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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:transport_aircraft
gptkb:aircraft
gptkb:military_aircraft
business aviation
regional airliners
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gptkbp:armament
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gptkb:4
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gptkbp:certification
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FAA certified
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gptkbp:compression_ratio
|
8:1
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gptkbp:configuration
|
free turbine
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
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gptkbp:cooling_system
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gptkb:oil
air-cooled
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gptkbp:design_features
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advanced aerodynamics
lightweight construction
modular design
high reliability
high power-to-weight ratio
high efficiency
easy maintenance
low operating costs
versatile applications
robust performance
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gptkbp:diameter
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0.5 m
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gptkbp:emissions_standard
|
low
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gptkbp:engine
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Brayton cycle
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gptkbp:engine_configuration
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pylon-mounted
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gptkbp:engine_type
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multi-role engine
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gptkbp:first_flight
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gptkb:1963
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gptkbp:fuel_economy
|
0.5 lb/hp/hr
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gptkbp:fuel_type
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gptkb:Jet_A
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gptkbp:gearbox
|
reduction gearbox
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|
https://www.w3.org/2000/01/rdf-schema#label
|
PT6 A-114 A
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gptkbp:ignition_system
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dual ignition
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gptkbp:launch_platform
|
electric starter
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gptkbp:length
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1.5 m
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gptkbp:maintenance
|
500 hours
|
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gptkbp:manufacturer
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gptkb:Pratt_&_Whitney_Canada
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gptkbp:market_segment
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general aviation
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gptkbp:noise_level
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low
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gptkbp:operational_range
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up to 25,000 feet
|
|
gptkbp:power_output
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600 shp
|
|
gptkbp:propulsion
|
600 lbf
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gptkbp:service
|
up to 10,000 hours
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gptkbp:type
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turbo-prop engine
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gptkbp:water_requirement
|
50-60 lb/hr
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gptkbp:weight
|
150 kg
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gptkbp:bfsParent
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gptkb:Cessna_208
gptkb:Cessna_208_B_Super_Cargomaster
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gptkbp:bfsLayer
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6
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