Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Honeywell_LTS101
|
| gptkbp:application |
gptkb:helicopter
fixed-wing aircraft |
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
18.5 in
|
| gptkbp:firstFlight |
1970s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming LTS101
|
| gptkbp:length |
39.5 in
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
650 shp
850 shp |
| gptkbp:status |
in production
|
| gptkbp:successor |
gptkb:Honeywell_LTS101
|
| gptkbp:type |
turboprop
turboshaft |
| gptkbp:usedIn |
gptkb:Bell_222
gptkb:Aérospatiale_AS350 gptkb:MBB/Kawasaki_BK_117 Aérospatiale AS355 Eurocopter EC135 (early models) |
| gptkbp:weight |
200 lb
|
| gptkbp:bfsParent |
gptkb:Bell_222
|
| gptkbp:bfsLayer |
6
|