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Dassault Falcon 2000LXS

Dassault Falcon 2000LXS -Go where others can’t go: The superior agility of the new 4,000 nm Falcon 2000LXS gives you access to challenging airfields. In fact, no other jet in its category can deliver so many airports and deliver so much range out of them. So fly farther. Tuck into short fields. Handle steep approaches. Go where others can’t.

Green dots represent airports the Falcon 2000LXS can use (at MTOW) in addition to the airports (red) usable by others in its class

The Falcon 2000LXS was launched in October 2012 during the NBAA convention in Orlando.
The Falcon 2000LXS flies 4,000 nm while cruising at Mach .80.
Thanks to its full span slats, optimized aerodynamics and advanced acoustics, it offers the ultimate combination of airfield agility, fuel efficiency and quiet, widebody comfort.
Just like the Falcon 2000S, it features EASy II, the world’s most advanced flight deck with FalconEye, Dassault’s unique Combined Vision System option as well as onboard connectivity.
It can fly direct from New York to Anchorage or Berlin; from Dubai to London City Airport or from Beijing to Mumbai. EASA/FAA certifications were received early April 2013.



DATASHEET

External dimensions

Height23 ft 2 in / 7.06 m
Length Overall66 ft 4 in / 20.23 m
Wing Span70 ft 2 in / 21.38 m

Weights

Max. Take Off Weight42,800 lb / 19,414 kg
Max. Landing Weight39,300 lb / 17,826 kg
Max. Zero Fuel Weight29,700 lb / 13,472 kg
Max. Fuel Weight16,600 lb / 7,530 kg

Engines & avionics

Type2 Pratt&Whitney Canada PW308C with new Talon II™ combustor for lower nitrogen oxides (NOx) emissions. – 7,000 lb / 31.14 kN (Thrust, ISA + 15°C, SL)
CockpitEASy Flight Deck (with Honeywell Primus Epic System)

Cabin dimensions

Cabin Length26 ft 2 in / 7.98 m
Cabin Height74 in / 1.88 m
Cabin Width92 in / 2.34 m
Cabin Volume1,024 ft3 / 29 m3
Baggage Volume130.6 ft3 / 3.7 m3

Performances

Range @ Mach 0.80(6 pax, 2 crew, NBAA IFR reserves, ISA, full fuel)4,150 nm / 7,686 km
MMO(Maximum Operating Mach Number)Mach 0.862
Max. Certified Altitude47,000 ft / 14,326 m
Take Off Distance(SL – ISA,Max Take Off Weight)4,675 ft / 1,425 m
Landing Distance (Typical)(FAR Part 91, 6 pax, SL, NBAA IFR reserves)2,260 ft / 689 m
Approach Speed (Vref)(Typical Landing Weight)105 kias / 194 km/h



Cessna Citation Longitude

Cessna Citation Longitude
Cessna’s entry into the super midsize jet category is going straight to the top. With a 4,000 nm range, a Mach .86 cruising speed, and a 45,000-foot maximum cruising altitude, the Citation Longitude delivers far more performance than other midsize jets far more efficiently. Performance is not the only bar-raising characteristic of the Longitude. It also sets a new standard in private business travel for cabin efficiency, technology, luxury, and comfort.

Cessna Citation X

Cessna Citation X
The fastest civil airplane in the world is going to get you where you’re going before anyone else. The Citation X will climb to 51,000 feet and cruise at incredible speeds of up to Mach 0.935. The fact that it gets you back on the ground sooner may be bittersweet, however, because this jet comes with a reimagined, smart plane interior you may never want to leave.

Cessna Citation Sovereign+

Cessna Citation Sovereign+
Improving on greatness is what we do best. With upgraded avionics, an all new interior, enhanced technology, and better performance, the Sovereign+ answers the call of today’s business leaders and what they want in a corporate jet. We’ve also lowered maintenance costs by extending and enhancing warranties. Get the visionary midsize jet for visionary travelers.

Cessna Citation Latitude

Cessna Citation Latitude
Cessna’s answer to the next-generation business-travel environment is here. We endeavored to create the most open, spacious, light, and refined cabin environment in this category of aircraft. When we came close to having it right, we displayed a concept mock-up of that cabin interior at our main service center for months, inviting our customers to scrutinize every detail and offer their feedback. That process led to today’s Citation Latitude: a clean, contemporary luxury environment with 77 inches of width, 6 feet of height, a flat floor, and over 21 feet of cabin length. Then we surrounded that interior with an aircraft built to the same rigorous standards. The result is a world-class business jet with 2,500 nm (4,630 km) of range and a maximum cruising altitude of 45,000 feet (13,106 meters). The Latitude takes up to nine passengers farther in wide and spacious luxury. 

