|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
Fairchild Aircraft engineers
|
|
gptkbp:engine_type
|
gptkb:radial_engine
|
|
gptkbp:first_flight
|
1939
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:fuselage_material
|
metal and fabric
|
|
gptkbp:historical_significance
|
used in World War II
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fairchild 21 A
|
|
gptkbp:landing_gear
|
tailwheel configuration
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Fairchild_Aircraft
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:nickname
|
gptkb:Fairchild_21
|
|
gptkbp:notable_features
|
high-wing monoplane design
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_history
|
used in various roles including reconnaissance and transport.
|
|
gptkbp:passenger_capacity
|
2
|
|
gptkbp:production_location
|
gptkb:United_States
|
|
gptkbp:production_years
|
1939-1941
|
|
gptkbp:range
|
800 km
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:used_by
|
military and civilian operators
|
|
gptkbp:variant
|
Fairchild 21 A-1
Fairchild 21 A-2
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:weight_limit
|
1,800 kg
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wingspan
|
12.8 m
|
|
gptkbp:bfsParent
|
gptkb:Fairchild_21
|
|
gptkbp:bfsLayer
|
7
|