|
gptkbp:instance_of
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gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Cessna_208_Caravan
gptkb:De_Havilland_Canada_Dash_8
gptkb:Pilatus_PC-12
gptkb:Beechcraft_1900
gptkb:Dornier_228
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:configuration
|
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
14.5 in
|
|
gptkbp:displacement
|
1,100 cubic inches
|
|
gptkbp:engine
|
gptkb:PT6_family
air start
|
|
gptkbp:engine_configuration
|
modular design
twin-shaft
twin-shaft turboprop
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
turboprop
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_capacity
|
350 lb
48.5 in
14.5 in
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6 A-68
|
|
gptkbp:ignition_system
|
dual ignition system
|
|
gptkbp:length
|
48.5 in
|
|
gptkbp:maintenance
|
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:number_of_engines
|
gptkb:6
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
commercial aviation
|
|
gptkbp:power_output
|
1,100 shp
|
|
gptkbp:powers
|
1.0 hp/lb
|
|
gptkbp:propeller
|
4.5 ft
variable pitch propeller
|
|
gptkbp:propeller_reduction_ratio
|
16:1
|
|
gptkbp:propulsion
|
3.14
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:torque
|
dry sump lubrication
|
|
gptkbp:weight
|
350 lb
|
|
gptkbp:bfsParent
|
gptkb:A-29_B
|
|
gptkbp:bfsLayer
|
5
|