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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
|
general aviation
|
|
gptkbp:armament
|
gptkb:4
|
|
gptkbp:average_temperature
|
up to 900 ° C
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gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
8:1
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gptkbp:configuration
|
twin-shaft
|
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gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
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gptkbp:cooling_system
|
air-cooled
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|
gptkbp:diameter
|
0.5 m
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gptkbp:emissions_standard
|
meets ICAO standards
|
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gptkbp:engine
|
gptkb:PT6_A_series
military and civilian aircraft
Brayton cycle
global support network
available upgrades
long history of service
versatile engine
continuously developed
electronic starter
|
|
gptkbp:engine_configuration
|
modular design
horizontally opposed
detailed specifications available
|
|
gptkbp:engine_power
|
high performance
very reliable
2000 RPM
up to 5000 hours
|
|
gptkbp:engine_type
|
turboprop
PT6 A-28, PT6 A-34
|
|
gptkbp:first_introduced
|
1960s
|
|
gptkbp:fuel_economy
|
approximately 200 lb/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel pumps
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6 A-27
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
2000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:market_segment
|
regional aviation
|
|
gptkbp:noise_level
|
low noise operation
|
|
gptkbp:notable_applications
|
gptkb:Beechcraft_King_Air
|
|
gptkbp:notable_features
|
high reliability
|
|
gptkbp:operational_range
|
up to 25,000 feet
|
|
gptkbp:power_output
|
600 shp
|
|
gptkbp:propulsion
|
600 lbf
4.0 shp/kg
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:weight
|
approximately 150 kg
|
|
gptkbp:bfsParent
|
gptkb:DHC-6-200
gptkb:DHC-6-300
|
|
gptkbp:bfsLayer
|
6
|