Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
7.3:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
19 in
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
40.5 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Allison_Engine_Company |
| gptkbp:numberOfStages |
2
7 axial, 1 centrifugal |
| gptkbp:part_of |
gptkb:Allison_Model_250_family
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:used_in |
gptkb:Bell_206L_LongRanger
gptkb:MD_500 gptkb:Eurocopter_AS355 |
| gptkbp:weight |
170 lb
|
| gptkbp:bfsParent |
gptkb:Sikorsky_S-333
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C20W
|