Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
centrifugal and axial
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:diameter |
13.8 in
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
41.5 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:marketedAs |
Rolls-Royce 250-C20J
|
| gptkbp:partOf |
Allison Model 250 engine family
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:usedIn |
gptkb:Bell_206B_JetRanger_III
gptkb:Enstrom_480 gptkb:Schweizer_333 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:TH-57_Sea_Ranger
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C20J turboshaft
|