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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:Piper_Navajo
gptkb:Beechcraft_King_Air
gptkb:Dornier_228
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gptkbp:application
|
general aviation aircraft
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gptkbp:certification
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FAA certified
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gptkbp:compressor_type
|
axial compressor
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gptkbp:configuration
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twin-shaft
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
electronic control unit
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gptkbp:cooling_system
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air-cooled
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gptkbp:diameter
|
approximately 14 in
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gptkbp:emissions_standard
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low emissions
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gptkbp:engine
|
military and civilian aircraft
global support network
upgrade options available
readily available parts
air start or electric start
part of PT6 family
|
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gptkbp:engine_configuration
|
modular design
horizontally opposed
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gptkbp:engine_power
|
high performance
high reliability
high thermal efficiency
widely used engine
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gptkbp:engine_type
|
turboprop
multiple variants available
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gptkbp:first_flight
|
gptkb:1963
|
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gptkbp:fuel_capacity
|
1.22 m
0.36 m
0.61 m
|
|
gptkbp:fuel_economy
|
approximately 30-40 gal/hr
|
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gptkbp:fuel_type
|
Jet A or Jet A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6 A-34
|
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gptkbp:ignition_system
|
dual ignition
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gptkbp:is_tested_for
|
extensively tested
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gptkbp:length
|
approximately 48 in
|
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gptkbp:maintenance
|
1,500 hours
easy maintenance access
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gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
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gptkbp:noise_level
|
low noise level
|
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gptkbp:number_of_engines
|
gptkb:6
|
|
gptkbp:power_output
|
600 to 1,000 shp
|
|
gptkbp:propeller
|
variable pitch propeller
up to 5 ft 6 in
|
|
gptkbp:propulsion
|
up to 1,000 lb
2.0:1
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:torque
|
dry sump
|
|
gptkbp:turbine_type
|
free turbine
|
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gptkbp:warranty
|
warranty options available
|
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gptkbp:weight
|
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:DHC-6_Series_400
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gptkbp:bfsLayer
|
6
|