Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
light helicopters
|
| gptkbp:compressor_type |
axial-centrifugal
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:family |
gptkb:Allison_Model_250
|
| gptkbp:firstProduced |
1970s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
approximately 40 inches
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Hughes_500
gptkb:Bell_206_JetRanger gptkb:Enstrom_480 |
| gptkbp:weight |
approximately 170 lbs
|
| gptkbp:bfsParent |
gptkb:Fantrainer_aircraft
gptkb:MD_500_Defender |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison 250-C20B turboshaft
|