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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-deck
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|
gptkbp:aircraft_operated
|
gptkb:aircraft
8.5 m
500 km/h
28.5 m
8,000 kg
|
|
gptkbp:aircraft_role
|
gptkb:Flight
|
|
gptkbp:aircraft_type
|
turboprop aircraft
|
|
gptkbp:capacity
|
up to 40 passengers
|
|
gptkbp:cargo_capacity
|
1,500 kg
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
2 pilots
2-3 crew members
|
|
gptkbp:decommissioned
|
gptkb:1980s
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine_power
|
1,200 hp
|
|
gptkbp:engine_type
|
twin-engine
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
3,000 liters
|
|
gptkbp:height
|
8.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas DC-26
|
|
gptkbp:introduced
|
1947
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
28.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
12,000 kg
15,000 kg
|
|
gptkbp:notable_operators
|
gptkb:United_Airlines
|
|
gptkbp:number_built
|
over 600
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:passenger_capacity
|
2-2 seating arrangement
|
|
gptkbp:production_years
|
1947-1950
|
|
gptkbp:propeller
|
variable-pitch propellers
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
passenger transport
|
|
gptkbp:service_ceiling
|
7,600 m
|
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:used_by
|
various airlines
|
|
gptkbp:variant
|
gptkb:Douglas_DC-3
|
|
gptkbp:wing_area
|
100 m²
|
|
gptkbp:wingspan
|
30.2 m
|
|
gptkbp:bfsParent
|
gptkb:James_S._Mc_Donnell_III
|
|
gptkbp:bfsLayer
|
7
|