gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:Junkers_Ju_52
gptkb:item
passenger transport
civil transport aircraft
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gptkbp:armament
|
gptkb:none
|
gptkbp:climb_rate
|
5 m/s
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gptkbp:cockpit
|
enclosed cockpit
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gptkbp:crew
|
2
|
gptkbp:decommissioned
|
1945
|
gptkbp:design
|
gptkb:Hugo_Junkers
low-wing monoplane
|
gptkbp:engine
|
2
2 x 400 hp
|
gptkbp:engine_type
|
piston engine
|
gptkbp:features
|
high aspect ratio wings
|
gptkbp:financial_performance
|
good stability characteristics
|
gptkbp:first_flight
|
1939
|
gptkbp:flaps
|
manual flaps
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gptkbp:fuel_capacity
|
800 L
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gptkbp:height
|
3.5 m
|
gptkbp:historical_significance
|
used in World War II
|
https://www.w3.org/2000/01/rdf-schema#label
|
Junkers A 260 A
|
gptkbp:influenced
|
post-war transport aircraft
|
gptkbp:influenced_by
|
gptkb:Junkers_F_13
|
gptkbp:is_used_by
|
gptkb:Luftwaffe
|
gptkbp:landing_gear
|
tailwheel landing gear
|
gptkbp:length
|
12.5 m
|
gptkbp:manufacturer
|
gptkb:Junkers
|
gptkbp:material
|
gptkb:item
|
gptkbp:max_speed
|
400 km/h
|
gptkbp:max_takeoff_weight
|
300 m
80 km/h
400 m
3,000 kg
|
gptkbp:notable_features
|
all-metal construction
|
gptkbp:operational_area
|
commercial flights
|
gptkbp:operational_history
|
limited operational history
|
gptkbp:origin
|
gptkb:government_agency
|
gptkbp:produced_by
|
approximately 200
|
gptkbp:production_years
|
1939-1945
|
gptkbp:propulsion
|
variable-pitch propeller
|
gptkbp:range
|
1,200 km
|
gptkbp:retirement_year
|
1945
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:seating_capacity
|
gptkb:6
1,000 kg
|
gptkbp:service_ceiling
|
6,000 m
|
gptkbp:services
|
gptkb:1940
|
gptkbp:successor
|
gptkb:Junkers_Ju_52
|
gptkbp:surface
|
elevator and ailerons
|
gptkbp:tail_type
|
conventional tail
|
gptkbp:used_in
|
gptkb:aircraft
|
gptkbp:variant
|
gptkb:Junkers_A_260_B
|
gptkbp:weight
|
1,800 kg
|
gptkbp:wing_area
|
40 m²
|
gptkbp:wingspan
|
15.5 m
|
gptkbp:bfsParent
|
gptkb:Junkers_A_260
|
gptkbp:bfsLayer
|
6
|