|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
high-wing configuration
|
|
gptkbp:aircraft_operated
|
general aviation
|
|
gptkbp:aircraft_type
|
gptkb:light_aircraft
|
|
gptkbp:cockpit
|
single pilot cockpit
|
|
gptkbp:control_surfaces
|
gptkb:elevator
rudder
aileron
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:cruise_speed
|
120 knots
|
|
gptkbp:design
|
Fairchild Aircraft design team
|
|
gptkbp:engine_configuration
|
front-mounted engine
|
|
gptkbp:engine_power
|
200 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
50 US gallons
|
|
gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
8 ft 6 in
|
|
gptkbp:historical_significance
|
used in various roles during its service life.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fairchild 390 B
|
|
gptkbp:landing_distance
|
1,000 ft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
27 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:Fairchild_Aircraft
|
|
gptkbp:marketed_as
|
gptkb:Fairchild_390_B
|
|
gptkbp:max_speed
|
150 knots
|
|
gptkbp:notable_users
|
gptkb:United_States_Army
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:offers_certificate
|
gptkb:TC_3_A2
|
|
gptkbp:passenger_capacity
|
gptkb:4
|
|
gptkbp:production_location
|
gptkb:United_States
|
|
gptkbp:production_years
|
1955-1960
|
|
gptkbp:propeller
|
two-bladed propeller
|
|
gptkbp:range
|
600 nautical miles
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:stall_speed
|
60 knots
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:takeoff_distance
|
1,200 ft
|
|
gptkbp:transportation
|
20 knots
|
|
gptkbp:variant
|
gptkb:Fairchild_24
|
|
gptkbp:weight
|
2,200 lb
|
|
gptkbp:weight_limit
|
3,600 lb
|
|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wing_configuration
|
gptkb:metal
|
|
gptkbp:wingspan
|
39 ft 6 in
|
|
gptkbp:bfsParent
|
gptkb:Fairchild_390
|
|
gptkbp:bfsLayer
|
7
|