Junkers F 13a

GPTKB entity

Statements (47)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aircraft_configuration single-engine
gptkbp:aircraft_operated gptkb:civil_aviation
gptkbp:cockpit enclosed
gptkbp:control_surfaces gptkb:elevator
rudder
aileron
gptkbp:country_of_origin gptkb:Germany
gptkbp:crew gptkb:1
gptkbp:design gptkb:Hugo_Junkers
gptkbp:design_date 1919
gptkbp:design_influence later aircraft models
gptkbp:engine_configuration nose
gptkbp:engine_power 200 hp
gptkbp:engine_type inline engine
gptkbp:first_flight 1919
gptkbp:fuel_capacity 200 L
gptkbp:fuselage_material monocoque
Junkers airfoil
gptkbp:historical_significance first all-metal transport aircraft
https://www.w3.org/2000/01/rdf-schema#label Junkers F 13a
gptkbp:landing_distance 2000 kg
gptkbp:landing_gear tailwheel
gptkbp:length 9.5 m
gptkbp:manufacturer gptkb:Junkers
gptkbp:material gptkb:metal
gptkbp:max_speed 200 km/h
gptkbp:max_takeoff_weight 2200 kg
gptkbp:notable_users gptkb:Lufthansa
gptkbp:number_built gptkb:255
gptkbp:operational_history used in commercial aviation
gptkbp:passenger_capacity gptkb:4
gptkbp:production_location gptkb:Germany
gptkbp:production_years gptkb:1920
1920-1930
gptkbp:propeller two-bladed
gptkbp:range 800 km
gptkbp:retirement_year gptkb:1930
gptkbp:role gptkb:aircraft
gptkbp:service_ceiling 4000 m
gptkbp:tail_type conventional tail
gptkbp:type gptkb:monoplane
gptkbp:variant gptkb:Junkers_F_13b
gptkbp:wing_configuration high-wing
gptkbp:wingspan 14.5 m
gptkbp:bfsParent gptkb:Junkers_F_13
gptkbp:bfsLayer 6