PT6 A engine

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:aircraft_operated gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:Beechcraft_King_Air
gptkbp:application general aviation
gptkbp:compression_ratio 8.5:1
gptkbp:configuration free turbine
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:design_feature high durability
modular design
easy maintenance
low operating costs
versatile applications
gptkbp:elevation up to 30,000 feet
gptkbp:emissions_standard low
gptkbp:engine Brayton cycle
gptkbp:first_introduced gptkb:1963
gptkbp:fuel_economy good
gptkbp:fuel_type Jet A or Jet A-1
gptkbp:global_presence used worldwide
gptkbp:governor gptkb:electronic
gptkbp:historical_significance proven track record
widely used since the 1960s
https://www.w3.org/2000/01/rdf-schema#label PT6 A engine
gptkbp:is_often_used_in gptkb:transport_aircraft
gptkb:military_aircraft
gptkb:business_jet
regional airliners
gptkbp:launch_platform electric starter
gptkbp:maintenance 1,500 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney_Canada
gptkbp:market_segment commercial aviation market
general aviation market
military aviation market
business aviation market
gptkbp:network extensive
gptkbp:noise_level moderate
gptkbp:power_output 600 to 1,800 shp
gptkbp:propeller variable pitch
gptkbp:propulsion low
high
gptkbp:reliability high
gptkbp:service_ceiling 25,000 feet
gptkbp:training_programs available for operators
gptkbp:type turbo-prop engine
gptkbp:used_in gptkb:aircraft
gptkbp:variant gptkb:PT6_A-60
PT6 A-67
PT6 A-34
gptkbp:weight approximately 300 lb
gptkbp:bfsParent gptkb:Pratt_&_Whitney_Canada
gptkbp:bfsLayer 6