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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single aisle
single aisle configuration
|
|
gptkbp:aircraft_operated
|
450 knots
narrow-body aircraft
45,000 lb
29 ft 0 in
99 ft 10 in
|
|
gptkbp:aircraft_role
|
gptkb:aircraft
|
|
gptkbp:aircraft_type
|
gptkb:aircraft
commercial jet airliner
|
|
gptkbp:cargo_capacity
|
1,500 lb
1,500 pounds
|
|
gptkbp:ceiling
|
37,000 ft
|
|
gptkbp:crew
|
2
2 pilots
|
|
gptkbp:cruise_speed
|
0.74 Mach
|
|
gptkbp:design
|
final design
|
|
gptkbp:engine
|
two engines
|
|
gptkbp:engine_type
|
gptkb:Pratt_&_Whitney_JT8_D
turbofan
|
|
gptkbp:first_delivery
|
1970-03-01
|
|
gptkbp:first_flight
|
1970-01-01
|
|
gptkbp:flight_deck
|
two-pilot cockpit
|
|
gptkbp:fuel_capacity
|
5,000 pounds
5,000 lb
|
|
gptkbp:height
|
8.84 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas DC-9-50
|
|
gptkbp:landing_distance
|
60,000 pounds
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
30.53 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:max_speed
|
0.85 Mach
|
|
gptkbp:max_takeoff_weight
|
65,000 pounds
65,000 lb
|
|
gptkbp:number_built
|
97
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_history
|
used by various airlines
|
|
gptkbp:operational_use
|
passenger transport
|
|
gptkbp:passenger_capacity
|
139
139 passengers
|
|
gptkbp:payload_capacity
|
20,000 pounds
|
|
gptkbp:production_years
|
1965-1982
|
|
gptkbp:range
|
2,000 nautical miles
2,000 mi
|
|
gptkbp:related_aircraft
|
gptkb:Mc_Donnell_Douglas_DC-9-40
gptkb:DC-9_family
gptkb:Mc_Donnell_Douglas_DC-9-30
|
|
gptkbp:retirement
|
gptkb:2006
|
|
gptkbp:service_ceiling
|
37,000 feet
|
|
gptkbp:service_entry
|
gptkb:1970
|
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_MD-80
|
|
gptkbp:tail_type
|
N12345
|
|
gptkbp:variant
|
gptkb:DC-9
|
|
gptkbp:wing_area
|
1,200 ft²
|
|
gptkbp:wingspan
|
28.35 m
93 ft 0 in
|
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gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas
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gptkbp:bfsLayer
|
4
|