Pratt & Whitney Canada PT6A-25A
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
approx. 19 inches
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
approx. 62 inches
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:marketedAs |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
550 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Embraer_EMB_110_Bandeirante
gptkb:Beechcraft_King_Air gptkb:Cessna_208_Caravan |
| gptkbp:weight |
approx. 278 lbs
|
| gptkbp:bfsParent |
gptkb:PC-7_Turbo_Trainer
gptkb:Pilatus_PC-7 gptkb:PC-7 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-25A
|