Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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
|
| 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 |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C30P turboshaft
|