|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
aircraft
|
|
gptkbp:climate
|
-40 to 50 °C
|
|
gptkbp:compressionRatio
|
8.5:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
16.5 in
|
|
gptkbp:displacement
|
1,100 cubic inches
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
350 lb
general aviation aircraft
16.5 in
42.5 in
free turbine design
|
|
gptkbp:engineConfiguration
|
twin-shaft
twin-shaft configuration
|
|
gptkbp:engineType
|
4
turbine engine
turboprop engine
PT6A-60A
PT6A-60B
PT6A-60D
PT6A-60E
PT6A-60C
|
|
gptkbp:fanEvents
|
composite
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
200 lb/hr
|
|
gptkbp:fuelType
|
Jet A
electronic fuel control
dual fuel system
dual ignition
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT6A-60
|
|
gptkbp:is_monitored_by
|
digital engine monitoring system
|
|
gptkbp:launched
|
electric starter
|
|
gptkbp:length
|
42.5 in
|
|
gptkbp:maintenance
|
1,500 hours
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:maximum_speed
|
250 knots
|
|
gptkbp:noise_level
|
75 dB
|
|
gptkbp:notable_feature
|
PT6A-34, PT6A-41
|
|
gptkbp:notableUsers
|
Beechcraft,_Cessna
|
|
gptkbp:performances
|
3,600 hours
|
|
gptkbp:powerOutput
|
1,100 shp
|
|
gptkbp:propulsion
|
3.14
constant speed propeller
1,100 shp
3.14 hp/lb
|
|
gptkbp:related_engine
|
PT6 family
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:weight
|
350 lb
|