Cessna Citation XLS+

Cessna Citation XLS+
Along with the largest cabin in its class, we’ve given the world’s most sought-after business jet a series of improvements that take it to a whole new level. The XLS+ combines transcontinental range, first-class cabin luxury for up to 12 passengers, and remarkable performance efficiency in a beautiful midsize jet loaded with features generally reserved for large, commercial aircraft. Take your business global and enjoy the ride.

Cessna Citation CJ4

Cessna Citation CJ4
The CJ4 marks a new level of performance maturity for the CJ family, providing added speed, range, and cabin size over its predecessor without incurring midsize jet operating costs. Technological advancements such as the Venue™ Cabin Management System and a spacious cabin interior upgraded for style and comfort also distinguish this jet. Impressive runway performance, refined wing design, and an enhanced powerplant round out the CJ4’s benefits, making it a favorite among corporate fleets.

Cessna Citation CJ2+

Cessna Citation CJ2+
The Citation CJ2+ jet introduces the CJ series with class. With a focus on technology, reliability, and performance to operating cost ratio, we’ve created a versatile business jet perfect for a private owner or as the optimal addition to any corporate fleet. Representing some of the smartest business jets in the world, the CJ2+ features excellent takeoff and landing capability, a spacious, comfortable cabin, more speed, greater range, and a higher ceiling. Get ready to expand your horizons.

Cessna Citation CJ3

Cessna Citation CJ3
Engineered for precise handling, superior performance, and aerodynamic prowess, the CJ3 features a new, wider-span, natural-laminar-flow wing design as well as a roomier cabin, longer range, greater speed, faster climb, and optimized fuel efficiency. Operating this single-pilot certified lightweight jet is so intuitive, it has pilots and passengers alike falling, or flying, in love with private air travel anew. Not all jets are distinguished as “Best of the Best,” but the CJ3 is. The Robb Report editors selected the Cessna Citation CJ3 as “Best of the Best Business Aircraft Light.”

Dassault Falcon 2000

The Dassault Falcon 2000 is a French Business jet and a member of Dassault Aviation's Falcon business jet line, and is a twin-engine, slightly smaller development of the Falcon 900 trijet, with transcontinental range.

Powerplants  
Two 25.6kN (5725lb) CFE (General Electric & AlliedSignal) CFE73811B turbofans.

Performance  
Max cruising speed at 39,000ft Mach 0.83-0.85. Max certificated altitude 47,000ft. Range at 0.80 Mach cruising speed with eight passengers 5560km (3000nm), at 0.75 Mach 5788km (3125nm).

Weights  
Empty equipped 9405kg (20,735lb), max takeoff 16,238kg (35,800lb).
Dimensions  
Wing span 19.33m (63ft 5in), length 20.23m (66ft 5in), height 7.06m (23ft 2in). Wing area 49.0m2 (527.6sq ft).
Capacity  
Flightcrew of two. Main cabin seating typically for eight passengers, or up to 12 in a high density layout.
Production  
First customer delivery occurred in March 1995. Over 60 delivered by late 1998.
Type  
Transcontinental range mid to large size corporate jet

History  
The Falcon 2000 is the latest member of the Falcon business jet line, and is a transcontinental range, slightly smaller development of the Falcon 900 trijet
The Falcon 2000 shares the 900's wing and forward fuselage, but there are a number of design changes. From the start the Falcon 2000 was designed with a range of 5560km (3000nm) in mind, which is less than the transcontinental 900's range. This design range removed the need for the redundancy of three engines for long range overwater flights, allowing the two new CFE738 engines to be fitted, which offer considerable maintenance and operating economics benefits. The CFE738 engine was developed specifically for the Falcon 2000 by a partnership of General Electric and AlliedSignal, known as CFE. Meanwhile, the 2000's fuselage is 1.98m (6ft 6in) shorter than the 900's and so houses less fuel, passengers and baggage.
Another noticeable design change between the 900 and 2000 is the area ruled rear fuselage. Dassault engineers found that the three engine layout of the 900 to be aerodynamically efficient, whereas the twin engine design of the 2000 originally would have been comparatively draggy. To combat this and reduce drag to desired levels Dassault designed an area ruled (or Coke bottle) rear fuselage, using its Catia three dimensional computer aided design program.
Changes to the wing include a modified leading edge and the inboard slats have been removed, while the cockpit features a Collins four screen EFIS avionics system with optional Flight Dynamics head-up displays (allowing hand flown approaches in Cat II and Cat IIIa conditions).
Dassault has a number of industry partners in the Falcon 2000 program, foremost of these being Alenia, which is a 25% risk sharing partner. Alenia in turn has subcontracted some work to Dee Howard and Piaggio.

