Pratt & Whitney Canada PT6A-27 turboprop
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
approx. 19 in
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-27 turboprop
|
| gptkbp:length |
approx. 62 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:notableFeature |
modular construction
reverse flow design |
| gptkbp:numberOfAxles |
two
|
| gptkbp:numberOfStages |
1 gas generator, 1 power
3 axial, 1 centrifugal |
| gptkbp:powerOutput |
680 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Embraer_EMB_110_Bandeirante
gptkb:de_Havilland_Canada_DHC-6_Twin_Otter |
| gptkbp:bfsParent |
gptkb:Beechcraft_99_Airliner
|
| gptkbp:bfsLayer |
7
|