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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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single-engine
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gptkbp:aircraft_operated
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general aviation
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gptkbp:cockpit
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enclosed cockpit
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gptkbp:control_surfaces
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elevator, ailerons, rudder
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gptkbp:country_of_origin
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gptkb:United_States
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gptkbp:crew
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gptkb:1
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gptkbp:design
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Fairchild Aircraft design team
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gptkbp:engine_power
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200 hp
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gptkbp:engine_type
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piston engine
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gptkbp:financial_stability
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conventional stability
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gptkbp:first_flight
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gptkb:1955
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gptkbp:flaps
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manual flaps
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gptkbp:fuel_capacity
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200 L
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gptkbp:fuselage_material
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gptkb:metal
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gptkbp:height
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2.74 m
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gptkbp:historical_significance
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used in various roles during its service life
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|
https://www.w3.org/2000/01/rdf-schema#label
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Fairchild 390 A
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gptkbp:introduced
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gptkb:1955
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gptkbp:landing_distance
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300 m
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
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8.23 m
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gptkbp:manufacturer
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gptkb:Fairchild_Aircraft
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gptkbp:market
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private and commercial use
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gptkbp:max_speed
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200 km/h
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gptkbp:max_takeoff_weight
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1,588 kg
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gptkbp:notable_features
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high wing configuration
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gptkbp:number_built
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approximately 200
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gptkbp:offers_certificate
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gptkb:Certification
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gptkbp:operational_history
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used in flight training and private ownership.
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gptkbp:passenger_capacity
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gptkb:4
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gptkbp:primary_user
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gptkb:civil_aviation
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gptkbp:production_years
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1955-1960
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gptkbp:propeller
|
two-bladed propeller
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gptkbp:range
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1,200 km
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gptkbp:retired
|
1970s
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gptkbp:role
|
utility aircraft
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gptkbp:service_ceiling
|
3,000 m
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gptkbp:successor
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gptkb:Fairchild_24
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gptkbp:tail_type
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T-tail
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gptkbp:takeoff_distance
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400 m
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gptkbp:variant
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gptkb:Fairchild_390_B
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gptkbp:weight
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1,000 kg
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gptkbp:wing_area
|
15.5 m²
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gptkbp:wing_configuration
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gptkb:metal
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gptkbp:wingspan
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11.58 m
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gptkbp:bfsParent
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gptkb:Fairchild_390
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gptkbp:bfsLayer
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7
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