Dassault announced it was developing the Falcon 2000, then known as the Falcon X, in June 1989. First flight occurred on March 4 1993 and certification was awarded in November 1994. The first customer delivery occurred in March 1995.

Dassault Falcon 900

The Dassault Falcon 900 is a French-built corporate jet aircraft made by Dassault Aviation. It, and its larger sibling the Falcon 7X, are the only trijets in production. Both aircraft are notable in featuring an S-duct central engine.

Variants

Falcon 900
Original production. Powered by three 20 kN (4,500 lbf) Garrett TFE731-5AR-1C turbofan engines.
Falcon 900 MSA
Maritime patrol version for Japan Coast Guard. Equipped with search radar and hatch for dropping rescue stores.
Falcon 900B
Revised production version from 1991. Powered by 21.13 kN (4,750 lbf) TFE731-5BR-1C engines.
Falcon 900EX
Long range version, with 22.24 kN (5,000 lbf) TFE731-60 engines and more fuel to give range of 8,340 km (4,501 nm; 5,180 miles). Improved avionics. Entered service 1996.
Falcon 900C
Replacement for 900B with improved avionics. Introduced 2000.
Falcon 900DX
Current medium range production type. TFE731-60 engines.
Falcon 900LX
Variant of EX fitted with Blended Winglets designed by Aviation Partners Inc.. Improved range of 8,890 km (5,520 mi).
VC-900A
Italian military designation for the 900EX.
VC-900B
Italian military designation for the 900EASY

Powerplants  
900B - Three 21.1kN (4750lb) AlliedSignal TFE731-5BRs.
900EX - Three 22.3kN (5000lb) TFE731-60s.


Performance  
900B - Max cruising speed 927km/h (500kt), economical cruising speed Mach 0.75. Max certificated altitude 51,000ft. Range with 15 passenger and reserves 7116km (3840nm), with eight passengers and reserves at Mach 0.80 7150km (3860nm).
900EX - Range with eight passengers at Mach 0.80 8020km (4330nm), at long range cruising speed 8335km (4500nm).


Weights  
900B - Empty equipped 10,255kg (22,611lb), max takeoff 20,640kg (45,500lb).
900EX - Empty equipped 10,830kg (23,875lb), max takeoff 21,909kg (48,300lb).

Dimensions  
Wing span 19.33m (63ft 5in), length 20.21m (66ft 4in), height 7.55m (24ft 9in). Wing area 49.0m2 (527.43sq ft).
Capacity  
Flightcrew of two. Main passenger cabin seating for between eight and 15 passengers, or up to 18 in a high density configuration.
Production  
Over 260 Falcon 900s (including 7 900Cs, 74 900EXs, and 2 900MSAs) delivered by mid 2000.
Type  
Large transcontinental range corporate jet

History  
The Falcon 900 intercontinental range trijet is a substantially revised development of the Falcon 50.
Dassault announced it was developing a new intercontinental range large size business jet based on the Falcon 50 on May 27 1983 at the Paris Airshow. The prototype, "Spirit of Lafayette", flew for the first time on September 21 1984. A second prototype flew on August 30 1985, and this aircraft demonstrated the type's long range potential by flying nonstop from Paris to Little Rock, Arkansas in the USA for a demonstration tour. French certification was awarded on March 14 1986, FAA certification followed on March 21, and first customer deliveries occurred in December that year.
While of similar overall configuration to the Falcon 50, the Falcon 900 intoduced an all new wider and longer fuselage which can seat three passengers abreast. The main commonality with the Falcon 50 is the wing, which despite being designed for a considerably lighter aircraft, was adapted almost directly unchanged. In designing the Falcon 900 Dassault made use of computer aided modelling, while the aircraft's structure incorporates a degree of composite materials.
Two Falcon 900s entered service with the Japanese Maritime Safety Agency for the long-range maritime surveillance role as the Falcon 900MSA, equipped with search radar, special communications equipment, observation windows, a control station, and a drop hatch.
From 1991 the standard production model was the Falcon 900B, which differs from the earlier 900 in having more powerful engines, increased range, the ability to operate from unprepared strips and Category II visibility approach clearance. Earlier production 900s can be retrofitted to 900B standard.
The Falcon 900EX is a longer range development launched in October 1994. It features TFE731-60 engines, a Honeywell Primus 2000 EFIS avionics suite, optional Flight Dynamics head-up displays, increased fuel capacity and greater range. Its first flight was on June 1 1995 and first delivery was in May 1996.
The latest Falcon 900 model is the 900C. Revealed in 1998, the C is a development of the B but incorporates the advanced Honeywell Primus avionics of the 900EX, but without autothrottles. The 900C replaced the 900B in the Falcon product line with first deliveries in early 2000.

