|
gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
gptkb:Antonov_An-140_family
twin turboprop
civil aircraft
twin-engine turboprop
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:cockpit
|
2
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Antonov_Design_Bureau
regional transport
|
|
gptkbp:developer
|
joint_project_with_Russia
|
|
gptkbp:engine
|
gptkb:Ivchenko_AI-20M
2
|
|
gptkbp:engineType
|
turboprop
|
|
gptkbp:firstFlight
|
1997
|
|
gptkbp:fuelCapacity
|
3,000 L
|
|
gptkbp:height
|
7.5 m
|
|
gptkbp:helicopterCapacity
|
glass cockpit
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Antonov An-140-300
|
|
gptkbp:influencedBy
|
gptkb:Antonov_An-24
|
|
gptkbp:introduced
|
2001
|
|
gptkbp:landingGear
|
tricycle type
|
|
gptkbp:length
|
22.7 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:market
|
regional aviation market
|
|
gptkbp:maximumDepth
|
4,000 kg
7,600 m
|
|
gptkbp:maxSpeed
|
550 km/h
|
|
gptkbp:maxTakeoffWeight
|
12,000 kg
|
|
gptkbp:modifications
|
various cargo and passenger configurations
|
|
gptkbp:notableFeature
|
2001
high-wing design
|
|
gptkbp:numberBuilt
|
over 20
|
|
gptkbp:operationalHistory
|
used in various countries
|
|
gptkbp:operationalRange
|
2,500 km
|
|
gptkbp:passengerCapacity
|
52
5,000 kg
|
|
gptkbp:primaryUser
|
gptkb:Ukrainian_Air_Force
|
|
gptkbp:productionCompany
|
1997-2005
|
|
gptkbp:productionLocation
|
gptkb:Ukraine
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:relatedAircraft
|
gptkb:Antonov_An-148
|
|
gptkbp:role
|
regional airliner
|
|
gptkbp:safetyFeatures
|
good
|
|
gptkbp:services
|
7,600 m
|
|
gptkbp:speed
|
500 km/h
|
|
gptkbp:status
|
in service
|
|
gptkbp:takeoffDistance
|
1,200 m
1,000 m
|
|
gptkbp:variant
|
gptkb:Antonov_An-140
|
|
gptkbp:wingArea
|
60 m²
|
|
gptkbp:wingspan
|
21.0 m
|