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gptkbp:instance_of
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gptkb:engine
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|
gptkbp:bfsLayer
|
5
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|
gptkbp:bfsParent
|
gptkb:Dassault_Falcon_900
gptkb:Falcon_900_series
gptkb:Falcon_900
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|
gptkbp:aircraft_operated
|
gptkb:Falcon_family
fixed-wing aircraft
low-wing
1.83 meters
varies by owner
2.34 meters
large business jet
7.92 meters
|
|
gptkbp:avionics
|
gptkb:Honeywell_Primus_2000
|
|
gptkbp:capacity
|
up to 19 passengers
|
|
gptkbp:certification
|
Stage 3 noise compliant
|
|
gptkbp:competitors
|
gptkb:Gulfstream_GIV
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
corporate jet
|
|
gptkbp:elevation
|
F L410
|
|
gptkbp:engine
|
gptkb:3
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:1984
|
|
gptkbp:fuel_capacity
|
14,000 pounds
|
|
gptkbp:height
|
7.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Falcon 900 B
|
|
gptkbp:interior_features
|
1.83 meters
|
|
gptkbp:involved_units
|
over 200
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
23.2 meters
|
|
gptkbp:maintenance
|
1,000 flight hours
|
|
gptkbp:manufacturer
|
gptkb:Dassault_Aviation
|
|
gptkbp:market_segment
|
business aviation
|
|
gptkbp:material
|
monocoque
|
|
gptkbp:max_speed
|
Mach 0.84
|
|
gptkbp:max_takeoff_weight
|
3,000 feet
5,000 feet
45,000 pounds
approximately 120 knots
|
|
gptkbp:notable_features
|
three-engine configuration
|
|
gptkbp:notable_operations
|
private individuals
|
|
gptkbp:operational_area
|
high
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:primary_source
|
business travel
|
|
gptkbp:production_years
|
1984-1999
|
|
gptkbp:range
|
4,750 nautical miles
4,000 nautical miles
4,500 nautical miles
|
|
gptkbp:seating_capacity
|
1,000 pounds
8-12 seats
|
|
gptkbp:service_ceiling
|
51,000 feet
|
|
gptkbp:speed
|
Mach 0.8
|
|
gptkbp:successor
|
gptkb:Falcon_900_EX
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:width
|
2.34 meters
|
|
gptkbp:wing_area
|
1,200 square feet
|
|
gptkbp:wingspan
|
24.5 meters
|
|
gptkbp:year_created
|
gptkb:1984
|