 | ||
The Bombadier Aerospace Learjet 45 nine-seat super-light business jet. |
The Learjet 45. Over 2000 Learjets have been built and are in operation as corporate jets worldwide. |
The passenger cabin seats up to nine passengers in double-club seating. |
The Learjet 45 business jet aircraft, shown here flying over Sydney Harbour in Australia, has been designed to provide midsize comfort at a light-jet price. |
The Learjet 45 is equipped with advanced flight software and architecture to minimise pilot and maintenance workloads. |
The Learjet 45 taking off. |
The long-range cruise speed is 778km/h and the maximum operating altitude is 51,000ft (15,545m). |
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| Century Jet | ||
Century Aerospace hopes that the Century Jet will be considerably cheaper than its rivals. |
The Century Jet was originally intended to have one engine but now has two. |
The Century Jet has a six-seat interior. |
The new Century Jet 100 will be powered by twin Williams International FJ33-1 engines. |
The Century Jet has a range of 1,500 nautical miles. |
The Century Jet has a CA-100 carbon-composite fuselage, designed with the help of SGL Carbon Composites. |
The airplane boasts a cruising speed of 370kts. |
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| Cessna Citation Bravo Light Business Jet | ||
The Cessna Citation Bravo light business jet entered service in 1997. |
The Citation Bravo flies to an altitude of 13,216m (45,000ft) and carries up to seven passengers. |
The standard interior configuration with four passengers in club seats facing each other plus three additional club seats. |
The range with full fuel and a maximum take-off weight is 3,232km. |
The Bravo has a cruise speed of up to 403kt true airspeed or 745km/hr. |
The Citation Bravo is powered by two Pratt & Whitney PW530A engines. Each engine delivers 12.84kN (2,287lb) of thrust. |
| Cessna Citation CJ3 Business Jet | ||
The Citation CJ3 at its first landing at Mid-Continent Airport, Wichita, Kansas. |
The Citation CJ3 first flight, in April 2003. |
The Citation CJ3 during first engine run up and taxi. |
The Citation CJ3 cabin accommodates six club seats in a centre aisle configuration. |
The Citation CJ3 flight deck is fitted with the Rockwell Collins ProLine 21 avionics system. |
The CJ3 has a more powerful engine, more cabin room, about 10% higher take-off weight and 12% higher cruise speed than the Citation CJ2. |
With two pilots, full fuel and four passengers with baggage, the CJ3 has a maximum range of 2,926km (1,580nm). |
The CJ3 aircraft is powered by two Williams FJ44-3A engines, each rated at 12.37kN. |
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| Cessna Citation CJ4 and Encore Plus | ||
The Citation CJ4 business jet first took flight as a production model on 19 August 2008. |
The CJ4 features two of the new Williams International FJ44-4A electronically controlled full authority digital engine control (FADEC) engines. |
The CJ4 will be certified for up to eight passengers and two crew members. |
The Encore plus is typically configured for seven passengers and up to two crew members. |
The Encore plus is powered by two Pratt & Whitney PW535B engines, generating 15.12kN of thrust each. |
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| Cessna Citation Mustang Light Business Jet | ||
The first flight of the Cessna Citation Mustang took place in April 2005 and first retail deliveries were in April 2007. |
The Citation Mustang is a single-pilot entry-level business jet and is the smallest of the Cessna Citation family. |
The Mustang aircraft has an all-glass cockpit, with a fully integrated Garmin International G1000 avionics suite. |
The Mustang is powered by two Pratt & Whitney Canada PW615F engines, each rated at 6.49kN (1,460lbs) thrust and fitted with FADEC. |
The Citation Mustang cabin can seat four passengers in club configuration. |
A Citation Mustang ground engine run. |
| Cessna Citation X and Columbus | ||
The Citation X is currently the fastest civilian aircraft, with an ability to cruise just under the sound barrier at Mach .92. |
In its typical configuration the Citation X carries up to eight passengers and two pilots. |
The Cessna Columbus is still a work in progress for Cessna and will be the largest Citation to date. |
