The Dassault Falcon 50EX 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 is a completely new design that is area ruled and includes a more advanced wing design.
The Dassault Falcon 50EX is the 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.
Seats Full Range (NM / SM): 3142 / 3616
Ferry Range (No Payload) (NM / SM): 3,303 / 3,801
Balance Field Length (Take-off Distance in Feet): 4,875
Landing Distance (Feet): 2,673
Average Block Speed (KTS / MPH): 448 / 515
Normal Cruise (KTS / MPH): 447 / 515
Long Range Cruise Speed (KTS / MPH): 419 / 482
Fuel Usage (Gallons Per Hour): 307.00
Service Ceiling (Feet): 49,000
Useful Payload With Full Fuel (Lbs): 2,077
Maximum Take Off Weight: 39,700
Maximum Landing Weight: 35,715
Basic Operating Weight: 21,694
Total Usable Fuel Weight: 15,132
RANGE MAP
Minimum Crew / Maximum Passengers: 2 / 9
Baggage Capacity External / Internal (Cubic Feet): 90 / 25
Cabin Height (Feet): 5’11”
Cabin Width (Feet): 6’1″
Cabin Length (Feet): 23’6″
Cabin Volume (Cubic Feet): 845.84
Years in Production: 1997-2007
Active Fleet (approximate): 101.00
Airframe Maintenance Per Hour: $649.00
Engine / APU Maintenance Per Hour: $1,080.00
Fuel Cost based on Gallons Per Hour: $1,304.75
Crew Misc.: $467.00
Total Variable Cost Per Hour: $3,500.75
Cost Per NM: $7.82