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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
3
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gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Mc_Donnell_Douglas_DC-9-40
gptkb:DC-9_family
gptkb:Mc_Donnell_Douglas_DC-9-30
450 knots
narrow-body aircraft
single aisle
45,000 lb
single aisle configuration
29 ft 0 in
commercial jet airliner
99 ft 10 in
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|
gptkbp:crew
|
2
2 pilots
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|
gptkbp:design
|
final design
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|
gptkbp:engine
|
2
two engines
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|
gptkbp:engine_type
|
turbofan
Pratt & Whitney J T8 D
|
|
gptkbp:first_flight
|
1970-01-01
two-pilot cockpit
|
|
gptkbp:first_released
|
1970-03-01
|
|
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
|
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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
60,000 pounds
65,000 lb
|
|
gptkbp:number_built
|
97
|
|
gptkbp:operational_area
|
passenger transport
|
|
gptkbp:operational_history
|
used by various airlines
|
|
gptkbp:production_years
|
1965-1982
|
|
gptkbp:range
|
2,000 nautical miles
2,000 mi
|
|
gptkbp:retirement_year
|
gptkb:2006
|
|
gptkbp:seating_capacity
|
139
20,000 pounds
1,500 lb
1,500 pounds
139 passengers
|
|
gptkbp:service_ceiling
|
37,000 feet
37,000 ft
|
|
gptkbp:services
|
gptkb:1970
|
|
gptkbp:speed
|
0.74 Mach
|
|
gptkbp:successor
|
gptkb:Mc_Donnell_Douglas_MD-80
|
|
gptkbp:tail_type
|
N12345
|
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gptkbp:variant
|
gptkb:DC-9
|
|
gptkbp:wing_area
|
1,200 ft²
|
|
gptkbp:wingspan
|
28.35 m
93 ft 0 in
|