|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Falcon_2000_EX
gptkb:Dassault_Falcon_900
gptkb:Falcon_900_series
gptkb:Falcon_900
|
|
gptkbp:aircraft_operated
|
gptkb:Falcon_900_series
fixed-wing aircraft
high-wing configuration
large business jet
|
|
gptkbp:annual_ridership
|
8 to 10 passengers
|
|
gptkbp:avionics
|
gptkb:Honeywell_Primus_2000
|
|
gptkbp:certification
|
Stage 4 noise compliant
|
|
gptkbp:competitors
|
gptkb:Gulfstream_G550
|
|
gptkbp:cooling_system
|
wing and tail de-icing
|
|
gptkbp:crew
|
2 pilots
2 pilots and 1 flight attendant
|
|
gptkbp:design
|
gptkb:engine
|
|
gptkbp:elevation
|
45,000 ft
|
|
gptkbp:emergency_services
|
2
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:engine_type
|
tri-engine
P W305 A
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:fuel_capacity
|
14,000 lb
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:height
|
7.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Falcon 900 EX
|
|
gptkbp:interior_features
|
1.83 m
customizable
|
|
gptkbp:involved_units
|
over 200
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
23.2 m
|
|
gptkbp:maintenance
|
1,500 flight hours
|
|
gptkbp:manufacturer
|
gptkb:Dassault_Aviation
|
|
gptkbp:market_segment
|
business aviation
|
|
gptkbp:max_speed
|
0.84 Mach
|
|
gptkbp:max_takeoff_weight
|
2,500 ft
5,000 ft
34,000 lb
|
|
gptkbp:noise_level
|
low noise emissions
|
|
gptkbp:notable_features
|
advanced avionics
|
|
gptkbp:operational_area
|
$3,000 per hour
|
|
gptkbp:operational_range
|
3,600 nautical miles
|
|
gptkbp:primary_source
|
corporate travel
|
|
gptkbp:production_years
|
1996 to present
|
|
gptkbp:range
|
5,800 km
4,500 nautical miles
|
|
gptkbp:safety_features
|
advanced autopilot system
|
|
gptkbp:seating_capacity
|
up to 14
1,000 lb
|
|
gptkbp:service_ceiling
|
51,000 ft
|
|
gptkbp:speed
|
Mach 0.80
|
|
gptkbp:successor
|
gptkb:Falcon_900_LX
|
|
gptkbp:width
|
2.34 m
|
|
gptkbp:wing_area
|
1,200 ft²
|
|
gptkbp:wingspan
|
24.5 m
|
|
gptkbp:year_created
|
gptkb:1996
|