From 2003 the 900EX will introduce Dassault's EASy avionics operating system with four colour displays, cursor control devices and multifunction keyboards.

Dassault Falcon 20

The Dassault Falcon 20 is a French business jet and was the first of a family of business jets built by Dassault Aviation.

Variants


Mystère/Falcon 20
Prototype, one built. F-WLKB. Now stored at Musée Air et Espace Aéroport Paris - Le Bourget.
Mystère/Falcon 20C
Initial production version. known originally as the Standard Falcon 20 both examples converted to D model.
Falcon 20CC
One aircraft similar to the Falcon 20C, equipped with low-pressure tyres.
Mystère/Falcon 20D
Higher thrust engines (General Electric CF700-2D) and lower fuel consumption and more fuel capacity.
Mystère/Falcon 20E
Higher thrust engines (General Electric CF700-2D-2), higher zero fuel weight.
Mystère/Falcon 20F
Full leading edge slats and more fuel capacity.
Falcon 20FH
This was the original designation of the Falcon 200 prototype.
Falcon 20G
Maritime patrol and surveillance version, equipped with two Garrett AiResearch ATF3-6-2C turbofan engines.
Falcon 20H
This was the original designation of the Falcon 200.
Falcon 200
Improved variant, powered by two 2360-kg (5,200-lb) Garrett ATF3-6A-4C turbofan engines and with more fuel. First flown 30 April 1980.
Falcon ST
This designation was given to two Falcon 20s used by the French Air Force as systems training aircraft. The aircraft were equipped with the combat radar and navigation systems of the Mirage IIIE.
HU-25A Guardian
United States Coast Guard version of the Falcon 20G. 41 built. Equipped with two Garrett AiResearch Garrett ATF3-6-2C turbofan engines.
HU-25B Guardian
Pollution control version for the US Coast Guard equipped with side-looking airborne radar (SLAR) under fuselage. Seven converted from HU-25As.
HU-25C Guardian
Drug interdiction version for the US Coast Guard, equipped with a Westinghouse APG-66 search radar and WF-360 Forward looking infrared turret. Nine HU-25As converted.
HU-25C+ Guardian
Upgrade of HU-25C, with improved AN/APG-66(V)2 radar and new FLIR turret. All nine HU-25Cs converted.
HU-25D Guardian
Upgraded HU-25A, with AN/APS-143B(V)3 Inverse synthetic aperture radar (ISAR) and same FLIR as HU-25C+. 15 upgraded.
Guardian 2
Maritime patrol and surveillance version of the Falcon 200. Never put into production.
CC-117
Canadian military designation of Falcon 20C from 1970.
Fan Jet Falcon
The Falcon 20 was marketed in North America under this name.
Falcon Cargo Jet
Conversion of Falcon 20 to light cargo aircraft. Large numbers purchased/converted by Federal Express for overnight courier service.
Falcon 20C-5, 20D-5, 20E-5, 20F-5
Falcon 20 aircraft equipped with Garrett TFE-731-5AR-2C or TFE-731-5BR-2C engines. Also includes adaptation of bleed air, anti-ice, hydraulic, fuel, electrical and engine control systems and installation of ATTCS (automatic takeoff thrust control system).

Dassault Falcon 50

The Dassault Falcon 50 is a French-built super mid-sized, long-range corporate jet, featuring a three jet engine layout with an S-duct central engine. It has the same fuselage cross section and similar capacity as the earlier Falcon 20 twinjet but is a completely new design that is Area ruled and includes a more advanced wing design.
The first prototype flew on 7 November 1976, with French airworthiness certification on 27 February 1979, followed by U.S. Federal Aviation Administration certification on 7 March 1979. Dassault developed a maritime surveillance and environmental protection version as the Gardian 50.
The Falcon 50 was later replaced by the Falcon 50EX, the first of which flew in 1996, and the last of which was delivered in 2008. The Falcon 50EX features improved engines and other enhancements to give further range improvements to an already long-legged jet. It remains a very popular corporate jet for its long-range, luxury, and for the recognition of status for owning a fast three-engined jet.
The last Falcon 50EX was built in late 2007 and delivered in early 2008. Successors of the Falcon 50 are the Falcon 7X and the Falcon 900 featuring a larger fuselage and the same three-engine arrangement. Dassault announced in January 2008 what is essentially a replacement aircraft for the Falcon 50, codenamed the "SMS" (Super Mid Size). The basic design process, including engine select was supposed to be completed by the early 2009. However, in a June 2009 press conference, CEO Charles Edelstenne said that all design choices had been reopened and the goal was intended to the end of the year.
Dassault and Aviation Partners Inc. have announced that High Mach blended winglets were being developed for the Falcon 50 as a retrofit kit.

