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gptkbp:instance_of
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gptkb:helicopter
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gptkbp:armament
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gptkb:none
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gptkbp:avionics
|
modern avionics suite
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|
gptkbp:climb_rate
|
8 m/s
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gptkbp:cockpit
|
glass cockpit
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gptkbp:combat_role
|
transport and reconnaissance
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gptkbp:configuration
|
tandem rotor
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gptkbp:country_of_origin
|
gptkb:China
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gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
twin-engine
Harbin Aircraft Design Institute
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gptkbp:design_features
|
compact design
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gptkbp:development
|
gptkb:2003
1990s
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gptkbp:diameter
|
10.7 m
fenestron tail rotor
two-blade main rotor
|
|
gptkbp:engine
|
WZ-8 A
|
|
gptkbp:first_flight
|
gptkb:2003
|
|
gptkbp:fuel_capacity
|
600 L
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gptkbp:height
|
3.4 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Z-11 helicopter
|
|
gptkbp:influences
|
gptkb:Eurocopter_EC120
|
|
gptkbp:introduced
|
gptkb:2003
|
|
gptkbp:landing_distance
|
400 m
|
|
gptkbp:length
|
12.8 m
|
|
gptkbp:manufacturer
|
gptkb:Harbin_Aircraft_Manufacturing_Corporation
|
|
gptkbp:market
|
domestic and international
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
2,600 kg
|
|
gptkbp:military_operations
|
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:navigation_system
|
gptkb:GPS
|
|
gptkbp:notable_case
|
none reported
|
|
gptkbp:number_built
|
over 100
|
|
gptkbp:operational_history
|
used in various missions
|
|
gptkbp:operational_range
|
300 km
|
|
gptkbp:operational_use
|
gptkb:2005
|
|
gptkbp:operator
|
various civilian operators
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:payload_capacity
|
1,000 kg
|
|
gptkbp:performance
|
high performance for its class
|
|
gptkbp:primary_user
|
gptkb:China
|
|
gptkbp:production_years
|
gptkb:2003
ongoing
|
|
gptkbp:range
|
600 km
|
|
gptkbp:related_aircraft
|
gptkb:Z-9_helicopter
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:safety_features
|
crashworthy design
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:Z-19_helicopter
|
|
gptkbp:takeoff_distance
|
500 m
|
|
gptkbp:type
|
civil and military use
|
|
gptkbp:used_by
|
gptkb:People's_Liberation_Army
|
|
gptkbp:variant
|
Z-11 D
Z-11 W
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:AVIC_Helicopter
|
|
gptkbp:bfsLayer
|
7
|