|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single engine
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
2.5 m
1,200 kg
220 km/h
short takeoff and landing
|
|
gptkbp:aircraft_role
|
gptkb:transport_aircraft
|
|
gptkbp:aircraft_type
|
general aviation
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:control_surfaces
|
gptkb:elevator
ailerons
rudder
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
Fairchild Aircraft engineers
|
|
gptkbp:engine
|
gptkb:Lycoming_O-360
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:fuselage_material
|
gptkb:metal
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fairchild 160
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Fairchild_Aircraft
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,588 kg
|
|
gptkbp:notable_features
|
good visibility
high wing configuration
large cabin space
|
|
gptkbp:number_built
|
gptkb:100
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_history
|
used in various roles
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:primary_user
|
gptkb:civil_aviation
|
|
gptkbp:production_years
|
1955-1960
|
|
gptkbp:propeller
|
2
constant speed propeller
|
|
gptkbp:propulsion
|
propeller-driven
|
|
gptkbp:range
|
1,200 km
1,000 km
|
|
gptkbp:related_aircraft
|
gptkb:Fairchild_24
gptkb:Fairchild_27
gptkb:Fairchild_22
|
|
gptkbp:retirement_year
|
gptkb:1970
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:successor
|
gptkb:Fairchild_24
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Fairchild_160_A
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wing_configuration
|
gptkb:metal
|
|
gptkbp:wingspan
|
11.58 m
|
|
gptkbp:bfsParent
|
gptkb:Sherman_Fairchild
|
|
gptkbp:bfsLayer
|
6
|