The passenger cabin is large on the new Columbus, measuring 8.31m long, it is still likely to carry up to eight passengers. |
The company expects that the Columbus will be the only aircraft in its class capable of flying 7,408km non-stop. |
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| Cessna Citation XLS Plus and Citation Sovereign | ||
The Citation XLS plus made its maiden flight in 2007. |
The XLS plus is capable of 815km/h and has a range of over 3,441km. |
In typical configuration the XLS plus can carry nine passengers and two pilots. |
The Cessna Citation Sovereign is a corporate intercontinental aircraft capable of carrying up to 12 passengers and two pilots at speeds of up to 848km/h. |
Cessna says that it has delivered 176 Sovereign aircraft by the end of 2007. |
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| Dassault Falcon 2000/2000EX | ||
The Falcon 2000 entered service in 1995. |
The Falcon 2000EX extended range business jet. |
The Dassault Falcon 2000 widebody business twinjet. |
First flight of the Falcon 2000EX was in October 2001. |
The cockpit of the Falcon 2000. |
The interior of the Falcon 2000EX cabin. |
With more powerful engines and extra fuel capacity, the 2000EX has a range of 7,000km. |
Maximum cruise speed of the Falcon 2000 is 891km/h. |
The Pratt & Whitney PW/3087/C engines on the 2000EX each provide 31.1kN thrust. |
The Falcon 2000 has a range of 5,778km. |
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| Dassault Falcon 50EX | ||
The Falcon 50EX three-engined business jet. |
The Falcon 50EX entered service in 1997. |
The cockpit avionics suite is the Rockwell Collins Pro Line 4. |
A maritime surveillance version, Falcon 50 Surmar, is in service with the French Navy. |
Falcon 50/50EX aircraft are in service with a number of governments for VIP transport. |
The 50EX is powered by three Honeywell TFE731-40 turbofan engines, each providing a thrust of 16.46kN. |
The 50EX can fly eight passengers 5,695km at 955km/h. |
The 50EX requires a runway length of 1,437m for taking off and 668m for landing. |
Over 330 Dassault Falcon 50 and Falcon 50EX business jets are in service. |
| Dassault Falcon 7X – Long-Range Business Jet | ||
The Falcon 7X received FAA and EASA certification in April 2007. |
The fly-by-wire Falcon 7X is the latest member of the Falcon family of aircraft and flies faster, farther and higher than its predecessors. |
The Dassault / Honeywell EASy cockpit reduces pilot workload, allowing the pilot to concentrate on situational awareness and the successful completion of the flight. |
A typical Falcon 7X cabin configuration. The cabin can accommodate up to eight passengers. |
The Falcon 7X is powered by three Pratt & Whitney Canada PW307A engines rated at 28.47kN (6,402lb) thrust. |
The first Falcon 7X test aircraft in ground run trial, February 2005 at Bordeaux Merignac. |
The range of the 7X is 10,556km (5,700nm), allowing for example non-stop flight from Riyadh to New York or from Paris to Tokyo. |
The Falcon 7X was developed entirely in a virtual environment, using Dassault Systemes product life cycle management software suite. |
The Falcon 7X cabin is configured in three lounges and can accommodate up to six fully berthable passenger seats. |
| Dassault Falcon 900C | ||
The Dassault Falcon 900C in flight. |
The interior of the Dassault Falcon 900C cabin, built for relaxed travel. |
The Dassault Falcon 900C is powered by three Honeywell TFE731-5B turbofan engines. |
The interior of the Dassault Falcon 900C business jet is fitted with functional tables for work or pleasure. |
The flight deck of the triengine Dassault Falcon 900C business jet. |
With three engines, the Falcon 900C is capable of extended flights over water. |
The Falcon 900C entered service in 2000. |
Over 200 Falcon 900B/C jets have been delivered. |
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| Dassault Falcon 900EX | ||
The Dassault Falcon 900EX long-range business tri-jet. |
The Falcon 900EX entered service in November 1996. |
Over 100 Falcon 900EX aircraft have been delivered and are operational worldwide. |
The long-range 900EX version has higher powered and more efficient engines compared to the 900. The capacity of the central fuel tank has been increased and a new rear tank added. |
Maximum speed of the 900EX is 890km/h. Range is up to 8,334km. |
The aircraft is powered by two Honeywell TFE731-60 turbofan engines each providing 22.24kN thrust. |
