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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
narrow-body
|
|
gptkbp:aircraft_role
|
passenger transport
|
|
gptkbp:aspect_ratio
|
7.5
|
|
gptkbp:cargo_capacity
|
3,000 lb
|
|
gptkbp:cockpit
|
two-pilot cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:cruise_speed
|
500 mph
|
|
gptkbp:design
|
low-wing
|
|
gptkbp:engine_type
|
gptkb:Pratt_&_Whitney_JT8_D
twin-engine
|
|
gptkbp:first_delivery
|
gptkb:1966
gptkb:1982
|
|
gptkbp:first_flight
|
2000s
1965-01-25
|
|
gptkbp:fuel_capacity
|
5,000 lb
|
|
gptkbp:fuselage_material
|
3.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Douglas DC-9-30
|
|
gptkbp:introduced
|
gptkb:1965
|
|
gptkbp:landing_distance
|
5,000 ft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
27.0 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:max_speed
|
550 mph
|
|
gptkbp:max_takeoff_weight
|
60,000 lb
|
|
gptkbp:notable_case
|
various incidents during service
|
|
gptkbp:number_built
|
976
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_history
|
commercial aviation
|
|
gptkbp:passenger_capacity
|
90 to 130
|
|
gptkbp:payload_capacity
|
20,000 lb
|
|
gptkbp:primary_user
|
gptkb:Delta_Air_Lines
gptkb:Alaska_Airlines
gptkb:Continental_Airlines
gptkb:Northwest_Airlines
|
|
gptkbp:production_years
|
1965 to 1982
|
|
gptkbp:range
|
2,000 miles
1,500 miles
|
|
gptkbp:related_aircraft
|
gptkb:DC-9_family
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:seating_capacity
|
100 passengers
130 passengers
|
|
gptkbp:service_ceiling
|
35,000 ft
|
|
gptkbp:service_entry
|
gptkb:1966
|
|
gptkbp:stall_speed
|
120 knots
|
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_MD-80
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
6,000 ft
|
|
gptkbp:variant
|
gptkb:Douglas_DC-9
|
|
gptkbp:wing_area
|
1,800 ft²
|
|
gptkbp:wingspan
|
28.4 m
|
|
gptkbp:bfsParent
|
gptkb:Piedmont_Airlines
|
|
gptkbp:bfsLayer
|
5
|