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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
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7
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gptkbp:bfsParent
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gptkb:Challenger_601-1_A
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|
gptkbp:aircraft_operated
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low-wing
1.83 meters
2.49 meters
7.32 meters
Challenger family
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gptkbp:average_temperature
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gptkb:military_base
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:capacity
|
up to 19 passengers
|
|
gptkbp:certification
|
gptkb:Transport_Canada
|
|
gptkbp:crew
|
2 pilots
|
|
gptkbp:cuisine
|
enclosed lavatory
|
|
gptkbp:design
|
business aviation
|
|
gptkbp:elevation
|
gptkb:10,000_meters
|
|
gptkbp:emergency_services
|
advanced emergency systems
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
twin-engine
General Electric C F34
|
|
gptkbp:first_flight
|
gptkb:1982
modern flight deck
|
|
gptkbp:fuel_capacity
|
3,600 liters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Challenger 601-1 B
|
|
gptkbp:interior_features
|
varies by customer
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
20.5 meters
|
|
gptkbp:maintenance
|
long maintenance intervals
|
|
gptkbp:manufacturer
|
gptkb:aircraft
|
|
gptkbp:market
|
gptkb:1982
|
|
gptkbp:market_segment
|
business jet market
|
|
gptkbp:material
|
pressurized fuselage
|
|
gptkbp:max_speed
|
850 km/h
|
|
gptkbp:max_takeoff_weight
|
24,000 kg
27,200 kg
|
|
gptkbp:noise_level
|
low noise level
|
|
gptkbp:notable_ships
|
full galley
|
|
gptkbp:notable_users
|
private individuals
|
|
gptkbp:operational_area
|
moderate operational cost
|
|
gptkbp:origin
|
gptkb:Native_American_tribe
|
|
gptkbp:production_years
|
1982-1996
|
|
gptkbp:range
|
5,500 kilometers
|
|
gptkbp:retirement_year
|
still in service
|
|
gptkbp:safety_features
|
advanced safety features
|
|
gptkbp:seating_capacity
|
1,500 kg
1,200 liters
high passenger comfort
|
|
gptkbp:service_ceiling
|
12,500 meters
|
|
gptkbp:speed
|
800 km/h
|
|
gptkbp:successor
|
gptkb:Challenger_604
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:wing_area
|
60.5 square meters
|
|
gptkbp:wingspan
|
19.2 meters
|