|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
two-class configuration
|
|
gptkbp:aircraft_operated
|
wide-body aircraft
|
|
gptkbp:aircraft_role
|
passenger and cargo transport
|
|
gptkbp:capacity
|
280 passengers
|
|
gptkbp:cargo_capacity
|
120 m³
|
|
gptkbp:cargo_types
|
large cargo door
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:crew
|
2 pilots
|
|
gptkbp:cruise_speed
|
850 km/h
|
|
gptkbp:decommissioned
|
gptkb:2016
|
|
gptkbp:design
|
Airbus engineers
|
|
gptkbp:design_feature
|
high-wing design
|
|
gptkbp:engine_type
|
gptkb:General_Electric_CF6-80_A
turbofan
|
|
gptkbp:first_delivery
|
1983-01-01
|
|
gptkbp:first_flight
|
2016-12-31
1982-04-03
|
|
gptkbp:fuel_capacity
|
40,000 L
|
|
gptkbp:fuselage_material
|
aluminum alloy
5.64 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Airbus A310-200 ST
|
|
gptkbp:landing_distance
|
250 km/h
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
46.66 m
|
|
gptkbp:manufacturer
|
gptkb:Airbus
|
|
gptkbp:max_speed
|
900 km/h
|
|
gptkbp:max_takeoff_weight
|
140,000 kg
|
|
gptkbp:number_built
|
gptkb:255
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:offers_certificate
|
gptkb:EASA
|
|
gptkbp:operational_cost
|
low
|
|
gptkbp:operational_history
|
used by various airlines globally.
|
|
gptkbp:operational_range
|
8,000 km
|
|
gptkbp:orbital_altitude
|
12,000 m
10,000 m
|
|
gptkbp:payload_capacity
|
40,000 kg
|
|
gptkbp:primary_user
|
gptkb:Air_Transat
|
|
gptkbp:production_years
|
1982-1998
|
|
gptkbp:range
|
9,600 km
|
|
gptkbp:related_aircraft
|
gptkb:Airbus_A310_family
|
|
gptkbp:role
|
gptkb:transport_aircraft
|
|
gptkbp:seating_capacity
|
240 passengers
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:successor
|
gptkb:Airbus
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
280 km/h
|
|
gptkbp:variant
|
gptkb:Airbus
|
|
gptkbp:wing_area
|
122.6 m²
|
|
gptkbp:wing_configuration
|
swept wing
|
|
gptkbp:wingspan
|
43.88 m
|
|
gptkbp:bfsParent
|
gptkb:Daimler_Chrysler_Aerospace_AG
|
|
gptkbp:bfsLayer
|
5
|