Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:configuration |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:Lycoming_T55
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T55-L-5 turboshaft
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
2,650 shp
|
| gptkbp:usedIn |
gptkb:Boeing_CH-47_Chinook
|
| gptkbp:bfsParent |
gptkb:CH-47A
|
| gptkbp:bfsLayer |
6
|