Pratt & Whitney Canada PT6A-67B turboprop
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| 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-67B turboprop
|
| gptkbp:length |
approx. 80 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
1200 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Beechcraft_1900D
gptkb:Pilatus_PC-12 |
| gptkbp:weight |
approx. 500 lb
|
| gptkbp:bfsParent |
gptkb:U-28A_Draco
gptkb:U-28A |
| gptkbp:bfsLayer |
7
|