Properties (53)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
general aviation
|
| gptkbp:climate |
up to 1,200 °F
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:cylinderCount |
6
|
| gptkbp:diameter |
24 inches
|
| gptkbp:displacement |
1,100 cubic inches
|
| gptkbp:emissionsStandard |
ICAO_Chapter_4
|
| gptkbp:engine |
24 inches
modular design 300 lbs 39.5 inches |
| gptkbp:engineConfiguration |
twin-shaft
|
| gptkbp:engineType |
4
free turbine air start |
| gptkbp:firstFlight |
1963
|
| gptkbp:fuel_capacity |
0.5 lb/hp/hr
150 lb/hr |
| gptkbp:fuelType |
dual ignition
dual fuel pumps Jet_A_or_Jet_A-1 |
| https://www.w3.org/2000/01/rdf-schema#label |
PT6A-42
|
| gptkbp:landing_gear |
17.5:1
|
| gptkbp:length |
39.5 inches
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:notableUsers |
gptkb:Cessna
gptkb:Bombardier Piper Beechcraft Dornier |
| gptkbp:powerOutput |
850 shp
|
| gptkbp:propulsion |
2.83
|
| gptkbp:related_engine |
temperature sensors
control unit pressure sensors speed sensors oil cooler starter-generator fuel filter oil filter fuel control unit ignition exciter power turbine governor vibration sensor Brayton_cycle |
| gptkbp:service_ceiling |
25,000 feet
|
| gptkbp:torque |
dry sump
|
| gptkbp:type |
turboprop engine
|
| gptkbp:weight |
approximately 300 lbs
|