Pratt & Whitney Canada PT6A-27
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Embraer_EMB_110_Bandeirante
gptkb:de_Havilland_Canada_DHC-6_Twin_Otter |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
reverse flow
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_PT6
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
Aviation kerosene
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
680 shp
|
| gptkbp:status |
in production
|
| gptkbp:type |
free-turbine
|
| gptkbp:bfsParent |
gptkb:DHC-6-300
gptkb:De_Havilland_Canada_DHC-6_Twin_Otter gptkb:Beechcraft_99A gptkb:Beechcraft_99B gptkb:EMB_110E gptkb:EMB_110P1 gptkb:Beechcraft_99C gptkb:Embraer_C-95_Bandeirante |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-27
|