|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
general aviation
|
|
gptkbp:certifications
|
FAA_certified
|
|
gptkbp:climate
|
up to 900 °F
|
|
gptkbp:compressionRatio
|
8.5:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
electric starter
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
approximately 1.5 ft
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
meets current standards
|
|
gptkbp:engine
|
horizontal layout
|
|
gptkbp:engineType
|
6
high
axial compressor
single-stage turbine
PT6A-67
|
|
gptkbp:exhaustSystem
|
single exhaust
|
|
gptkbp:firstRace
|
1963
|
|
gptkbp:fuel_capacity
|
highly efficient
approximately 0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
Jet A
reverse flow
|
|
gptkbp:historicalEvent
|
evolved from earlier PT6 models
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT6A-600
|
|
gptkbp:is_used_in
|
aircraft
|
|
gptkbp:length
|
approximately 4.5 ft
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:market
|
widely used globally
|
|
gptkbp:market_segment
|
regional aviation
|
|
gptkbp:maximum_speed
|
250 knots
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Cessna
gptkb:Bombardier
Piper
Beechcraft
Dornier
|
|
gptkbp:operational_status
|
commercial and military
|
|
gptkbp:performances
|
up to 5,000 hours
|
|
gptkbp:powerOutput
|
600 shp
|
|
gptkbp:propulsion
|
2.0 hp/lb
600 lbf
|
|
gptkbp:related_engine
|
PT6 family
Brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:weight
|
approximately 300 lb
|