Pratt & Whitney Canada PT6A-25
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
gptkb:FAA
gptkb:Transport_Canada |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
approx. 19 in
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_PT6
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-25
|
| gptkbp:length |
approx. 62 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfStages |
1 gas generator, 1 power
3 axial, 1 centrifugal |
| gptkbp:powerOutput |
550 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedIn |
gptkb:Beechcraft_99
gptkb:Beechcraft_Super_King_Air_200 gptkb:Beechcraft_King_Air_C90 |
| gptkbp:weight |
approx. 278 kg
|
| gptkbp:bfsParent |
gptkb:T-34C_Turbo-Mentor
gptkb:Beechcraft_T-34C_Turbo_Mentor |
| gptkbp:bfsLayer |
7
|