gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
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4
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gptkbp:bfsParent
|
gptkb:Singapore_Air_Force
gptkb:No._3_Group_RAF
gptkb:No._21_Group_RAF
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gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:engine
swept wing
Challenger series
standard and high-density configurations
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gptkbp:avionics
|
gptkb:Honeywell_Primus_1000
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gptkbp:certification
|
gptkb:Transport_Canada
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gptkbp:climb_rate
|
3,800 feet per minute
|
gptkbp:cockpit
|
glass cockpit
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gptkbp:cooling_system
|
wing and tail de-icing
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gptkbp:crew
|
2 pilots
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gptkbp:design
|
executive transport
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gptkbp:elevation
|
35,000 feet
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gptkbp:emergency_services
|
dual hydraulic system
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gptkbp:engine_type
|
twin-engine
General Electric C F34-3 B
|
gptkbp:first_flight
|
gptkb:1995
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gptkbp:fuel_capacity
|
3,600 liters
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label
|
Challenger 604
|
gptkbp:interior_features
|
1.83 meters
|
gptkbp:is_often_used_in
|
corporate travel
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
20.2 meters
|
gptkbp:maintenance
|
600 hours
|
gptkbp:manufacturer
|
gptkb:Bombardier_Aerospace
|
gptkbp:market
|
gptkb:1995
|
gptkbp:market_segment
|
business aviation
|
gptkbp:max_speed
|
850 km/h
|
gptkbp:max_takeoff_weight
|
1,500 meters
1,800 meters
27,200 pounds
|
gptkbp:noise_level
|
75 d B
|
gptkbp:notable_features
|
spacious cabin
|
gptkbp:notable_operations
|
private individuals
charter companies
|
gptkbp:number_of_doors
|
2
|
gptkbp:operational_area
|
$3,000 per hour
|
gptkbp:production_years
|
1995 to 2006
|
gptkbp:propulsion
|
8,729 lbf per engine
|
gptkbp:range
|
6,000 kilometers
4,000 kilometers
5,300 kilometers
|
gptkbp:retirement_year
|
gptkb:2006
|
gptkbp:seating_capacity
|
1,200 pounds
up to 10 passengers
|
gptkbp:service_ceiling
|
41,000 feet
|
gptkbp:setting
|
8 passengers and 2 crew
|
gptkbp:speed
|
828 km/h
|
gptkbp:successor
|
gptkb:Challenger_605
|
gptkbp:tail_type
|
T-tail
|
gptkbp:width
|
2.49 meters
|
gptkbp:wing_area
|
60.5 square meters
|
gptkbp:wingspan
|
19.2 meters
|