Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
single-spool
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:family |
gptkb:Turbomeca_Arrius
|
| gptkbp:firstFlight |
1995
|
| gptkbp:fuelType |
gptkb:Jet-A1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arrius 2F
|
| gptkbp:intendedUse |
light helicopter
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:numberOfAxles |
1
|
| gptkbp:powerOutput |
504 shp
|
| gptkbp:usedIn |
gptkb:Eurocopter_EC120_Colibri
|
| gptkbp:bfsParent |
gptkb:Eurocopter_EC120
gptkb:EC-120_Colibri gptkb:Eurocopter_EC120_Colibri |
| gptkbp:bfsLayer |
6
|