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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
two-class or three-class
freighter version
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:DC-10-40
used in various airlines worldwide
part of the DC-10 family
|
|
gptkbp:aircraft_role
|
passenger and cargo
commercial aviation
|
|
gptkbp:aircraft_type
|
wide-body airliner
|
|
gptkbp:built
|
60
|
|
gptkbp:cargo_capacity
|
20,000 kg
|
|
gptkbp:crew
|
2
|
|
gptkbp:cruise_speed
|
Mach 0.84
|
|
gptkbp:design
|
Mc Donnell Douglas engineers
|
|
gptkbp:engine
|
gptkb:General_Electric
|
|
gptkbp:engine_type
|
gptkb:CF6-50
turbofan
|
|
gptkbp:first_delivery
|
1972-02-01
1989-12-31
|
|
gptkbp:first_flight
|
1970-08-29
|
|
gptkbp:fuel_capacity
|
110,000 liters
|
|
gptkbp:height
|
17.4 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas DC-10-40
|
|
gptkbp:influenced
|
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:influenced_by
|
gptkb:Douglas_DC-8
|
|
gptkbp:introduced
|
gptkb:1972
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
55.4 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:max_speed
|
850 km/h
|
|
gptkbp:max_takeoff_weight
|
260,000 lb
|
|
gptkbp:notable_case
|
several accidents
|
|
gptkbp:number_of_engines
|
gptkb:3
|
|
gptkbp:operational_cost
|
high
|
|
gptkbp:operational_range
|
4,500 nautical miles
|
|
gptkbp:orbital_altitude
|
12,500 m
|
|
gptkbp:passenger_capacity
|
270
|
|
gptkbp:payload_capacity
|
45,000 lb
|
|
gptkbp:primary_user
|
gptkb:American_Airlines
gptkb:United_Airlines
gptkb:Continental_Airlines
|
|
gptkbp:production_years
|
1970-1989
|
|
gptkbp:range
|
5,000 km
6,000 km
|
|
gptkbp:related_aircraft
|
gptkb:DC-10_family
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:safety_record
|
mixed
|
|
gptkbp:service_ceiling
|
13,700 m
|
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:variant
|
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:wing_area
|
370 m²
|
|
gptkbp:wingspan
|
50.4 m
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_RB211
|
|
gptkbp:bfsLayer
|
5
|