Junkers A 260 A

GPTKB entity

Statements (59)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aircraft_operated gptkb:Junkers_Ju_52
gptkb:item
passenger transport
civil transport aircraft
gptkbp:armament gptkb:none
gptkbp:climb_rate 5 m/s
gptkbp:cockpit enclosed cockpit
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
gptkbp:fuel_capacity 800 L
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