Pratt & Whitney Canada PT6A-135
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:certification |
gptkb:FAA
gptkb:Transport_Canada |
| gptkbp:compression_system |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
19 in
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1980s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
62.5 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:powerOutput |
750 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Beechcraft_King_Air_C90GT
gptkb:Quest_Kodiak gptkb:Cessna_208_Caravan |
| gptkbp:weight |
278 kg
|
| gptkbp:bfsParent |
gptkb:F90
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-135
|