gptkbp:instance_of
|
gptkb:engine
|
gptkbp:bfsLayer
|
4
|
gptkbp:bfsParent
|
gptkb:Falcon_2000_LXS
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Falcon_7_X
gptkb:Falcon_900_EX
gptkb:Falcon_50_EX
gptkb:Falcon_2000_series
low-wing
swept wing
|
gptkbp:avionics
|
gptkb:Honeywell_Primus_2000
|
gptkbp:certification
|
gptkb:EASA
|
gptkbp:competes_with
|
gptkb:Bombardier_Challenger_300
gptkb:Embraer_Legacy_600
gptkb:Gulfstream_G200
|
gptkbp:crew
|
2 pilots
|
gptkbp:design
|
corporate transport
Dassault engineers
|
gptkbp:elevation
|
F L410
|
gptkbp:engine
|
2
|
gptkbp:engine_type
|
Honeywell TF E731-40 BR
|
gptkbp:environmental_impact
|
air conditioning and pressurization
|
gptkbp:first_flight
|
gptkb:2003
|
gptkbp:fuel_capacity
|
14,000 pounds
|
gptkbp:height
|
20 feet 4 inches
|
https://www.w3.org/2000/01/rdf-schema#label
|
Falcon 2000 EX
|
gptkbp:interior_features
|
1,100 cubic feet
|
gptkbp:landing_gear
|
tricycle gear
retractable landing gear
|
gptkbp:layout
|
glass cockpit
|
gptkbp:length
|
68 feet 2 inches
|
gptkbp:manufacturer
|
gptkb:Dassault_Aviation
|
gptkbp:market_segment
|
business aviation
|
gptkbp:marketed_as
|
gptkb:Falcon_2000_EX
|
gptkbp:max_speed
|
Mach 0.84
|
gptkbp:max_takeoff_weight
|
38,000 pounds
43,000 pounds
|
gptkbp:notable_features
|
advanced avionics
large cabin
high speed cruise
|
gptkbp:notable_operations
|
private and commercial use
|
gptkbp:operational_range
|
3,000 nautical miles with 8 passengers
|
gptkbp:production_location
|
gptkb:Monarch
|
gptkbp:production_years
|
2003 to present
|
gptkbp:propulsion
|
4,600 lbf
|
gptkbp:range
|
3,800 nautical miles
|
gptkbp:seating_capacity
|
3,000 pounds
1,000 pounds
8 to 10 passengers
|
gptkbp:service_ceiling
|
45,000 feet
|
gptkbp:setting
|
8 passengers and 2 crew
|
gptkbp:speed
|
480 knots
|
gptkbp:successor
|
gptkb:Falcon_2000_LXS
|
gptkbp:tail_type
|
T-tail
|
gptkbp:variant
|
gptkb:Falcon_2000
|
gptkbp:wing_area
|
750 square feet
|
gptkbp:wingspan
|
86 feet 3 inches
|
gptkbp:year_created
|
gptkb:2003
|