Pratt & Whitney Canada PW206B2
GPTKB entity
Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:PW200
|
| gptkbp:firstFlight |
1990s
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:powerOutput |
approx. 609 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
Eurocopter EC135 T2
|
| gptkbp:bfsParent |
gptkb:EC135_P2
gptkb:EC135_P2+ |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW206B2
|