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gptkbp:instanceOf
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turboprop engine
|
|
gptkbp:aircraft
|
gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:De_Havilland_Canada_DHC-6_Twin_Otter
gptkb:Beechcraft_King_Air
Dornier 228
|
|
gptkbp:application
|
general aviation aircraft
|
|
gptkbp:compressionRatio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engineConfiguration
|
free turbine
|
|
gptkbp:engineType
|
4
turboprop
starter-generator
PT6A-34AG
PT6A-34B
PT6A-34D
PT6A-34G
PT6A-34H
PT6A-34K
PT6A-34L
PT6A-34M
PT6A-34P
PT6A-34S
PT6A-34T
PT6A-34U
PT6A-34Y
PT6A-34Z
PT6A-34F
PT6A-34J
PT6A-34N
PT6A-34Q
PT6A-34R
PT6A-34V
PT6A-34W
PT6A-34X
|
|
gptkbp:fanEvents
|
composite
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
50-60 lb/hr
|
|
gptkbp:fuelType
|
Jet_A_or_Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6A-34
|
|
gptkbp:length
|
approximately 48 in
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
75 dB
|
|
gptkbp:operationalRange
|
1,000 nautical miles
|
|
gptkbp:performances
|
up to 5,000 hours
|
|
gptkbp:powerOutput
|
600 to 1,000 shp
|
|
gptkbp:propulsion
|
constant speed
2.0:1
|
|
gptkbp:related_engine
|
PT6A
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:setting
|
twin-shaft
|
|
gptkbp:weight
|
approximately 300 lb
|