Pratt & Whitney Canada PT6A-67
GPTKB entity
Statements (28)
| 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 inches
|
| gptkbp:family |
gptkb:PT6A
|
| gptkbp:firstFlight |
1980s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-67
|
| gptkbp:length |
approx. 80 inches
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:market |
gptkb:helicopter
regional aircraft |
| gptkbp:notableFeature |
modular design
reverse flow combustion |
| gptkbp:numberOfStages |
1 gas generator, 1 power
3 axial, 1 centrifugal |
| gptkbp:powerOutput |
1200-1600 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Viking_Air_DHC-6_Twin_Otter_Series_400
gptkb:Beechcraft_1900 gptkb:Pilatus_PC-12 gptkb:Air_Tractor_AT-802 |
| gptkbp:weight |
approx. 350 kg
|
| gptkbp:bfsParent |
gptkb:Pilatus_PC-12
|
| gptkbp:bfsLayer |
6
|