| Diamond D-Jet – | ||
Diamond Aircraft Industries D-Jet five-seat executive very light jet. |
First flight of the D-Jet took place in April 2006 from London International Airport, Ontario. |
The D-Jet's avionics system is based on the Garmin G1000 avionics suite with two 12in primary flight displays (PFDs) and one 15in multi-function display. |
The D-Jet has a maximum cruise speed of 583km/h (315ktas) and a maximum range of 2,500km (1,350nm). |
The cabin provides five seats in a two-plus-three configuration. The rear-seat bench can accommodate three people or two executive-class passengers. |
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| Eclipse 500 Very Light Jet | ||
The first Eclipse 500 very light jet was delivered on 31 December 2006. |
The Eclipse 500 very light jet received provisional US FAA certification in July 2006. |
The Eclipse 500's certification process involved five pre-production flight test aircraft. |
The Eclipse 500 is fitted with an all glass cockpit and the Avio NG avionics suite. |
The Eclipse 500 can operate from paved, grass or dirt runways. |
The Eclipse 500 standard configuration cabin. |
The twin turbofan jet engines provide a maximum altitude of 12,497m (41,000ft) which avoids most severe weather systems. |
The Eclipse 500 has a cruise speed of 694km/h (375 knots) and a 2,371km (1,280-mile) range with four occupants. |
The aircraft is powered by two Pratt & Whitney Canada PW610F medium bypass turbofan engines with FADEC. |
Flight test aircraft N504EA and N503EA, flying in April 2005. |
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| Embraer Legacy | ||
The Legacy super mid-size corporate and executive jet. |
The Legacy can be configured as a Corporate Shuttle with up to 19 seats or Executive Jet with up to 15 seats. |
Legacy is derived from the airframe of the ERJ-135 and ERJ-145 commercial regional jetliners. |
The Legacy Executive has a range of 5,926km and cruise speed of 0.80 Mach. Legacy Corporate has a range of 3,445km. |
The Legacy has a full glass cockpit with advanced digital avionics suite. |
The Legacy is powered by new, rear-mounted high by-pass ratio turbofan engines from Rolls-Royce. |
The wings are fitted with winglets, which provide increased lift and improved efficiency with reduced drag of the tip vortex. |
The T-tail is of aluminium box construction with aluminium leading edges on the tailplane and composite leading edge on the fin. |
The Legacy has integral wing tanks, belly tanks and aft fuel tanks in new extended fairings on the underwing. |
| Embraer Lineage 1000 | ||
First flight of the Lineage 1000 in October 2007. |
Artist's impression of the Lineage 1000 in flight. |
The flight deck of the Lineage 1000 is based on the Honeywell Primus Epic avionics suite. |
Lineage 1000 has an innovative and luxurious cabin layout designed by Priestman Goode of the UK. |
The crew rest area and galley of the Lineage 1000. |
The Embraer Lineage 1000 large, long-range luxury business jet is based on the proven Embraer 190 long-range design. |
| Embraer Phenom 100 | ||
The Embraer Phenom 100 on its maiden flight, 26 July 2007. |
The Phenom 100 taking off on its first flight in Sao Jose dos Campos, Sao Paulo, Brazil. |
Flight deck of the Phenom 100 with Garmin Prodigy avionics suite. |
The Phenom 100 has a range of 1,160nm (2,148km) with four occupants. |
The Phenom 100 cabin lay-out typically seats four passengers. |
The Phenom 100 (below) and Phenom 300 (above) programme was launched in May 2005. |
| Embraer Phenom 300 | ||
The Embraer Phenom 300 light business jet. |
The Embraer Phenom 300 completed its maiden flight in April 2008. |
The Phenom 300 Prodigy flight deck with G1000 all-glass avionics suite supplied by Garmin. |
The Phenom 300 cabin interior designed by BMW Group DesignworksUSA. |
Phenom 300 in the livery of launch customer JetBird of Switzerland. |
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| Grob SPn Light Business Jet | ||
The all-composite SPn combines the speed of a jet aircraft with the flexibility of a turboprop. |
The maiden flight of the Grob Aerospace SPn aircraft took place in July 2006. |
The SPn can use small and unpaved grass or gravel runways close to the passengers' destinations. |
With six passengers and one pilot, the SPn can fly non-stop 3,334km (2,071 miles). |
