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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single aisle
|
|
gptkbp:aircraft_operated
|
10.5 m
commercial aviation
0.78 Mach
38.1 m
50,000 lb
|
|
gptkbp:aircraft_role
|
gptkb:Flight
|
|
gptkbp:aircraft_type
|
narrow-body airliner
|
|
gptkbp:cargo_capacity
|
1,500 kg
|
|
gptkbp:climb_rate
|
2,500 ft/min
|
|
gptkbp:crew
|
2
2 pilots
|
|
gptkbp:design
|
Mc Donnell Douglas engineers
|
|
gptkbp:difficulty
|
2,500 nautical miles
|
|
gptkbp:engine_type
|
gptkb:Pratt_&_Whitney_PW_1000_G
turbofan
|
|
gptkbp:first_delivery
|
1999-06-30
|
|
gptkbp:first_flight
|
2006-12-31
1998-01-16
|
|
gptkbp:flight_deck
|
glass cockpit
|
|
gptkbp:fuel_capacity
|
6,500 US gallons
|
|
gptkbp:fuselage_material
|
3.5 m
|
|
gptkbp:height
|
10.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mc Donnell Douglas MD-95-30
|
|
gptkbp:introduced
|
gptkb:1999
|
|
gptkbp:landing_distance
|
67,000 lb
|
|
gptkbp:landing_gear
|
tricycle type
|
|
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:nickname
|
gptkb:MD-95
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_cost
|
$3,500 per hour
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:passenger_capacity
|
142
|
|
gptkbp:primary_user
|
gptkb:Air_Tran_Airways
|
|
gptkbp:produces
|
173
|
|
gptkbp:production_years
|
1995-2000
|
|
gptkbp:range
|
2,500 nautical miles
|
|
gptkbp:related_aircraft
|
gptkb:Mc_Donnell_Douglas_MD_family
|
|
gptkbp:retired
|
gptkb:2006
|
|
gptkbp:roll_rate
|
3.0°/s
|
|
gptkbp:safety_rating
|
gptkb:5_stars
|
|
gptkbp:service_ceiling
|
37,000 ft
|
|
gptkbp:stall_speed
|
120 knots
|
|
gptkbp:successor
|
gptkb:Bombardier_CRJ-900
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Mc_Donnell_Douglas_MD-95
|
|
gptkbp:wing_area
|
1,200 ft²
|
|
gptkbp:wing_configuration
|
low-wing
|
|
gptkbp:wingspan
|
28.4 m
|
|
gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:bfsLayer
|
4
|