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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
|
general aviation
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gptkbp:armament
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gptkb:4
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|
gptkbp:average_temperature
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-40 to 50 ° C
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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:compressor_type
|
axial compressor
6 stages
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gptkbp:configuration
|
free turbine
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gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
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gptkb:oil
air-cooled
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gptkbp:diameter
|
0.5 m
|
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gptkbp:emissions_standard
|
low
|
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gptkbp:engine
|
gptkb:PT6_family
Brayton cycle
global support network
available upgrades
technical manuals available
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gptkbp:engine_configuration
|
pylon mounted
twin spool
|
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gptkbp:engine_power
|
5000 hours
|
|
gptkbp:engine_shutdown_time
|
10 seconds
|
|
gptkbp:engine_start_time
|
30 seconds
|
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gptkbp:engine_type
|
gptkb:turbofan_engine
60 series
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_economy
|
high
40 g/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel pumps
|
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gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT6 A-60
|
|
gptkbp:ignition_system
|
dual ignition
|
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gptkbp:launch_window
|
electric starter
|
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gptkbp:length
|
1.5 m
|
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gptkbp:maintenance
|
300 hours
|
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gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:market_segment
|
regional aviation
|
|
gptkbp:max_speed
|
250 knots
|
|
gptkbp:noise_level
|
75 d B
|
|
gptkbp:notable_applications
|
gptkb:business_jet
|
|
gptkbp:operational_range
|
2000 miles
|
|
gptkbp:power_output
|
600 shp
|
|
gptkbp:propeller
|
constant speed
|
|
gptkbp:propulsion
|
4:1
3:1
|
|
gptkbp:reliability
|
high
|
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gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:training
|
pilot training available
|
|
gptkbp:turbine_type
|
2 stages
nickel alloy
single stage turbine
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:warranty
|
3 years
|
|
gptkbp:weight
|
150 kg
200 kg
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PT6_A-68
|
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gptkbp:bfsLayer
|
5
|