Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
helicopters
|
| gptkbp:compressionRatio |
centrifugal and axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
19 in
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C30P
|
| gptkbp:length |
40.5 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Allison_Engine_Company |
| gptkbp:partOf |
gptkb:Allison_Model_250_family
|
| gptkbp:powerOutput |
650 shp
|
| gptkbp:status |
in production
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_206L_LongRanger
gptkb:Agusta_A109 gptkb:MD_Helicopters_MD_500 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Bell_206L-10_LongRanger_X
gptkb:Bell_206L-14_LongRanger_XIV gptkb:Bell_206L-3_LongRanger_III gptkb:Bell_206L-4_LongRanger_IV gptkb:Bell_206L-5_LongRanger_V |
| gptkbp:bfsLayer |
6
|