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gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:bfsLayer
|
6
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|
gptkbp:bfsParent
|
gptkb:RCAF_Station_St._Hubert
gptkb:CH-124_Sea_King_helicopter
|
|
gptkbp:aircraft_operated
|
gptkb:CH-146_Griffon
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized for improved navigation
|
|
gptkbp:communication
|
advanced radio systems
|
|
gptkbp:country
|
gptkb:none
|
|
gptkbp:crew
|
2
requires a small ground crew for operations
|
|
gptkbp:decommissioned
|
gptkb:2015
|
|
gptkbp:design
|
gptkb:Boeing_Vertol
twin-engine
|
|
gptkbp:engine_type
|
turboshaft
|
|
gptkbp:filmography
|
gptkb:North_America
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
1,500 L
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:historical_significance
|
important part of Canadian military aviation history
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CH-113 Labrador
|
|
gptkbp:legacy
|
served for over four decades in Canadian service
|
|
gptkbp:length
|
16.76 m
|
|
gptkbp:maintenance
|
requires regular maintenance checks
|
|
gptkbp:manufacturer
|
gptkb:aircraft
|
|
gptkbp:material
|
metallic construction
|
|
gptkbp:max_speed
|
260 km/h
|
|
gptkbp:mission
|
transport, search and rescue, medical evacuation
|
|
gptkbp:modifications
|
upgraded for specific missions
|
|
gptkbp:notable_features
|
capable of operating in harsh weather conditions
|
|
gptkbp:number_built
|
approximately 40
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:performance
|
highly versatile and reliable
|
|
gptkbp:primary_user
|
gptkb:Royal_Canadian_Air_Force
gptkb:Canadian_Forces
|
|
gptkbp:propulsion
|
two engines
|
|
gptkbp:related_model
|
CH-113 B
|
|
gptkbp:retirement_year
|
gptkb:2015
|
|
gptkbp:role
|
gptkb:mythological_figure
gptkb:helicopter
|
|
gptkbp:safety_features
|
equipped with flotation devices
|
|
gptkbp:seating_capacity
|
gptkb:12
2,500 kg
|
|
gptkbp:service_ceiling
|
4,600 m
|
|
gptkbp:service_history
|
used in various missions including humanitarian aid
|
|
gptkbp:services
|
gptkb:1971
|
|
gptkbp:setting
|
tandem rotor
|
|
gptkbp:status
|
retired from active service
|
|
gptkbp:successor
|
gptkb:CH-149_Cormorant
|
|
gptkbp:survivability
|
designed for high survivability in combat zones
|
|
gptkbp:training
|
used for pilot training in Canada
|
|
gptkbp:variant
|
CH-113 A
|
|
gptkbp:weight
|
5,400 kg
|
|
gptkbp:wingspan
|
15.24 m
|