Pratt & Whitney Canada PT6A-68C
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
gptkb:trainer_aircraft |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1990s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
approx. 2.1 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
1,600 shp
|
| gptkbp:usedIn |
gptkb:Beechcraft_T-6_Texan_II
gptkb:Embraer_EMB_314_Super_Tucano |
| gptkbp:weight |
approx. 300 kg
|
| gptkbp:bfsParent |
gptkb:A-29_Super_Tucano
gptkb:A-29B_Super_Tucano |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-68C
|