Pratt & Whitney Canada PT6A-28
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
regional aircraft |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_PT6
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-28
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
680 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedIn |
gptkb:Embraer_EMB_110_Bandeirante
gptkb:Beechcraft_King_Air gptkb:Shorts_330 |
| gptkbp:bfsParent |
gptkb:Beechcraft_Model_100
|
| gptkbp:bfsLayer |
6
|