Powerplants  
50 - Three 16.5kN (3700lb) AlliedSignal TFE7313 turbofans. 50EX - Three 16.5kN (3700lb) TFE73140s.

Performance  
50 - Max cruising speed 880km/h (475kt), long range cruising speed 797km/h (430kt). Max operating altitude 45,000ft. Range with eight passengers and reserves 5715km (3084nm). 50EX - Range with eight passengers at Mach 0.80 5600km (3025nm), at Mach 0.75 6046km (3265nm).

Weights  
50 - Empty equipped 9150kg (20,170lb), standard max takeoff 17,600kg (38,800lb), or optionally 18,500kg (40,780lb). 50EX - Empty equipped 9603kg (21,270lb), max takeoff 18,005kg (39,700lb).
Dimensions  
Wing span 18.86m (61ft 11in), length 18.52m (61ft 11in), height 6.98m (22ft 11in). Wing area 46.8m2 (504.1sq ft).
Capacity  
Flightcrew of two pilots. A number of cabin seating arrangements offered. Seating for eight or nine with aft toilet, or for up to 12 with forward toilet. Max accommodation for 19. Can accommodate three stretchers, two medical attendants and medical equipment in a medevac role.
Production  
More than 275 have been delivered since 1979.
Type  
Long range mid size corporate jet

History  
The trijet Falcon 50 is a very substantial long range upgrade based on the earlier twinjet Mystère/Falcon 20 and 200 family.
The Dassault Falcon 50 was developed for long range trans Atlantic and transcontinental flight sectors, using the Falcon 20 as the design basis. However, to meet the 6440km (3475nm) range requirement significant changes mean that the Falcon 50 is for all intents and purposes an all new aircraft.
Key new features include three 16.6kN (3700lb) Garrett TFE731 turbofans, in place of the Falcon 20's two General Electric CF700s, mounted on a new area ruled tail section, plus a new supercritical wing of greater area than that on the 20 and 200. Falcon 20 components retained include the nose and fuselage cross section.
The first flight of the prototype Falcon 50 occurred in November 1976, although it wasn't until March 7 1979 that FAA certification was granted. In the meantime the design had been changed to incorporate the supercritical wing, although the original wing's basic planform was retained. A second prototype first flew on February 18 1978, the first preproduction aircraft following on June 13 1978. First customer deliveries began in July 1979.
In April 1995 Dassault announced the long range Falcon 50EX with more fuel efficient TFE73140 turbofans, 740km (400nm) greater range (at Mach 0.80) than the base Falcon 50 and a new EFIS flightdeck based on the Falcon 2000's with Collins Pro Line 4 avionics. The 50EX also features as standard equipment items offered as options only on the standard Falcon 50.
The Falcon 50EX's maiden flight was on April 10 1996, with French and US certification in November and December 1996 respectively. First delivery (to Volkswagen) was in the following January.

The Surmar is a maritime patrol version of the 50 ordered by the French navy (fitted with a FLIR and search radar).

Dassault Falcon 7X

Dassault Falcon 7X


The benchmark for the 21st century business jet

When designing the new 7X, we were inspired by our customers’ business needs. Together with our unrivalled experience, technological strengths and military knowledge, we built more than a jet. We created a vision for the future.
 
One that delivers more Falcon qualities, more innovations and more benefits to corporate flight than ever before.

The next generation Falcon 7X. The benchmark for the 21st century business jet.


 

Design in the digital age

A completely new aircraft needed a completely new engineering process. The
Falcon 7X engineering team used ‘Dassault Systèmes’ powerful PLM solutions to create a virtual design representing every feature on the 7X, from the smallest component to the complete, finished aircraft while optimizing future operating performance and maintenance requirements.


The figures

From nose to tail, wingtip to wingtip, the Falcon 7X is pure elegance, efficiency, and performance. The following specifications physically define the world’s most technologically advanced business jet. 

