|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
general aviation
|
|
gptkbp:compressionRatio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
oil
air-cooled
|
|
gptkbp:diameter
|
0.5 m
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
gptkb:PT6A-114A
1.8 m
30 seconds
300 lbs
15 seconds
regional aircraft
pylon-mounted
2500 Nm
|
|
gptkbp:engineConfiguration
|
gptkb:Pratt_&_Whitney_Canada
turboprop
twin-shaft
|
|
gptkbp:engineDisplacement
|
0.6 m
|
|
gptkbp:enginePower
|
450 kW
|
|
gptkbp:engineType
|
turbine engine
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuelCapacity
|
40 g/hp/hr
|
|
gptkbp:fuelType
|
Jet A
spark ignition
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT6A-114A
|
|
gptkbp:launchSite
|
electric starter
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:numberOfEpisodes
|
4
|
|
gptkbp:operationalRange
|
up to 25,000 feet
|
|
gptkbp:operationalStatus
|
up to 900 °C
|
|
gptkbp:performances
|
5000 hours
2000 RPM
|
|
gptkbp:powerOutput
|
600 shp
|
|
gptkbp:propulsion
|
constant speed
600 lbf
|
|
gptkbp:related_engine
|
PT6 series
Brayton_cycle
|
|
gptkbp:services
|
30,000 feet
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:torque
|
2000 lb-ft
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:usedIn
|
aircraft
|
|
gptkbp:weight
|
150 kg
|