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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:Douglas_DC_family
commercial transport
high-mounted wing
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|
gptkbp:capacity
|
12 passengers
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|
gptkbp:cockpit
|
open cockpit
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|
gptkbp:crew
|
2 pilots
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|
gptkbp:design
|
gptkb:Donald_W._Douglas
low-wing monoplane
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|
gptkbp:engine
|
gptkb:Pratt_&_Whitney_R-1830
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:features
|
streamlined fuselage
|
|
gptkbp:first_flight
|
1937
1933-02-01
TWA route from New York to Chicago
|
|
gptkbp:fuel_capacity
|
1,500 liters
|
|
gptkbp:height
|
3.9 m
|
|
gptkbp:historical_significance
|
first all-metal airliner
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas DC-1
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|
gptkbp:influenced
|
future aircraft designs
|
|
gptkbp:influenced_by
|
gptkb:Douglas_DC-2
|
|
gptkbp:introduced
|
1934
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:legacy
|
foundation for DC-2 and DC-3
|
|
gptkbp:length
|
24.4 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:material
|
metal construction
|
|
gptkbp:max_speed
|
320 km/h
|
|
gptkbp:max_takeoff_weight
|
90 km/h
7,500 kg
|
|
gptkbp:nationality
|
gptkb:United_States
|
|
gptkbp:number_built
|
gptkb:musical
|
|
gptkbp:operational_history
|
TWA, American Airlines
|
|
gptkbp:operator
|
gptkb:TWA
|
|
gptkbp:production_years
|
1933-1934
|
|
gptkbp:propulsion
|
2
|
|
gptkbp:range
|
1,600 km
|
|
gptkbp:retired
|
gptkb:TWA
|
|
gptkbp:retirement_year
|
1937
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
7,600 m
|
|
gptkbp:services
|
1934
|
|
gptkbp:significance
|
pioneering airliner design
|
|
gptkbp:speed
|
250 km/h
|
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_DC-2
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:type
|
propeller-driven aircraft
|
|
gptkbp:variant
|
gptkb:DC-2
|
|
gptkbp:wing_area
|
80 m²
|
|
gptkbp:wingspan
|
30.5 m
|
|
gptkbp:bfsParent
|
gptkb:James_S._Mc_Donnell_III
|
|
gptkbp:bfsLayer
|
6
|