|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas_MD-90-30
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Mc_Donnell_Douglas_MD-80_family
passenger transport
narrow-body
low-wing
|
|
gptkbp:airlines
|
gptkb:Delta_Air_Lines
|
|
gptkbp:aspect_ratio
|
8.5
|
|
gptkbp:avionics
|
modern digital cockpit
|
|
gptkbp:certification
|
TC 7 A1
|
|
gptkbp:crew
|
2
2 pilots
|
|
gptkbp:decommissioned
|
2000s
|
|
gptkbp:design
|
gptkb:engine
|
|
gptkbp:elevation
|
35,000 feet
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
1993-04-30
|
|
gptkbp:fuel_capacity
|
6,500 gallons
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
MD-90-30 ER
|
|
gptkbp:introduced
|
gptkb:1995
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
38.1 meters
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:market_segment
|
domestic and regional flights
|
|
gptkbp:material
|
3.5 meters
|
|
gptkbp:max_speed
|
Mach 0.82
|
|
gptkbp:max_takeoff_weight
|
65,000 pounds
75,000 pounds
|
|
gptkbp:number_built
|
116
|
|
gptkbp:operational_range
|
2,000 to 2,500 nautical miles
|
|
gptkbp:production_years
|
1993 to 2000
|
|
gptkbp:propulsion
|
18,500 lbf
|
|
gptkbp:range
|
2,500 nautical miles
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:safety_features
|
high
|
|
gptkbp:seating_capacity
|
153
20,000 pounds
130 to 150 passengers
|
|
gptkbp:service_ceiling
|
37,000 feet
|
|
gptkbp:speed
|
450 knots
Mach 0.78
|
|
gptkbp:successor
|
gptkb:MD-95
|
|
gptkbp:surface
|
elevators, ailerons, rudder
|
|
gptkbp:variant
|
gptkb:Mc_Donnell_Douglas_MD-90
|
|
gptkbp:wing_area
|
1,200 square feet
|
|
gptkbp:wingspan
|
32.9 meters
|