|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
aircraft
|
|
gptkbp:climate
|
up to 1,200 °F
|
|
gptkbp:compressionRatio
|
9:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
electric starter
|
|
gptkbp:coolingSystem
|
air-cooled
air cooling
|
|
gptkbp:design
|
5,000 hours
|
|
gptkbp:diameter
|
14.5 in
|
|
gptkbp:displacement
|
1,100 cubic inches
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:engine
|
300 lb
aluminum alloy
modular design
gray
rear-mounted
42.5 in
14.5 in
|
|
gptkbp:engineConfiguration
|
single engine
|
|
gptkbp:engineType
|
gptkb:PT6A-27
gptkb:PT6A-60
turboprop
free turbine
PT6A-34
PT6A-21
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuel_capacity
|
high
50-60 lb/hr
|
|
gptkbp:fuelType
|
Jet A
electronic fuel control
dual spark plug
|
|
gptkbp:hasArea
|
FAA_certified
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT6A-20
|
|
gptkbp:length
|
42.5 in
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notableUsers
|
gptkb:Cessna
gptkb:Bombardier
Piper
Beechcraft
Dornier
|
|
gptkbp:operationalRange
|
up to 30,000 ft
|
|
gptkbp:performances
|
field repairable
|
|
gptkbp:powerOutput
|
1,100 shp
|
|
gptkbp:propulsion
|
variable pitch
4 blades
3.67:1
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:setting
|
twin-shaft
|
|
gptkbp:weight
|
300 lb
|