|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:Beechcraft_1900
gptkb:Dornier_228
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:4
gptkb:6
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:compression_ratio
|
12:1
8:1
|
|
gptkbp:configuration
|
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
0.5 m
|
|
gptkbp:engine
|
gptkb:PT6_A
Brayton cycle
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:PT6_A-114_A
gptkb:PT6_A-70
turboprop
PT6 A-67 B
PT6 A-67 D
PT6 A-60 A
PT6 A-42 A
PT6 A-135 A
PT6 A-140 A
PT6 A-41
PT6 A-45 A
PT6 A-60 C
PT6 A-68 D
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PT6 A-42
|
|
gptkbp:ignition_system
|
gptkb:electronic
|
|
gptkbp:is_often_used_in
|
regional aircraft
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
2000 hours
3000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:notable_applications
|
gptkb:Beechcraft_King_Air
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:power_output
|
850 shp
|
|
gptkbp:propeller
|
constant speed
|
|
gptkbp:propulsion
|
5.67:1
850 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:weight
|
150 kg
|
|
gptkbp:bfsParent
|
gptkb:Piper_PA-46_Meridian
|
|
gptkbp:bfsLayer
|
6
|