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Dassault Falcon 8X

Unveiled in May 2014 at EBACE, the latest addition to the growing Falcon business jet family entered into service in October 2016 after receiving both EASA and FAA certifications in June 2016.
It also received FalconEye certification and London City approval in the first quarter of 2017.
The Falcon 8X offers a range of 6,450 nm and all the advanced technological features of the popular Falcon 7X from which it is derived, including the industry’s quietest and most comfortable cabin.
The 8X also features the greatest range and the longest cabin in the Falcon line, along with the most extensive selection of cabin configurations available on any large cabin business jet.

DATASHEET

External dimensions

Height(with optional fin tip radome)26 ft 1 in / 7.94 m
Length Overall80 ft 3 in / 24.46 m
Wing Span86 ft 3 in / 26.29 m

Weights

Max. Takeoff Weight73,000 lb / 33,113 kg
Max. Landing Weight62,400 lb / 28,304 kg
Max Zero-Fuel Weight41,000 lb / 18,598 kg
Max. Fuel Weight34,900 lb / 15,830 kg

Engines & avionics

Type3 Pratt & Whitney Canada PW307D – 6,722 lb / 29.9 kN (Max Thrust, ISA + 17°C, SL)
Cockpit3rd Generation of EASy Flight Deck (with Honeywell Primus Epic System)

Cabin dimensions

Cabin Length(excluding cockpit & baggage)42 ft 8 in / 13 m
Cabin Height74 in / 1.88 m
Cabin Width92 in / 2.34 m
Cabin Volume(excluding cockpit & baggage)1,695 ft3 / 48 m3
Baggage Volume140 ft3 / 4 m3

Performances

Range @ .80 Mach cruise(8 pax, 3 crew, NBAA IFR reserves)6,450 nm / 11,945 km
MMO(Maximum Operating Mach Number)Mach .90
Takeoff Distance(SL – ISA, Max Takeoff Weight)6,000 ft / 1,829 m
Landing Distance(FAR 91, 8 pax / 3 Crew, SL, NBAA IFR Reserves)2,150 ft / 656 m
Approach Speed, Vref(8 pax / 3 Crew, NBAA IFR Reserves)106 kias / 197 kph
Max. Certified Altitude51,000 ft / 15,545 m

Dassault Falcon 2000S

The Falcon 2000S, announced at EBACE in May 2011, introduced an entirely new concept of performance, efficiency and value to the business jet market.
The twin-engined, 3,350 nm aircraft provides owners with a full size cabin with onboard connectivity, outstanding short-field and steep approach performance and the ability to make long inter-continental flights in comfort.
Yet, its fuel efficiency and operating costs are much less than that of jets in the next smaller category.
The 2000S features inboard slats, EASy II, the world’s most advanced flight deck with FalconEye, Dassault’s unique Combined Vision System option, along with one of the most competitive acquisition costs in its category. 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. Takeoff Weight41,000 lb / 18,598 kg
Max. Landing Weight39,300 lb / 17,827 kg
Max. Zero Fuel Weight29,700 lb / 13,472 kg
Max. Fuel Weight14,600 lb / 6,622 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 II Flight Deck (with Honeywell Primus Epic System)

Cabin dimensions

Cabin Length(excluding cockpit & baggage)26 ft 2 in / 7.98 m
Cabin Height74 in / 1.88 m
Cabin Width92 in / 2.34 m
Cabin Volume(excluding cockpit & baggage)1,024 ft3 / 29 m3
Baggage Volume130.6 ft3 / 3.7 m3

Performances

Range @ Long Range Cruise(6 pax, 2 crew, NBAA IFR reserves)3,500 nm / 6,482 km
MMO(Maximum Operating Mach Number)Mach 0.862
Takeoff Distance(SL – ISA,Max Take Off Weight)4,325 ft / 1,318 m
Landing Distance (Typical)(FAR Part 91, 6 pax, SL, NBAA IFR reserves)2,315 ft / 706 m
Approach Speed (Vref)(Typical Landing Weight)107 kias / 198 km/h
Max. Certified Altitude47,000 ft / 14,325 m

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



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).

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