The SPn can seat eight passengers in a business layout or six passengers in the executive layout (shown). The interior has been designed by the Porsche Design Studio. |
The SPn is powered by two Williams FJ44-3A turbofan engines, fitted with FADEC and rated at 1,270kg thrust. |
The SPn cabin can be rapidly converted for passenger, cargo or air ambulance missions. |
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| Gulfstream G150 Mid-Size Business Jet | ||
The Gulfstream G150 is powered by two Honeywell TFE731-40R turbofan engines, each rated at 19.6kN. |
The G150 cockpit is equipped with a Rockwell Collins Pro Line21 integrated avionics suite. |
The Gulfstream G150 forward interior – the interior design styles are based on the operator’s selection of leathers, upholstery fabrics, wood finishes and floor coverings. |
The G150 has a long-range cruise speed of Mach 0.75 (895km/h), flying four passengers non-stop up to 5,467km (3,397 miles). |
The cabin is wider and higher than the G100 and gives stand up headroom and generous legroom for up to eight passengers. |
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| Gulfstream G200 (Galaxy) | ||
The first Galaxy, now renamed the G200, business jet was delivered in January 2000. |
The G200 business jet has an IFR range of 6,667km (3,600nm). |
The business jet is powered by twin Pratt & Whitney Canada PW 306A engines. |
The G200 can be configured for eight to 18 passengers. |
The business jet's typical cruise speed is Mach 0.82. |
The G200 has a cabin height of 6ft 3in (1.91m) and width of 7ft 2in (2.18m). |
| Gulfstream G450 Long-Range Business Jet | ||
The Gulfstream long-range, large-cabin G450 business jet. |
The G450 aircraft entered service in May 2005 - in the week after entering service the aircraft established a new intercontinental city-pair speed record with a flight of 3,550nm from Chicago to London in seven hours and fifteen minutes. |
The Gulfstream G450 business jet set another new intercontinental city-pair speed record in November 2005, flying 3,290nm from Washington DC to Luton, England, in six hours and twelve minutes, at an average speed of Mach 0.85. |
The aircraft can carry up to 19 passengers and cruise at an altitude up to 13,715m (45,000ft), climbing to 41,000ft in 23 minutes. |
The G450 is powered by two Rolls Royce Tay Mark 611-8C turbofan engines, each providing 61.6kN thrust. |
The PlaneView cockpit of the G450 has four large liquid crystal flight displays, a Gulfstream Enhanced Vision System (EVS) with a Honeywell HUD 2020 head up display and a cursor control device. |
| Gulfstream G650 Jet liner | ||
Honeywell has provided a next-generation flight management system that features path guidance, required time of arrival and display of engine-out drift-down and curved-path transitions. |
The aircraft is expected to receive a joint certification from the Federal Aviation Administration (FAA) and the European Aviation Safety Agency (EASA) in 2011. |
The G650 is a long-range jet and has a larger cabin than other business jets in its class. |
Gulfstream Aerospace Corporation has received orders for 100 jet liners and 400 letters of intent for the G650. |
Bonded skin panels, machined frames and precision assembly were employed in the design and manufacturing processes of G650's fuselage. |
The jet liner is fitted with a Plane View II cockpit, which includes a Triplex Flight Management System. |
| Hawker Beechcraft Hawker 4000 | ||
The Hawker 4000 (previously known as the Hawker Horizon) entered service in December 2004. |
The Hawker Beechcraft Hawker 4000 super mid-size business jet. |
The Hawker 4000 features all-composite fuselage for lightness and strength and swept aluminium wings for speed. |
The Hawker 4000 made its first flight on 11 August 2001. |
The Hawker Beechcraft new family of business jets features the Hawker 4000 (foreground) and the Premier I (background). |
The cabin can be configured for eight to 12 passengers. |
The aircraft is powered by two PW308A turbofan engines from Pratt & Whitney Canada, with target thrust reversers and Full Authority Digital Engine Control (FADEC). |
Side view of the Hawker 4000. |
The Hawker 4000 avionics suite includes a Honeywell Primus Epic integrated flight control and flight management system. |
| Hawker Beechcraft Hawker 400XP | ||
