|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12
gptkb:Beechcraft_1900
|
|
gptkbp:armament
|
gptkb:4
|
|
gptkbp:blade_material
|
composite
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
8.5:1
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
16.5 in
|
|
gptkbp:displacement
|
1,100 cubic inches
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:PT6_family
small turboprop
|
|
gptkbp:engine_configuration
|
free turbine
pylon-mounted
PT6 A-25
|
|
gptkbp:engine_power
|
high
5,000 hours
550 shp
2,000 RPM
|
|
gptkbp:engine_shutdown_time
|
15 seconds
|
|
gptkbp:engine_startup_time
|
30 seconds
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
turboprop
|
|
gptkbp:engine_use
|
gptkb:transport_aircraft
gptkb:aircraft
gptkb:military_aircraft
general aviation
commercial aviation
|
|
gptkbp:engine_version
|
PT6 A-25
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_capacity
|
350 lb
16.5 in
42.5 in
|
|
gptkbp:fuel_economy
|
40-50 lb/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney PT6 A-25
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:length
|
42.5 in
|
|
gptkbp:maintenance
|
moderate
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_continuous_power
|
500 shp
|
|
gptkbp:noise_level
|
75 d B
|
|
gptkbp:operational_range
|
1,000 miles
|
|
gptkbp:power_output
|
550 shp
|
|
gptkbp:propeller
|
constant speed
|
|
gptkbp:propeller_blade_material
|
aluminum
|
|
gptkbp:propeller_diameter
|
5.5 ft
|
|
gptkbp:propulsion
|
1,200 lb
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:starter_type
|
electric starter
|
|
gptkbp:torque
|
1,200 lb-ft
|
|
gptkbp:weight
|
350 lb
|
|
gptkbp:bfsParent
|
gptkb:T-6_P_Texan_II
|
|
gptkbp:bfsLayer
|
6
|