|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
aircraft
|
|
gptkbp:compressionRatio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
approximately 2.5 ft
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
gptkb:PT6A-600
gptkb:PT6A-400
gptkb:PT6A-27
gptkb:PT6A-60
gptkb:PT6A-20
gptkb:PT6A-42
gptkb:PT6A-66
gptkb:PT6A-1400
PT6A-34
0.76 m
1.37 m
PT6A-68
PT6A-67
PT6A-1000
PT6A-1100
PT6A-1200
PT6A-1300
PT6A-140
PT6A-150
PT6A-1500
PT6A-160
PT6A-1600
PT6A-1700
PT6A-180
PT6A-1800
PT6A-1900
PT6A-200
PT6A-2000
PT6A-300
PT6A-500
PT6A-700
PT6A-800
PT6A-900
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
4
turbine engine
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
Jet_A_or_Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6A
|
|
gptkbp:length
|
approximately 4.5 ft
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
75 dB
|
|
gptkbp:notableUsers
|
gptkb:Cessna
gptkb:De_Havilland_Canada
gptkb:Pilatus
Beechcraft
|
|
gptkbp:powerOutput
|
600 to 1,800 shp
|
|
gptkbp:propulsion
|
variable pitch
0.5 to 0.6
|
|
gptkbp:related_engine
|
PT6 family
Brayton_cycle
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:weight
|
approximately 300 lb
|