Pratt & Whitney Canada PT6A-28 turboprop
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
19 in
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-28 turboprop
|
| gptkbp:length |
62.5 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
680 shp
|
| gptkbp:status |
in production
|
| gptkbp:type |
turboprop
|
| gptkbp:usedIn |
gptkb:Embraer_EMB_110_Bandeirante
gptkb:Beechcraft_King_Air_C90 |
| gptkbp:bfsParent |
gptkb:Embraer_EMB_121_Xingu
|
| gptkbp:bfsLayer |
7
|