Pratt & Whitney Canada PT6A-114A
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
gptkb:FAA
gptkb:Transport_Canada |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1990s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-114A
|
| gptkbp:length |
approx. 62 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
675 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Cessna_208B_Grand_Caravan
gptkb:Cessna_208_Caravan |
| gptkbp:weight |
approx. 278 kg
|
| gptkbp:bfsParent |
gptkb:Cessna_Grand_Caravan
gptkb:Cessna_208B_Grand_Caravan gptkb:Cessna_208B gptkb:Cessna_208_Super_Cargomaster |
| gptkbp:bfsLayer |
7
|