Statements (54)
Predicate | Object |
---|---|
gptkbp:instanceOf |
turboprop engine
|
gptkbp:application |
aircraft
|
gptkbp:certifications |
FAA_certified
|
gptkbp:climate |
up to 1,200 °F
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:design |
geared turboprop
|
gptkbp:design_feature |
modular design
|
gptkbp:emissionsStandard |
low emissions
|
gptkbp:engine |
approximately 2.5 ft
versatile applications approximately 3.5 ft approximately 1.5 ft |
gptkbp:engineConfiguration |
horizontal installation
|
gptkbp:engineType |
turboprop
free turbine axial compressor |
gptkbp:firstFlight |
1963
|
gptkbp:fuel_capacity |
approximately 0.5 lb/hp/hr
|
gptkbp:fuelType |
Jet A
dual ignition system electronic fuel control |
gptkbp:hasArea |
extensively tested
|
https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney PT6A
|
gptkbp:launchSite |
starter-generator
|
gptkbp:maintenance |
1,500 hours
|
gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
gptkbp:noise_level |
low noise level
|
gptkbp:notable_feature |
gptkb:PT6A-27
gptkb:PT6A-60 gptkb:PT6A-20 gptkb:PT6A-42 PT6A-34 |
gptkbp:notableUsers |
gptkb:Pilatus_Aircraft
gptkb:De_Havilland_Canada gptkb:Cessna_Aircraft_Company Beechcraft |
gptkbp:number_of_stages |
6 stages
|
gptkbp:operationalHistory |
used in military applications
used in commercial aviation widely used in general aviation |
gptkbp:operationalRange |
up to 30,000 ft
|
gptkbp:performances |
high performance
high efficiency up to 5,000 hours proven reliability popular among operators every 3,600 hours |
gptkbp:powerOutput |
600 to 1,800 shp
|
gptkbp:propulsion |
2.5:1
up to 1,800 lb |
gptkbp:reliability |
high reliability
|
gptkbp:setting |
twin-shaft
|
gptkbp:warranty |
up to 5 years
|
gptkbp:weight |
approximately 300 lb
|