|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas_DC-9-10
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:DC-9_family
narrow-body aircraft
|
|
gptkbp:aspect_ratio
|
7.5
|
|
gptkbp:cockpit
|
two-pilot cockpit
|
|
gptkbp:crew
|
2 pilots
|
|
gptkbp:decommissioned
|
gptkb:2006
|
|
gptkbp:design
|
short to medium-haul airliner
|
|
gptkbp:elevation
|
31,000 ft
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney
2
|
|
gptkbp:engine_type
|
turbofan
J T8 D
|
|
gptkbp:financial_performance
|
T-tail
conventional tail
|
|
gptkbp:first_flight
|
gptkb:2006
1965-02-25
|
|
gptkbp:first_released
|
gptkb:1965
gptkb:1972
|
|
gptkbp:flaps
|
slotted flaps
|
|
gptkbp:fuel_capacity
|
5,000 lb
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DC-9-10 Series
|
|
gptkbp:introduced
|
gptkb:1965
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
28.35 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:material
|
3.35 m
|
|
gptkbp:max_takeoff_weight
|
6,000 ft
5,000 ft
54,000 lb
|
|
gptkbp:operational_range
|
domestic and regional flights
|
|
gptkbp:primary_user
|
gptkb:Delta_Air_Lines
gptkb:United_Airlines
gptkb:Alaska_Airlines
gptkb:Northwest_Airlines
|
|
gptkbp:produced_by
|
gptkb:30
|
|
gptkbp:production_years
|
1965 to 1972
|
|
gptkbp:range
|
1,500 nautical miles
1,500 miles
|
|
gptkbp:retired
|
gptkb:2006
|
|
gptkbp:seating_capacity
|
15,000 lb
80 to 100 passengers
|
|
gptkbp:service_ceiling
|
31,000 ft
|
|
gptkbp:speed
|
500 knots
0.8 Mach
|
|
gptkbp:successor
|
gptkb:DC-9-30_Series
|
|
gptkbp:tail_type
|
N1000
|
|
gptkbp:variant
|
gptkb:DC-9
|
|
gptkbp:wing_area
|
1,800 ft²
|
|
gptkbp:wingspan
|
28.35 m
|