Statements (20)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:certification |
FAA type certified
|
gptkbp:compressor_type |
axial-centrifugal
|
gptkbp:diameter |
13.8 in
|
gptkbp:family |
gptkb:Allison_Model_250
|
gptkbp:firstProduced |
1970s
|
gptkbp:fuelType |
gptkb:Jet-A
|
https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C30P turboshaft
|
gptkbp:length |
41.5 in
|
gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
gptkbp:marketedAs |
gptkb:Rolls-Royce_250-C30P
|
gptkbp:numberOfStages |
7 axial, 1 centrifugal
2 gas generator, 2 power turbine |
gptkbp:powerOutput |
650 shp
|
gptkbp:type |
turboshaft
|
gptkbp:usedInAircraft |
gptkb:Bell_206L_LongRanger
gptkb:MD_Helicopters_MD_500 |
gptkbp:weight |
170 lb
|
gptkbp:bfsParent |
gptkb:Bell_206L_LongRanger
|
gptkbp:bfsLayer |
6
|