Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:family |
gptkb:Allison_Model_250
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C30 turboshaft
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:powerOutput |
650 shp
|
| gptkbp:successor |
gptkb:Allison_250-C40
|
| gptkbp:usedIn |
gptkb:Bell_206L_LongRanger
gptkb:Agusta_A109 gptkb:MD_Helicopters_MD_500 |
| gptkbp:bfsParent |
gptkb:MH-6_Little_Bird
|
| gptkbp:bfsLayer |
5
|