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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aerodynamic_layout
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monoplane layout
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gptkbp:aircraft_operated
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gptkb:civil_aviation
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gptkbp:armament
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gptkb:none
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gptkbp:capacity
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gptkb:6
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gptkbp:cockpit
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enclosed
tandem seating
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gptkbp:control_surfaces
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elevators, ailerons, rudder
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gptkbp:crew
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gptkb:1
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gptkbp:cruise_speed
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250 km/h
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gptkbp:design
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low-wing monoplane
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gptkbp:elevator_control
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conventional control
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gptkbp:engine
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gptkb:Pratt_&_Whitney_R-985
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gptkbp:engine_configuration
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front-mounted
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gptkbp:engine_type
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gptkb:radial_engine
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gptkbp:first_flight
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1936
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gptkbp:flaps
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split flaps
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gptkbp:fuel_capacity
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1,200 L
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gptkbp:fuselage_material
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gptkb:metal
gptkb:NACA_23012
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gptkbp:height
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3.05 m
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gptkbp:historical_significance
|
used in early commercial aviation
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|
https://www.w3.org/2000/01/rdf-schema#label
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Model 12 Electra Junior
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gptkbp:landing_distance
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90 km/h
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gptkbp:landing_gear
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tailwheel
tailwheel landing gear
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gptkbp:length
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10.67 m
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gptkbp:manufacturer
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gptkb:Lockheed
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gptkbp:max_speed
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320 km/h
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gptkbp:notable_users
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gptkb:Pan_American_Airways
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gptkbp:number_built
|
approximately 100
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gptkbp:power_source
|
2 × Pratt & Whitney R-985-AN-1
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gptkbp:production_location
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gptkb:United_States
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gptkbp:production_years
|
1936-1941
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gptkbp:propeller
|
2
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gptkbp:range
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1,600 km
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gptkbp:role
|
gptkb:transport_aircraft
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gptkbp:rudder_control
|
conventional control
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gptkbp:service_ceiling
|
6,000 m
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gptkbp:stall_speed
|
70 km/h
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gptkbp:successor
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gptkb:Lockheed_Model_14_Super_Electra
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gptkbp:tail_type
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conventional tail
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gptkbp:takeoff_distance
|
500 m
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gptkbp:taxi_speed
|
30 km/h
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gptkbp:variant
|
gptkb:Lockheed_Electra
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gptkbp:weight
|
2,500 kg
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gptkbp:weight_limit
|
3,600 kg
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gptkbp:wing_area
|
30.5 m²
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gptkbp:wing_configuration
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gptkb:metal
85 kg/m²
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gptkbp:wing_structure
|
cantilever wing
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gptkbp:wingspan
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15.24 m
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gptkbp:bfsParent
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gptkb:Lockheed_Model_10_Electra
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gptkbp:bfsLayer
|
6
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