External dimensions
Length23.19 m
Height7.83 m
Wing span26.21 m
Internal dimensions
Cabin length (excluding cockpit and baggage)11.91 m
Maximum headroom1.88 m
Maximum width2.34 m
Cabin volume (excluding cockpit and baggage)44 m3
Weights
Maximum take off weight31,751 kg
Maximum zero fuel weight18,598 kg
Maximum fuel14,488 kg
Maximum landing weight28,304 kg
Engines
ManufacturerP&W Canada
Nbr/Type3 x PW307A
SL-ISA Thrust28.48 kN
Flat rated toISA+17°C


Advanced technologies. Ground-breaking innovations. Near-perfect aerodynamics, space-age materials and jet fighter heritage. This is the 7X. Where will it take you?

Redefining performance

The Falcon 7X is the most technologically advanced business jet in service anywhere in the world today. Sleek yet practical, it is redefining ownership, pilot and passenger performance. It is the new generation of business aircraft.

Further. Faster. And better connected.

The Falcon 7X is designed to fly 5,950 nm, linking you to the vital city pairs including Paris-Tokyo, Shanghai-Seattle, New-York-Jeddah, and Johannesburg-London. And with a payload of eight passengers and a crew of three. It has a 0.90 Mach Maximum Operating Speed (MMO) to get you where you need to be faster - so you arrive fresh and alert.


Slower, safer landings

When it comes to landing, slower is safer. At typical landing weight, the approach speed of the 7X is only 104 knots. It can land and stop in just 2,070 ft and as a result, can access hundreds of airports other jets cannot. And that includes those with hot and high conditions, steep approaches and stringent noise restrictions.

The 7X is the only aircraft in its class cleared for operation at London City Airport.​

Agile and efficient

The maximum landing weight of the 7X is very close to its maximum take-off weight. So it can perform multiple short and long flights without having to refuel. 


“The 7X redefines ownership, pilot and passenger performance.”

BFL at MTOW: SL - ISA5,710 ft 1,740 m
FAR 91 landing distance: at typical landing weight2,070 ft631 m
Approach Speed Vref at typical landing weight104 kias193 kph
Maximum operating altitude51,000 ft15,545 m
Range5,950 nm11,019 km
Maximum speed370 kias685 kph
Maximum operating Mach MMOM .90M .90

Flexible and cost-effective

The flexibility of the Falcon 7X allows it to perform varied missions easily. Its fuel consumption is 15-30% lower than other jets in its class. And its operating and maintenance costs save operators millions of dollars compared to other global-range aircraft.



The innovative Digital Flight Control System

The Falcon 7X is the first business jet in the world equipped with a Digital Flight Control System. This technology is transferred directly from our jet fighters and gives more precise handling, reduces workload, thus improving safety. This fly-by-wire system also delivers a quieter, smoother ride by calming turbulence.



EASy II: Business aviation’s most advanced flight deck

In 2003, Falcon introduced the EASy flight deck. This revolutionary cockpit, designed using Dassault’s military Man-to-Machine expertise, was a major breakthrough that dramatically improved situational awareness and decreased pilot workload and stress. EASy II is a major new upgrade of this flight deck. Built on the latest technological developments and operator feedback, EASy II further improves pilot situational awareness, safety and efficiency.


PW307A Engines: Power behind the performance

Delivering 6,400 lb of thrust each, the three Pratt & Whitney Canada PW307A engines power the 7X to new levels of performance and efficiency. The engines are quiet enough to use airports like London City and clean enough to exceed stringent emission standards. They are dependable enough to be given an outstanding warranty, guaranteed maintenance plan and worldwide support from Pratt & Whitney Canada.





