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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:aircraft_operated
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gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:Beechcraft_King_Air_200
gptkb:Dornier_228
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gptkbp:application
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gptkb:aircraft
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gptkbp:certification
|
FAA certified
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gptkbp:compression_ratio
|
8:1
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gptkbp:compressor_type
|
axial compressor
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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
|
16.5 in
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|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
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gptkbp:engine
|
gptkb:PT6_A
starter-generator
civil and military aircraft
widely used in general aviation.
TBO of 3,600 hours
in production since 1980
|
|
gptkbp:engine_configuration
|
modular design
twin-shaft turboprop
|
|
gptkbp:engine_monitoring_system
|
digital engine monitoring system
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_type
|
gptkb:PT6_A-60
turboprop
PT6 A-60 A, PT6 A-60 C
|
|
gptkbp:first_introduced
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
300 lb
16.5 in
45.5 in
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical fuel control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6 A-60 A
|
|
gptkbp:ignition_system
|
dual spark ignition
|
|
gptkbp:length
|
45.5 in
|
|
gptkbp:maintenance
|
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:max_takeoff_weight
|
1,200 shp
|
|
gptkbp:maximum_continuous_power
|
1,100 shp
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:power_output
|
1,100 shp
|
|
gptkbp:propeller
|
gptkb:4
4.5 ft
variable pitch propeller
|
|
gptkbp:propulsion
|
1,200 lb
3.67 hp/lb
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:torque
|
dry sump
|
|
gptkbp:turbine_type
|
free turbine
|
|
gptkbp:weight
|
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:King_Air_350i
|
|
gptkbp:bfsLayer
|
7
|