|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:6
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:configuration
|
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:diameter
|
approximately 16 inches
|
|
gptkbp:displacement
|
1,100 cubic inches
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
gptkb:transport_aircraft
gptkb:PT6_family
Brayton cycle
|
|
gptkbp:engine_configuration
|
high performance design
|
|
gptkbp:engine_type
|
gptkb:PT6_A-60
gptkb:PT6_A-65
gptkb:PT6_A-66
turboprop
PT6 A-67
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_capacity
|
lightweight
short length
compact diameter
|
|
gptkbp:fuel_economy
|
high fuel efficiency
approximately 400 lbs/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
electronic fuel control
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney PT6 A-68
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:length
|
approximately 48 inches
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_applications
|
business aviation
|
|
gptkbp:power_output
|
1,100 shp
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:propulsion
|
high thrust-to-weight ratio
1,100 lbf
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
25,000 feet
|
|
gptkbp:turbine_type
|
free turbine
|
|
gptkbp:weight
|
approximately 300 lbs
|
|
gptkbp:bfsParent
|
gptkb:A-29_Super_Tucano
gptkb:T-6_Texan_II
|
|
gptkbp:bfsLayer
|
4
|