Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:firstFlight |
1976
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:powerOutput |
1,240–1,776 kW
|
| gptkbp:status |
in production
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Eurocopter_AS532_Cougar
gptkb:Eurocopter_AS332_Super_Puma gptkb:Eurocopter_EC225_Super_Puma gptkb:HAL_Dhruv Denel Oryx |
| gptkbp:bfsParent |
gptkb:Turbomeca_engines
gptkb:Turbomeca_Makila_1A1 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Makila
|