Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:helicopter
regional aircraft |
| gptkbp:basedOn |
gptkb:Walter_M601
|
| gptkbp:certification |
2011
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:features |
extended time between overhauls
improved hot section materials no need for engine inlet particle separator |
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:marketedAs |
gptkb:twin-engine_turboprop_aircraft
|
| gptkbp:powerOutput |
800 shp
|
| gptkbp:usedIn |
gptkb:Let_L-410NG
|
| gptkbp:bfsParent |
gptkb:Let_L-410
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
GE H80 (L-410NG)
|