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gptkbp:instanceOf
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gptkb:helicopter
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gptkbp:aircraft
|
rotorcraft
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gptkbp:armament
|
machine guns
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gptkbp:avionics
|
modern avionics suite
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gptkbp:cockpit
|
glass cockpit
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gptkbp:commissioningDate
|
1990s
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gptkbp:constructionMaterial
|
composite materials
|
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gptkbp:countryOfOrigin
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gptkb:China
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gptkbp:crew
|
2
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gptkbp:design
|
military and civilian use
Chief_Engineer_Zhang
Nanchang_design_team
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gptkbp:developer
|
significant investment
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|
gptkbp:engine
|
WZ-8A
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gptkbp:engineType
|
turboshaft engine
|
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gptkbp:exportedTo
|
several countries
|
|
gptkbp:firstFlight
|
2003
|
|
gptkbp:firstGeneration
|
2005
|
|
gptkbp:fuelCapacity
|
600 L
|
|
gptkbp:futurePlans
|
upgrades and modernization
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|
gptkbp:hasCompetitors
|
gptkb:Bell_206
|
|
gptkbp:height
|
3.4 m
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|
gptkbp:historicalEvent
|
developed from Z-9
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nanchang Z-11
|
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gptkbp:influencedBy
|
gptkb:Eurocopter_AS350
|
|
gptkbp:length
|
12.8 m
|
|
gptkbp:maintenance
|
easy maintenance access
|
|
gptkbp:manufacturer
|
gptkb:Nanchang_Aircraft_Manufacturing_Corporation
|
|
gptkbp:maximumDepth
|
1,100 kg
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,600 kg
|
|
gptkbp:militaryRank
|
Z-11W and Z-11B
aerial work and tourism
|
|
gptkbp:missions
|
fly-by-wire system
|
|
gptkbp:notableFeature
|
high maneuverability
|
|
gptkbp:notableUsers
|
gptkb:Chinese_police
|
|
gptkbp:numberBuilt
|
over 100
|
|
gptkbp:operationalRange
|
600 km
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:participatesIn
|
transport and support
|
|
gptkbp:passengerCapacity
|
5
|
|
gptkbp:performance
|
high performance in various conditions
|
|
gptkbp:primaryUser
|
gptkb:Chinese_military
|
|
gptkbp:productionCompany
|
present
|
|
gptkbp:productionStartYear
|
2003
|
|
gptkbp:propulsion
|
twin-engine configuration
|
|
gptkbp:range
|
600 km
|
|
gptkbp:relatedAircraft
|
gptkb:Z-10
Harbin Z-9
|
|
gptkbp:role
|
utility and reconnaissance
|
|
gptkbp:rotorDiameter
|
11.0 m
|
|
gptkbp:safetyFeatures
|
crashworthy design
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:setting
|
twin-engine
|
|
gptkbp:supportRole
|
pilot training
|
|
gptkbp:takeoffDistance
|
500 m
400 m
|
|
gptkbp:type
|
light utility helicopter
|
|
gptkbp:usedBy
|
gptkb:People's_Liberation_Army
|
|
gptkbp:variant
|
Z-11W
|
|
gptkbp:weight
|
1,500 kg
|