gptkbp:instance_of
|
gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:Mc_Donnell_Douglas_DC_family
narrow-body aircraft
single aisle
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gptkbp:crew
|
2
|
gptkbp:design
|
low-wing monoplane
Mc Donnell Douglas engineers
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gptkbp:engine
|
2
Pratt & Whitney J T8 D
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gptkbp:engine_type
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twin-engine
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gptkbp:first_flight
|
gptkb:2006
February 25, 1965
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gptkbp:fuel_capacity
|
5,000 liters
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gptkbp:height
|
7.87 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas DC-9 family
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gptkbp:introduced
|
gptkb:1965
|
gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
28.35 m
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gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
gptkbp:marketed_as
|
gptkb:DC-9
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gptkbp:max_speed
|
Mach 0.84
|
gptkbp:max_takeoff_weight
|
60,000 lb
55,000 lb
|
gptkbp:notable_event
|
several accidents and incidents during service
|
gptkbp:operational_history
|
used in passenger and cargo transport
|
gptkbp:operational_range
|
short to medium-haul
|
gptkbp:primary_user
|
gptkb:American_Airlines
gptkb:Delta_Air_Lines
gptkb:United_Airlines
gptkb:Alaska_Airlines
gptkb:Northwest_Airlines
|
gptkbp:produced_by
|
gptkb:battle
976
|
gptkbp:range
|
1,500 miles
|
gptkbp:retired
|
gptkb:2006
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:seating_capacity
|
up to 139
|
gptkbp:service_ceiling
|
35,000 ft
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_MD-80
|
gptkbp:variant
|
gptkb:DC-9-20
gptkb:DC-9-10
gptkb:DC-9-30
gptkb:DC-9-40
gptkb:DC-9-50
|
gptkbp:wing_area
|
120 m²
|
gptkbp:wingspan
|
28.35 m
|
gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas_MD-80_series
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gptkbp:bfsLayer
|
4
|