The Falcon 50 of Dassault Aviation is the third business aircraft and the first tri-jet launched by the company in 1976. It was an extrapolation of the Mystère 20 with a third engine placed in foot of drift. The 3 engines were of Garrett. The first MSA 50 left factory on September 4th, 1976 is only Falcon to be equipped with ejector seats.

The model was replaced in April 1996 by the 50EX ( Extended arranges ) motorized by of Honeywell.

The extrapolation of the 50 is the Falcon 900 which is equipped with a widened fuselage. Falcon 50 is exploited by companies of businesses and the National marine within the framework of the maritime surveillance missions in a slightly modified version (Falcon 50M Surmar).

The last Falcon 50 left chain in 2007 was the n°353.

Characteristics Falcon 50

• Many passengers: 8 to 12

• Passable distance: 6480 km (2940 Nm)
• Cruising speed max: Mach 0.80
• Scale: 18,85 m
• Length: 18,50 m
• Height: 6,97 m
• wing Surface: 46,83 m ²
• Ceiling: 14.935 m
• Empty weight: 9150 kg
• Driving: 3 X Garrett TFE731-3-1C

Characteristics Falcon 50 Surmar ( ON veillance MAR itime)

Same features as higher, but light modifications:

• Bays of observation

• Trap door of dropping of chains SAR/SECMAR
• Radar built-in Thomson-CSF OM 100 (Ocean Master 100)
• infra-red Camera & thermal FLIR Chlio (Thalès Detexis)
• satellite Station (inmarsat)
• Cruising speed max: Mach 0.85 (lower mass)

External bonds

• Official site Dassault Falcon 50
• Falcon 50 the site of the National marine
• Airliners.net

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