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gptkbp:instanceOf
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aircraft
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|
gptkbp:aircraft
|
gptkb:STOL_aircraft
106 kg/m²
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
high-wing monoplane
|
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gptkbp:electrification
|
gptkb:PT6A-20_engine
|
|
gptkbp:engine
|
turboprop engine
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|
gptkbp:firstFlight
|
1959
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gptkbp:fuelCapacity
|
300 L
|
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gptkbp:height
|
4.1 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pilatus PC-6
|
|
gptkbp:landingGear
|
tailwheel
|
|
gptkbp:length
|
12.4 m
|
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gptkbp:manufacturer
|
gptkb:Pilatus_Aircraft
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,200 kg
|
|
gptkbp:notableFeature
|
short takeoff and landing capabilities
versatile utility capabilities
rugged design for rough terrain
|
|
gptkbp:notableOperations
|
gptkb:Royal_Canadian_Air_Force
gptkb:United_Nations
gptkb:United_States_Army
gptkb:Australian_Army
gptkb:Swiss_Air_Force
|
|
gptkbp:numberBuilt
|
over 600
|
|
gptkbp:operationalHistory
|
used in various roles
|
|
gptkbp:passengerCapacity
|
1,200 kg
up to 10
|
|
gptkbp:productionStartYear
|
1959
|
|
gptkbp:productionYears
|
1986
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:services
|
6,000 m
|
|
gptkbp:setting
|
single-engine
|
|
gptkbp:speed
|
65 km/h
200 km/h
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:usedBy
|
military
civil aviation
|
|
gptkbp:variant
|
gptkb:PC-6/Porter
PC-6/Aircraft
PC-6/B2-H4
|
|
gptkbp:wingArea
|
30 m²
|
|
gptkbp:wingspan
|
15.5 m
|