Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Rolls-Royce_M250
|
| gptkbp:application |
helicopters
fixed-wing aircraft |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1961
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison Model 250
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:numberBuilt |
over 30,000
|
| gptkbp:powerOutput |
317 to 715 shaft horsepower
|
| gptkbp:producedBy |
gptkb:Rolls-Royce_North_America
|
| gptkbp:status |
in production
|
| gptkbp:successor |
gptkb:Rolls-Royce_M250
|
| gptkbp:type |
turboprop
turboshaft |
| gptkbp:usedIn |
gptkb:Agusta_A109
gptkb:Bell_206_JetRanger gptkb:Eurocopter_AS355 gptkb:MD_Helicopters_MD_500 gptkb:Cessna_421C_Golden_Eagle_(conversion) gptkb:Schweizer_330 |
| gptkbp:bfsParent |
gptkb:Allison_250-C30_turboshaft
|
| gptkbp:bfsLayer |
6
|