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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Junkers_A_20
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Junkers_A_50
gptkb:item
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:date
|
gptkb:1922
|
|
gptkbp:design
|
gptkb:Hugo_Junkers
|
|
gptkbp:engine
|
200 hp
|
|
gptkbp:engine_type
|
inline engine
|
|
gptkbp:first_flight
|
1923
|
|
gptkbp:fuel_capacity
|
300 L
|
|
gptkbp:height
|
3.1 m
|
|
gptkbp:historical_context
|
post-World War I aviation development
|
|
gptkbp:historical_role
|
pioneering transport aircraft
|
|
gptkbp:historical_significance
|
early commercial aviation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Junkers A 20a
|
|
gptkbp:influenced_by
|
gptkb:Junkers_F.13
|
|
gptkbp:is_used_by
|
gptkb:Luftwaffe
|
|
gptkbp:landing_gear
|
tailwheel landing gear
|
|
gptkbp:legacy
|
influenced future aircraft designs
|
|
gptkbp:length
|
9.5 m
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:material
|
gptkb:item
high-wing monoplane
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,500 kg
|
|
gptkbp:notable_features
|
all-metal construction
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_history
|
used in the 1920s and 1930s
|
|
gptkbp:primary_user
|
German airlines
|
|
gptkbp:production_location
|
gptkb:government_agency
|
|
gptkbp:production_years
|
1923-1930
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:4
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:setting
|
high-wing monoplane configuration
|
|
gptkbp:successor
|
gptkb:Junkers_A_50
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:variant
|
gptkb:Junkers_A_20b
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
12.5 m
|