Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:diameter |
19 in
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C20R turboshaft
|
| gptkbp:length |
41.5 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:marketedAs |
Rolls-Royce 250-C20R turboshaft
|
| gptkbp:partOf |
Allison Model 250 engine family
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:successor |
gptkb:Rolls-Royce_250-C30
|
| gptkbp:usedIn |
gptkb:Bell_206L_LongRanger
gptkb:MD_Helicopters_MD_500 gptkb:Schweizer_333 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:MD_520N
|
| gptkbp:bfsLayer |
7
|