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The Dassault Falcon 50 is a French super-midsize, long-range business jet, featuring a trijet layout with an S-duct air intake for the central engine. It has the same fuselage cross-section and similar capacity as the earlier twin-engined Falcon 20, but was a new design that is area ruled and includes a more advanced wing design.^[3]

• 3Operators
• 7References

Design and development[edit]

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.^[3] Dassault developed a maritime surveillance and environmental protection version as the Gardian 50.^[4]

The Falcon 50 was later updated as the Falcon 50EX, the first of which flew in 1996,^[5] and the last of which was delivered in 2008.^[1] The Falcon 50EX features improved engines and other enhancements to give further range improvements to an already long-range jet. The Falcon 50EX designation applies to serial numbers 253–352, which marks the end of the production line for the Falcon 50/50EX.

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The last Falcon 50EX was built in late 2007 and delivered in early 2008.

Successors to the Falcon 50 are the Falcon 7X^[6] 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 selection, was supposed to be completed by early 2009. However, in a June 2009 press conference, CEO Charles Edelstenne said that all design choices had been reopened and the goal was extended 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.^{[citation needed]}

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By 2018, Falcon 50s from the mid-late 1980s were priced at $0.879 to $1.6 million while 1998-2003 Falcon 50EXs can be had for $2.95 to $3.95 million.^[7]

Variants[edit]

Falcon 50

Basic initial variant with Honeywell TFE 731-3-1C engines and optional auxiliary power unit (APU); 252 manufactured, with one serving as a prototype for the Falcon 50EX.^[8][9]

Falcon 50EX

Marketing name for Falcon 50 with TFE 731-40 engines; an APU installed as standard equipment; changes to the rudder control system; updated avionics; and other improvements; 100 manufactured, plus one modified Falcon 50^[8][9]

Operators[edit]

The majority of Falcon 50s are operated by corporate and individual owners.

Military and government operators[edit]

Benin

Bolivia

Bulgaria

• Bulgarian Air Force - former operator

Burundi

Djibouti

France

• French Air Force - former operator
• French Navy operate eight Falcon 50M for maritime surveillance.

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Egypt

• Egyptian Air Force - former operator

Falcon 50 Emergency Slot Extension System

Iran

Iraq^[10]

Italy

• The Italian Air Force operated four Falcon 50s from 1985 until 2005, when two aircraft were retired.^[11]

Jordan

• Jordanian Royal Flight; Libya

Morocco

Portugal

Rwanda

Serbia

South Africa

Spain

Sudan

• Sudan Government

Falcon 50 Emergency Slot Extension Machine

Switzerland

Venezuela

Accidents and incidents[edit]

• 6 April 1994: Rwandan President Juvénal Habyarimana and Burundian President Cyprien Ntaryamira were killed when the Falcon 50 they were travelling in (registration 9XR-NN) was shot down near Kigali, Rwanda, triggering the Rwandan genocide.
• 20 October 2014: Falcon 50EX F-GLSA collided with a snow plow while taking off from Moscow Vnukovo Airport, Russia, killing all four people on board, including the CEO of Total oil and gas company Christophe de Margerie.

Specifications (50EX)[edit]

Data from Flight International^[12]

General characteristics

• Crew: 2
• Capacity: 8 to 9 passengers / 1,080 kg (2,381 lb) payload with full fuel
• Length: 18.52 m (60 ft 9 in)
• Wingspan: 18.86 m (61 ft 11 in)
• Height: 6.98 m (22 ft 11 in)
• Wing area: 46.83 m² (504.1 sq ft) ^[13]
• Max takeoff weight: 18,008 kg (39,701 lb)
  
• Max Landing Weight: 16,200 kg (35,715 lb)
• Powerplant: 3 × Honeywell TFE 731-40turbofan engines, 16.46 kN (3,700 lbf) thrust each

Performance

• Maximum speed: 1,015 km/h (631 mph, 548 kn)
• Maximum speed: Mach 0.86
• Cruise speed: 903 km/h (561 mph, 488 kn) / M0.85 at 15,000 m (49,000 ft)
• Range: 5,695 km (3,539 mi, 3,075 nmi)
• Service ceiling: 14,936 m (49,003 ft)
• Rate of climb: 10.433 m/s (2,053.7 ft/min)
  
• Take-off run: 1,504 m (4,934 ft)
• Landing run: 685 m (2,247 ft)

See also[edit]

Related development

Aircraft of comparable role, configuration and era

Related lists

References[edit]

1. ^ ^ab'News Channel - Homepage - flightglobal.com'. Flightglobal.com. Archived from the original on 28 August 2008. Retrieved 26 April 2018.
2. ^'Purchase Planning Handbook'(PDF). Business & Commercial Aviation. Aviation Week. May 2006. Archived(PDF) from the original on 2017-03-09.
3. ^ ^abTaylor 1988, p.75.
4. ^Taylor 1993, p.928
5. ^'News Channel - Homepage - flightglobal.com'. Flightglobal.com. Archived from the original on 6 June 2009. Retrieved 26 April 2018.
6. ^'News Channel - Homepage - flightglobal.com'. Flightglobal.com. Archived from the original on 6 June 2009. Retrieved 26 April 2018.
7. ^Mark Huber (December 2018). 'For many models, market hitting the apex'(PDF). Aviation International News. pp. 20–21, 24.
8. ^ ^abType Certificate Data Sheet A46EU, p. 4
9. ^ ^abType Certificate Data Sheet A46EU, p. 16
10. ^'The USS Stark Incident: That time a Modified Iraqi Falcon 50 Business Jet almost Sank a US Navy Frigate'. 2019-07-10.
11. ^'Official website Aeronautica Militare'. difesa.it. Archived from the original on 15 December 2014. Retrieved 26 April 2018.
12. ^'Super Mid-Size Jets'. Flight International.
13. ^Taylor 1988, pp.75–76.

Bibliography[edit]

• Federal Aviation Administration Type Certificate Data Sheet No. A46EU, Revision 18: Dassault Aviation Mystere-Falcon 50, Mystere-Falcon 900, Falcon 900EX; August 17, 2016
• Taylor, Michael J. H. (1993). Jane's Encyclopedia of Aviation. London: Studio Editions.
• Taylor, John W. R. (editor). Jane's All the World's Aircraft 1988–89. Coulsdon, Surrey, UK: Jane's Information Group. ISBN0-7106-0867-5.

External links[edit]

The cruciform tail is an aircraftempennage configuration which, when viewed from the aircraft's front or rear, looks much like a cross. The usual arrangement is to have the horizontal stabilizer intersect the vertical tail somewhere near the middle, and above the top of the fuselage. The design is often used to locate the horizontal stabilizer away from jet exhaust, propeller and wing wake, as well as to provide undisturbed airflow to the rudder.^[1]

• 3References

Applications[edit]

• British Aerospace Jetstream 31/32
• Cessna Citation - Excel, Sovereign and Latitude variants only
• Dassault Falcon 10/100
• Dassault Falcon 20/200
• McDonnell F2H Banshee - early variants only^{[N 1]}
• Rockwell Commander 112/114

See also[edit]

References[edit]

Notes[edit]

Falcon 50 Emergency Slot Extension Tool

1. ^A cruciform tail was used on the XF2D-1, F2H-1, F2H-2, F2H-2B, F2H-2N, and F2H-2P Banshee variants. The later F2H-3 and F2H-4 used a conventional tail.

References[edit]

1. ^What-when-how. 'Tail designs'. what-when-how.com. Retrieved 8 April 2018.