Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
FAA type certified
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
13.8 in
|
| gptkbp:family |
gptkb:Rolls-Royce_Model_250
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 250-C30P
|
| gptkbp:length |
40.5 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Allison_Engine_Company |
| gptkbp:marketedAs |
gptkb:Allison_250-C30P
|
| gptkbp:numberOfStages |
2
6 axial, 1 centrifugal |
| gptkbp:powerOutput |
650 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_206L_LongRanger
gptkb:MD_Helicopters_MD_500 Eurocopter AS355 TwinStar |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Bell_206L-6_LongRanger_VI
gptkb:Bell_206L-7_LongRanger_VII |
| gptkbp:bfsLayer |
6
|