Pratt & Whitney Canada PT6A-62 turboprop
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1980s
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-62 turboprop
|
| gptkbp:length |
approx. 62 inches
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:marketedAs |
PT6A-62
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
950 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedIn |
gptkb:Pilatus_PC-7_MkII
gptkb:Pilatus_PC-9 |
| gptkbp:weight |
approx. 350 lbs
|
| gptkbp:bfsParent |
gptkb:Pilatus_PC-9
gptkb:Pilatus_PC-9A gptkb:Pilatus_PC-9B |
| gptkbp:bfsLayer |
6
|