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gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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general aviation
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gptkbp:average_temperature
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up to 1,000 ° C
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gptkbp:compression_ratio
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8:1
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gptkbp:controls
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gptkb:full_authority_digital_engine_control_(FADEC)
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gptkbp:cooling_system
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air-cooled
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gptkbp:diameter
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1,000 mm
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gptkbp:drivetrain
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reduction gearbox
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gptkbp:emissions_standard
|
mixed flow
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gptkbp:engine
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twin-shaft
up to 5,000 hours
turbine cycle
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gptkbp:engine_type
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turboprop
P T6 A-20
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gptkbp:features
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modular design
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gptkbp:first_flight
|
gptkb:1963
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gptkbp:fuel_capacity
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1,000 mm
1,200 mm
1,500 mm
400 lb
approximately 0.5 lb/hp/hr
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gptkbp:fuel_type
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Jet A or Jet A-1
dual fuel system
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|
https://www.w3.org/2000/01/rdf-schema#label
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PT6 A-20
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gptkbp:ignition_system
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dual ignition
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gptkbp:launch_site
|
electric starter
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gptkbp:length
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1,500 mm
|
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gptkbp:maintenance
|
1,500 hours
|
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gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
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gptkbp:max_takeoff_weight
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1,200 shp
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gptkbp:notable_users
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gptkb:Cessna
gptkb:De_Havilland_Canada
gptkb:Beechcraft
gptkb:Dornier
gptkb:Piper
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gptkbp:number_of_stages
|
2
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gptkbp:power_output
|
1,100 to 1,200 shp
|
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gptkbp:powers
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1,200 shp
|
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gptkbp:propulsion
|
1.8 m
variable pitch
2.75:1
|
|
gptkbp:service_ceiling
|
25,000 ft
|
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gptkbp:setting
|
free turbine
|
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gptkbp:speed
|
2,000 rpm
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gptkbp:type
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gptkb:engine
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|
gptkbp:weight
|
approximately 400 lb
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