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gptkbp:instance_of
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gptkb:turbofan_engine
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|
gptkbp:aircraft_operated
|
gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:De_Havilland_Canada_DHC-6_Twin_Otter
gptkb:Beechcraft_King_Air
gptkb:Dornier_228
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gptkbp:application
|
general aviation
|
|
gptkbp:average_temperature
|
up to 1,200 ° F
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:compressor_type
|
centrifugal compressor
centrifugal
|
|
gptkbp:configuration
|
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_base
|
commercial and military
|
|
gptkbp:design_feature
|
modular design
high power-to-weight ratio
easy maintenance
versatile installation options
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:diameter
|
1,000 mm
600 mm
|
|
gptkbp:emissions_standard
|
low
low emissions
|
|
gptkbp:engine
|
gptkb:PT6_family
Brayton cycle
|
|
gptkbp:engine_power
|
up to 5,000 hours
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_economy
|
high
high fuel efficiency
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel system
|
|
gptkbp:global_presence
|
used worldwide
|
|
gptkbp:has_variations
|
over 20
multiple variants
|
|
gptkbp:history
|
evolved from earlier designs.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6 A
|
|
gptkbp:ignition_system
|
dual ignition system
|
|
gptkbp:length
|
1,200 mm
1,500 mm
|
|
gptkbp:maintenance
|
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:market_position
|
global
widely available
|
|
gptkbp:market_segment
|
gptkb:military_aircraft
business aviation
cargo aviation
regional aviation
|
|
gptkbp:network
|
extensive
extensive support network
|
|
gptkbp:noise_level
|
low
low noise level
|
|
gptkbp:operational_cost
|
low operational cost
|
|
gptkbp:operational_history
|
over 50 years
widely used since 1963
|
|
gptkbp:power_output
|
up to 1,000 hp
500 to 1,000 hp
|
|
gptkbp:produces
|
over 50,000 units
|
|
gptkbp:propeller
|
1.8 m
variable pitch
|
|
gptkbp:propulsion
|
3.3:1
|
|
gptkbp:reliability
|
high
high reliability
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:turbine_type
|
free turbine
|
|
gptkbp:weight
|
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:U-28_A_Draco
gptkb:Pilatus_PC-12
gptkb:DHC-5_Buffalo
gptkb:T-1_A_Jayhawk
gptkb:De_Havilland_Canada_DHC-6_Twin_Otter
|
|
gptkbp:bfsLayer
|
5
|