Gulfstream G150

Gulfstream G150

G150 Overview

The G150® is quickly becoming a favorite in the mid-size market. With the longest range at the fastest speed, an advanced avionics suite, and the most comfortable cabin, the G150 provides the most value in its class.
Through the use of high thrust, fuel-efficient Honeywell TFE731-40AR engines, combined with numerous aerodynamic improvements, the Gulfstream G150 is the fastest mid-sized business aircraft in the world today. The G150 started breaking speed records even before it went into service. A G150 test aircraft established a city-pair speed record on a flight from Tel Aviv to Geneva.
Turning to the cockpit, Gulfstream's avionics and research staff improved the Rockwell Collins ProLine 21 avionics system, adding some of the advanced technology inherent in the vaunted Gulfstream PlaneView® cockpit. The result was a fully integrated avionics system that enhances flight-crew performance and improves the overall level of flight safety.
Gulfstream engineers and interior designers also focused on the G150's cabin. Now with a longer, wider, more oval-shaped cabin, the G150 offers operators a choice of three seating configurations accommodating up to eight passengers. It also provides more seated shoulder room, headroom and legroom than any competing aircraft in the mid-sized category.
Many elements support the inherent value of the G150. In the six years of service, the G150 fleet boasts an enviable 99.8 percent dispatch-reliability rate. On the financial side, the G150 generates some of the lowest operating costs in the industry. The comprehensive warranty on the airplane covers its primary structures, engines, and all production components (APU, avionics, etc.) for five years. Then there's Gulfstream's award-winning worldwide product support, bolstered by a network of 3,500 fully trained professionals positioned across six continents.
The best-in-class in the mid-sized aircraft category, the G150 proudly upholds the Gulfstream tradition.

G150 Overview
Long Range Cruise Mach 0.75
Mmo Mach 0.85
Range at LRC 3,000 nm / 5,556 km
Typical Passenger Payload 4 passengers



G150 Performance

The wide-cabin, high-speed Gulfstream G150® is the fastest mid-size business jet in the world today. To create this unique, continental-range, eight-passenger aircraft, Gulfstream's G150 development team worked to provide the longest range at the fastest speed while enabling short takeoff distances from demanding airports. In fact, Gulfstream delivered the G150 with more range and shorter takeoff and landing distances than what was originally promised. Gulfstream has a tradition of not only meeting, but also exceeding our customer's expectations.
The outstanding performance of the G150 is the result of superior aerodynamic design and efficient Honeywell engines. These TFE731-40AR engines have an increased thrust of 4,420 pounds (19.7 kN) each for good performance from hot and high airports. Think Aspen in summer or Toluca virtually anytime. These advanced engines also meet the stringent Stage 4 noise regulations.
With its improved aerodynamic profile and its more powerful engines, the new Gulfstream G150 has posted impressive numbers since going into service. In the first two years of service, the G150 has set 10 world city-pair speed records including New York to California, California to Hawaii, and from Aspen to New York.
The G150 can reach a maximum operating speed of Mach 0.85 and climb in steps to a ceiling of 45,000 feet (13,716 m), well above commercial traffic and weather. At its long-range cruise speed of Mach 0.75, it can whisk four passengers some 3,000 nautical miles (5,556 km). At Mach 0.80, the G150 can fly four passengers 2,600 nautical miles (4,185 km) in less than six hours. With this range and at this speed, Gulfstream's first true mid-size jet easily links New York with Los Angeles, London with Gander, São Paulo with Caracas and Cairo with Delhi.
The G150 outperforms every other mid-size business jet on the market today. It flies higher, faster and farther than the competition yielding an outstanding reputation. Due to its performance capability, large cabin and advanced avionics, the editors of Flying Magazine were so impressed, they presented the G150 with the Flying Magazine's 2006 "Editor's Choice" award.

G150 Performance
Long Range Cruise Mach 0.75
Mmo Mach 0.85
Normal Cruise Mach 0.80
Range at LRC 3,000 nm / 5,556 km
Range at Normal Cruise 2,600 nm / 4,815 km
Takeoff Distance (MTOW, SL, ISA) 5,000 ft / 1,524 m
Typical Passenger Payload 4 passengers


G150 Technology

When Gulfstream developed the wide-cabin, high-speed G150® business jet, they set out to build the most technically advanced mid-sized business jet in the world. They succeeded.
The advanced G150 cockpit employs Rockwell Collins ProLine 21 avionics systems as the basic architecture now enhanced by PlaneView™-like features that improves situational awareness for the pilot and creates a safer operating environment for the airplane.
The Rockwell Collins ProLine 21 avionics encompass four 12-by-10-inch (30 cm by 25 cm) LCD flight displays with Engine Indicating Crew Alerting System, a dual integrated Flight Management System with integrated GPS and a maintenance diagnostic computer. To enhance its operational efficiency, Gulfstream added a series of PlaneView-like features, including: Gulfstream's signature Cursor Control Devices (CCD) and electronic Jeppesen charts at no additional charge.
The Cursor Control Device, a Gulfstream innovation that was first introduced on the G550®, enables G150 pilots to input data easily and provides instant display of information, including flight plan and routing changes. The side-mounted cursor control device is integrated with the cockpit so as to be redundant with traditional controls. It reduces pilot workload through interactive controls, menu selections and range / speed scrolling. The G150 also offers options for a paperless cockpit, electronic checklists, graphical weather, a three dimensional view of your flight path, and a moving map system.
Gulfstream is also incorporating new, advanced technologies on the G150. In 2009, Gulfstream will be offering the Enhanced Vision System™ (EVS II, Heads Down) as an option to improve safety through greater situational awareness.
The Gulfstream G150 boasts the most advanced cockpit with its fully integrated systems, large easy to read displays, and unique features to reduce pilot workload and enhance safety.

