|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:air_support
|
Type Certificate A24 SO
|
|
gptkbp:aircraft_configuration
|
single-aisle
low-wing monoplane
two-class
|
|
gptkbp:aircraft_operated
|
high performance
20 years
narrow-body
modern avionics systems
easy maintenance access
50,000 lb
25 ft 9 in
88 ft 10 in
|
|
gptkbp:aircraft_role
|
passenger transport
|
|
gptkbp:aircraft_type
|
gptkb:aircraft
|
|
gptkbp:control_surfaces
|
elevators, ailerons, rudder
|
|
gptkbp:crew
|
2
|
|
gptkbp:cruise_speed
|
540 mph
|
|
gptkbp:design
|
final design
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:engine_type
|
gptkb:JT8_D
turbofan
|
|
gptkbp:first_delivery
|
gptkb:1967
gptkb:1982
|
|
gptkbp:first_flight
|
1967-01-01
|
|
gptkbp:fuel_capacity
|
5,000 lb
|
|
gptkbp:fuselage_material
|
aluminum alloy
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DC-9-40 Series
|
|
gptkbp:introduced
|
gptkb:1967
|
|
gptkbp:landing_gear
|
gptkb:Cycling
retractable tricycle gear
|
|
gptkbp:length
|
27.4 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:max_speed
|
600 mph
|
|
gptkbp:max_takeoff_weight
|
60,000 lb
|
|
gptkbp:notable_features
|
quiet operation
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:offers_certificate
|
gptkb:FAA
|
|
gptkbp:operational_range
|
2,000 mi
|
|
gptkbp:orbital_altitude
|
30,000 ft
37,000 ft
|
|
gptkbp:passenger_capacity
|
gptkb:100
|
|
gptkbp:payload_capacity
|
20,000 lb
|
|
gptkbp:primary_user
|
airlines
|
|
gptkbp:produces
|
gptkb:100
|
|
gptkbp:production_years
|
1967-1982
|
|
gptkbp:range
|
1,500 mi
2,000 mi
|
|
gptkbp:related_aircraft
|
gptkb:DC-9_family
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:safety_features
|
advanced safety systems
|
|
gptkbp:service_ceiling
|
37,000 ft
|
|
gptkbp:successor
|
gptkb:MD-80_series
|
|
gptkbp:variant
|
gptkb:DC-9
|
|
gptkbp:wing_area
|
1,200 sq ft
|
|
gptkbp:wing_configuration
|
low-wing
swept wing
|
|
gptkbp:wingspan
|
28.4 m
|
|
gptkbp:bfsParent
|
gptkb:DC-9_family
|
|
gptkbp:bfsLayer
|
6
|