The Hawker Beechcraft Beechjet 400A light business jet was renamed the Hawker 400XP in May 2003 and has been upgraded with an increase in gross weight of 90kg. |
The Beechjet 400A entered service in 1990. |
The 400XP business jet can accommodate up to eight passengers. |
Maximum range with four passengers is more than 1,400nm. |
The aircraft is powered by two Pratt & Whitney Canada JT15D-5 axial flow turbofan engines rated at 2,965lb take-off power. |
The aircraft has been sold to the US Air Force and the Japan Air Self Defence Force, for use in pilot training. |
More than 700 Beechjet aircraft are in service worldwide. |
Maximum speed of the 400XP is 538mph. |
The flight deck is equipped with Rockwell Collins Pro Line 4 electronic flight and information system. |
| Hawker Beechcraft Hawker 750 | ||
The Hawker Beechcraft Hawker 750 offers the speed and take-off performance advantages of the longer range Hawker 800XP aircraft, but the ventral fuel tank has been replaced with an external baggage compartment providing 32ft³ of additional baggage capacity. |
The 5ft 9in-high, 6ft-wide cabin of the Hawker 750 allows easy movement during the flight. |
The Hawker 750 is equipped with the Rockwell Collins Pro Line 21 avionics suite with four 8in x 10in high-resolution Active Matrix Liquid Crystal Displays (AMLCD). |
| Hawker Beechcraft Hawker 800XP | ||
The Hawker 800XP extended performance mid-size business jet. |
The Hawker 800XP taking off. |
The Hawker 800XP can be configured as a business or VIP jet or as a special mission aircraft. |
The Hawker 800XP entered service in 1995. |
The 800XP features an uprated engine, enhanced aerodynamics, increased design weight and system upgrades. |
The interior has been extensively restyled with new windows, seats, lighting and tables. |
Over 1,000 Hawker series aircraft have been delivered. |
800XP aircraft have been configured for special missions including flight inspection. |
The 800XP is powered by two Honeywell TFE731-5BR-1H turbofan engines each rated at 20.73kN. |
| Hawker Beechcraft Hawker 900XP | ||
The Hawker Beechcraft Hawker 900XP is a development of the Hawker 800/800XP mid-sized business jet with improved payload capabilities, enhanced performance and upgraded systems. |
The versatile cabin of the Hawker 900XP allows a large variety of layouts with each aircraft interior being designed to satisfy the requirements and tastes of the individual customer. |
The Hawker 900XP is equipped with the Rockwell Collins Pro Line 21 avionics suite with four 8in x 10in high-resolution Active Matrix Liquid Crystal Displays (AMLCD). |
| Hawker Beechcraft Premier 1 | ||
Deliveries of the Premier 1 light business jet I began in 2001, following FAA certification, including single pilot approval. |
The Premier 1 aircraft features a composite fuselage for superior strength and less weight and swept metal wings for greater speed. |
The Premier 1 with the Hawker 4000 (previously known as the Hawker Horizon) in the foreground. |
The interior of the Premier 1 has four club-style seats and two fixed seats at the rear. |
The six-passenger entry-level Premier 1, shown alongside the Hawker 4000 (previously known as the Hawker Horizon - foreground). |
The Premier 1 has a cruise speed of more than 520mph. |
| SJ30-2 | ||
The SJ30-2 intercontinental light business jet. |
The SJ30-2 has a range of 4,630km (2,500 miles) and flies at speeds up to 890km/h (Mach 0.83). |
The flight deck is equipped with Honeywell Primus Epic avionics. |
A typical cabin layout includes six passenger seats. |
The SJ30-2 maintains a sea level pressure cabin to an altitude of 12,500m (41,000ft) with a very high pressurisation differential of 12psi. |
The SJ30-2 received Federal Aviation Administration (FAA) certification in October 2005. |
The SJ30-2 is powered by two Williams International FJ44-2A turbofan engines rated at 10.23kN. |
Orders for over 150 aircraft have been received. |
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| TBM 850 | ||
The TBM 850's top speed of 320ktas puts it close to that of light business jets, which are more expensive to operate. |
The TBM 850 comes with an avionics system that includes a three-axis autopilot, colour weather radar, terrain avoidance system, in-flight traffic avoidance system (TCAS). |
The standard TBM 850 configuration consists of four seats and a two-piece rear bench seat (four forward and two facing aft). |