|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
reverse flow
|
|
gptkbp:compression_ratio
|
9:1
|
|
gptkbp:configuration
|
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
14 in
|
|
gptkbp:displacement
|
1,100 cubic inches
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:PT6_family
gptkb:advanced_technology
general aviation
|
|
gptkbp:engine_configuration
|
modular design
twin-shaft turboprop
|
|
gptkbp:engine_power
|
high
excellent
5,000 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
turboprop
PT6 A-68
PT6 A-67
PT6 A-69
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_capacity
|
350 lb
48.5 in
14 in
|
|
gptkbp:fuel_economy
|
high
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT6 A-66
|
|
gptkbp:launch_window
|
air start
|
|
gptkbp:length
|
48.5 in
|
|
gptkbp:maintenance
|
easy
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
75 d B
|
|
gptkbp:notable_users
|
gptkb:Cessna
gptkb:Beechcraft
gptkb:Bombardier
gptkb:Piper_Aircraft
|
|
gptkbp:power_output
|
1,100 shp
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:propulsion
|
3.14
1,100 shp
3.14 hp/lb
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:water_requirement
|
200 lb/hr
|
|
gptkbp:weight
|
350 lb
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PT6_A-68
|
|
gptkbp:bfsLayer
|
5
|