Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
19.0 in
|
| gptkbp:family |
gptkb:Allison_Model_250
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
39.0 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:marketedAs |
Rolls-Royce M250-C18
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Allison_250-C20
|
| gptkbp:usedIn |
gptkb:Hughes_500
gptkb:Bell_206_JetRanger helicopters fixed-wing aircraft |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Allison_T63-A-5_turboshaft
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C18
|