Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C28B turboshaft
|
| gptkbp:length |
approximately 40 inches
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:partOf |
gptkb:Allison_Model_250_family
|
| gptkbp:powerOutput |
500 shp
|
| gptkbp:usedIn |
gptkb:Bell_206L_LongRanger
gptkb:MBB_Bo_105 gptkb:Agusta_A109 |
| gptkbp:weight |
approximately 170 lbs
|
| gptkbp:bfsParent |
gptkb:Bell_206L-1_LongRanger_II
|
| gptkbp:bfsLayer |
6
|