Pratt & Whitney PT6A-114A

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instanceOf turboprop engine
gptkbp:application aircraft
gptkbp:climate up to 1,200 °F
gptkbp:community large user community
gptkbp:compressionRatio 12:1
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:coolingSystem air-cooled
gptkbp:diameter approximately 1.5 ft
gptkbp:engine advanced technology
modular design
rear-mounted
regional aviation
turbine engine design
gptkbp:engineConfiguration continuous development
gptkbp:engineType 4
turboprop
free turbine
centrifugal
global support network
starter-generator
gptkbp:exhaustSystem axial
gptkbp:fuel_capacity approximately 40-50 gal/hr
gptkbp:fuelType Jet A
dual ignition system
dual fuel pumps
gptkbp:hasArea FAA_certified
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney PT6A-114A
gptkbp:launchDate 1960s
gptkbp:length approximately 4.5 ft
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:noise_level low noise
gptkbp:notable_feature PT6A-114
gptkbp:notableFeature gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:De_Havilland_Canada_DHC-6_Twin_Otter
Beechcraft 1900
Dornier 228
gptkbp:operationalHistory long history of service
gptkbp:operationalRange up to 1,500 miles
gptkbp:performances high reliability
high efficiency
easy maintenance
up to 10,000 hours
excellent performance
gptkbp:powerOutput 600 shp
gptkbp:powers 1.0 hp/lb
gptkbp:propulsion constant speed
up to 5.5 ft
up to 600 lbf
gptkbp:service_ceiling 25,000 ft
gptkbp:setting twin-shaft
gptkbp:updates various modifications available
gptkbp:weight approximately 300 lb