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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:MD-90
|
|
gptkbp:aircraft_operated
|
high-mounted wings
|
|
gptkbp:aspect_ratio
|
8.5
|
|
gptkbp:avionics
|
digital avionics
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:competitors
|
gptkb:aircraft
gptkb:Mc_Donnell_Douglas_MD-80
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
2010s
|
|
gptkbp:design
|
low-wing
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
turbofan
Pratt & Whitney P W2000
|
|
gptkbp:first_flight
|
1993-12-30
|
|
gptkbp:first_released
|
1995-03-01
2000-12-31
|
|
gptkbp:flaps
|
slotted flaps
|
|
gptkbp:fuel_capacity
|
20,000 liters
|
|
gptkbp:height
|
10.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
MD-90-30
|
|
gptkbp:introduced
|
gptkb:1995
|
|
gptkbp:landing_gear
|
gptkb:horse_race
|
|
gptkbp:length
|
38.1 meters
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:material
|
3.5 meters
supercritical airfoil
|
|
gptkbp:max_speed
|
850 km/h
|
|
gptkbp:max_takeoff_weight
|
66,000 kg
75,000 kg
|
|
gptkbp:notable_event
|
none reported
|
|
gptkbp:number_built
|
116
|
|
gptkbp:primary_user
|
gptkb:Delta_Air_Lines
|
|
gptkbp:range
|
4,500 km
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:seating_capacity
|
153
15,000 kg
|
|
gptkbp:service_ceiling
|
12,500 meters
|
|
gptkbp:speed
|
780 km/h
|
|
gptkbp:successor
|
gptkb:MD-95
|
|
gptkbp:surface
|
elevators
ailerons
rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
narrow-body airliner
|
|
gptkbp:type_of
|
leading-edge slats
|
|
gptkbp:variant
|
gptkb:MD-90-30_ER
|
|
gptkbp:wing_area
|
120 m²
|
|
gptkbp:wingspan
|
32.9 meters
|