|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single aisle
|
|
gptkbp:aircraft_operated
|
27 ft
narrow-body
60,000 lb
93 ft
124 ft
|
|
gptkbp:aircraft_role
|
gptkb:Flight
|
|
gptkbp:aircraft_type
|
gptkb:aircraft
|
|
gptkbp:built
|
gptkb:100
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mc_Donnell_Douglas
final design
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:engine_type
|
turbofan
PW-100
|
|
gptkbp:first_delivery
|
1995-06-01
2000-12-01
|
|
gptkbp:first_flight
|
1993-01-16
|
|
gptkbp:fuel_capacity
|
5,000 L
|
|
gptkbp:fuselage_material
|
3.5 m
|
|
gptkbp:height
|
8.4 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas MD-95
|
|
gptkbp:landing_distance
|
130 knots
67,000 lb
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
38.1 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:max_speed
|
0.78 Mach
|
|
gptkbp:max_takeoff_weight
|
75,000 lb
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
2,500 km
|
|
gptkbp:orbital_altitude
|
35,000 ft
|
|
gptkbp:passenger_capacity
|
142
|
|
gptkbp:payload_capacity
|
15,000 lb
|
|
gptkbp:primary_user
|
gptkb:Delta_Air_Lines
|
|
gptkbp:production_years
|
1995-2000
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:related_aircraft
|
gptkb:Mc_Donnell_Douglas_MD_family
|
|
gptkbp:release_date
|
1993-10-01
|
|
gptkbp:retired
|
gptkb:2000
|
|
gptkbp:service_ceiling
|
37,000 ft
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:status
|
out of production
|
|
gptkbp:successor
|
gptkb:Bombardier_CRJ-900
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
140 knots
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
gptkb:Mc_Donnell_Douglas_MD-90
|
|
gptkbp:wing_area
|
120 m²
|
|
gptkbp:wing_configuration
|
low-wing
|
|
gptkbp:wingspan
|
28.4 m
|
|
gptkbp:year_established
|
gptkb:1995
|
|
gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:bfsLayer
|
4
|