G150 Cockpit

The G150 cockpit features Rockwell Collins Pro Line 21 avionics.

G150 CCD

The G150 cockpit features the Gulfstream-exclusive cursor control device (CCD) also employed in large-cabin flight decks.

G150 Interiors

Gulfstream engineers and interior designers had two goals in mind when they began to design the cabin of the G150® business jet into a larger, wider, more comfortable and productive business tool. They sought to create a cabin that would promote productivity while vastly improving passenger comfort at the same time.
Relative to its predecessor, the G100®, the new cabin on the G150 is 16 inches (41 cm) longer, 12 inches (30 cm) wider, and has a reshaped interior cross section to produce a cabin dimension of 5 feet 9 inches (1.75 m) in width by 5 feet 9 inches (1.75 m) in height. They developed three distinct cabin layouts to comfortably accommodate six, seven or eight passengers with an option to include an additional passenger with a belted lavatory.
The G150 cabin is designed to maximize passenger comfort with the best overall environment. The G150 includes the G200®-style windows for more natural lighting and better viewing. Passengers will enjoy the 100 percent fresh air that is infused into the living environment to help inhibit jet lag. By applying the technologies and materials found in our large cabin aircraft, Gulfstream was successful in providing the quietest cabin in its class with unmatched interior quality.
"I would say probably one of the most impressive aspects of the interior for me personally was the storage," says John Morikis, president and chief operating officer of the Sherwin-Williams Company. Sherwin-Williams is a global leader in the manufacture and sale of coatings and related products. "The quietness of the plane was a pleasant surprise for me. I hadn't noticed how much quieter this one was until we started bopping around between different planes and we're all now fighting for this 150. We all like it because of the comfort and just how quiet it is."
Dale Hood, the chief pilot and director of aviation at Sherwin-Williams, agrees. "We've had nothing but positive feedback from passengers regarding the cabin quality and comfort," he says.
It is evident that the G150 development team has created the ideal working environment for creative collaboration at 41,000 feet (12,497 m).



Executive Six

Designed for maximum comfort and storage space, this cabin configuration seats six passengers.

Universal Seven

This configuration provides the same comfortable four-seat grouping as the Executive, but by replacing a club chair with a two-place divan, the interior can now accommodate an additional passenger.

Hallmark Eight

Designed for maximum passenger capacity, this interior can accommodate eight passengers.

G150 Specifications

Performance

Long Range Cruise Mach 0.75
Mmo Mach 0.85
Normal Cruise Mach 0.80
Range at LRC 3,000 nm / 5,556 km
Range at Normal Cruise 2,600 nm / 4,815 km
Takeoff Distance (MTOW, SL, ISA) 5,000 ft / 1,524 m

Weights

Basic Operating 15,100 lbs / 6,849 kg
Maximum Fuel 10,300 lbs / 4,672 kg
Maximum Landing 21,700 lbs / 9,843 kg
Maximum Payload 2,400 lbs / 1,090 kg
Maximum Payload/Full Fuel 850 lbs / 386 kg
Maximum Ramp 26,250 lbs / 11,907 kg
Maximum Takeoff 26,100 lbs / 11,839 kg
Maximum Zero Fuel 17,500 lbs / 7,938 kg

Design Standards

Engine Type Honeywell TFE731-40AR
Thrust Rating 4,420 lbs / 19.66 kN (each)
Typical Passenger Payload 4 passengers

Interior

Total Interior Length 17 ft 8 in / 5.38 m
Cabin Length 17 ft 8 in / 5.38 m
Height 5 ft 9 in / 1.75 m
Width 5 ft 9 in / 1.75 m
Cabin Volume 465 cu ft / 13.16 cu m
Baggage Volume (Gross) 80 cu ft / 2.26 cu m

Exterior

Height 19 ft, 1 in / 5.82 m
Length 56 ft, 9 in / 17.30 m
Wingspan 55 ft, 7 in / 16.94 m
Range with 4 passengers, 2 crew, NBAA IFR reserves. Actual range will be affected by ATC routing, operating speed, weather, outfitting options and other factors.

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