Pratt & Whitney Canada PT6A-41
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
gptkb:Transport_Canada
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
approx. 19 in
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-41
|
| gptkbp:length |
approx. 62 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfStages |
2 axial, 1 centrifugal
1 gas generator, 1 power |
| gptkbp:powerOutput |
850 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Beechcraft_King_Air_200
|
| gptkbp:weight |
approx. 350 lb
|
| gptkbp:bfsParent |
gptkb:C-12_Huron
gptkb:Beechcraft_Model_200 gptkb:Beechcraft_Model_900 |
| gptkbp:bfsLayer |
6
|