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gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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business aviation
turboprop aircraft
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gptkbp:armament
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gptkb:4
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gptkbp:certification
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FAA certified
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gptkbp:compression_ratio
|
8:1
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gptkbp:controls
|
digital
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gptkbp:cooling_system
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gptkb:engine
air-cooled
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gptkbp:diameter
|
approximately 1.5 ft
|
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gptkbp:drivetrain
|
reduction gearbox
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gptkbp:elevation
|
up to 25,000 ft
|
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gptkbp:emissions_standard
|
low
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gptkbp:engine
|
Brayton cycle
twin-shaft
up to 5,000 hours
small turboprop
P T6 family
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gptkbp:engine_type
|
gptkb:engine
P T6 A-65
|
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gptkbp:features
|
modular design
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gptkbp:first_introduced
|
1960s
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gptkbp:fuel_capacity
|
high
variable
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gptkbp:fuel_type
|
gptkb:Jet_A
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|
https://www.w3.org/2000/01/rdf-schema#label
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PT6 A-65
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gptkbp:launch_site
|
electric starter
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gptkbp:length
|
approximately 4.5 ft
|
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gptkbp:maintenance
|
3,600 hours
|
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gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
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gptkbp:market_segment
|
regional aviation
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gptkbp:max_speed
|
250 knots
|
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gptkbp:noise_level
|
low
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gptkbp:operational_area
|
commercial aviation
|
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gptkbp:power_output
|
1,100 shp
|
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gptkbp:propulsion
|
high
constant speed
1,100 lbf
|
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gptkbp:reliability
|
high
|
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gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:setting
|
free turbine
|
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gptkbp:type
|
turbo-prop engine
|
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gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:weight
|
approximately 400 lb
|