Pratt & Whitney Canada PT6A-42
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Beechcraft_King_Air_200
gptkb:Beechcraft_Super_King_Air_B200 |
| gptkbp:certification |
gptkb:FAA
gptkb:Transport_Canada |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
reverse flow
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
19 in
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_PT6
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-42
|
| gptkbp:length |
62.5 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:marketedAs |
gptkb:helicopter
regional aircraft |
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
850 shp
|
| gptkbp:type |
free-turbine turboprop
|
| gptkbp:weight |
278 kg
|
| gptkbp:bfsParent |
gptkb:Beechcraft_King_Air_B200
gptkb:C-12_Huron |
| gptkbp:bfsLayer |
6
|