gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:aircraft_operated
|
general aviation
|
gptkbp:cargo_capacity
|
1,000 kg
|
gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:controls
|
yoke
|
gptkbp:crew
|
2
|
gptkbp:design
|
high-wing monoplane
Fairchild Aircraft engineers
|
gptkbp:engine_configuration
|
nose-mounted
|
gptkbp:engine_type
|
piston engine
|
gptkbp:first_flight
|
1950
|
gptkbp:flaps
|
split flaps
|
gptkbp:fuel_capacity
|
1,200 L
|
gptkbp:fuselage_material
|
gptkb:metal
|
gptkbp:historical_significance
|
used in various military operations.
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fairchild 280
|
gptkbp:landing_distance
|
300 m
90 km/h
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
8.23 m
|
gptkbp:manufacturer
|
gptkb:Fairchild_Aircraft
|
gptkbp:max_speed
|
300 km/h
|
gptkbp:max_takeoff_weight
|
3,402 kg
|
gptkbp:military_technology
|
gptkb:transportation
charter flights
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
gptkbp:number_built
|
approximately 200
|
gptkbp:number_of_engines
|
gptkb:1
|
gptkbp:operational_range
|
1,200 km
|
gptkbp:passenger_capacity
|
gptkb:6
|
gptkbp:power_source
|
gptkb:Lycoming_O-540
|
gptkbp:primary_user
|
gptkb:United_States_military
|
gptkbp:production_location
|
gptkb:United_States
|
gptkbp:production_years
|
1950-1955
|
gptkbp:propeller
|
two-bladed propeller
|
gptkbp:range
|
1,200 km
|
gptkbp:related_aircraft
|
gptkb:Fairchild_24
gptkb:Fairchild_45
|
gptkbp:retirement_year
|
1970s
|
gptkbp:role
|
utility aircraft
|
gptkbp:service_ceiling
|
4,600 m
|
gptkbp:successor
|
gptkb:Fairchild_300
|
gptkbp:tail_type
|
T-tail
|
gptkbp:takeoff_distance
|
400 m
|
gptkbp:variant
|
gptkb:Fairchild_280_A
gptkb:Fairchild_280_B
gptkb:Fairchild_280_C
|
gptkbp:wing_area
|
25.5 m²
|
gptkbp:wing_configuration
|
gptkb:metal
|
gptkbp:wingspan
|
12.19 m
|
gptkbp:year_established
|
1950
|
gptkbp:bfsParent
|
gptkb:Sherman_Fairchild
|
gptkbp:bfsLayer
|
6
|