Pratt & Whitney Canada PT6A-20
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Embraer_EMB_110_Bandeirante
gptkb:Beechcraft_King_Air gptkb:de_Havilland_Canada_DHC-6_Twin_Otter |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:PT6
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-20
|
| gptkbp:introducedIn |
1963
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
550 shp
|
| gptkbp:usedIn |
fixed-wing aircraft
|
| gptkbp:bfsParent |
gptkb:DHC-6-100
gptkb:DHC-6-200 |
| gptkbp:bfsLayer |
7
|