Lycoming T53-L-11 turboshaft
GPTKB entity
Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
helicopters
|
| gptkbp:compressionStages |
5 axial, 1 centrifugal
|
| gptkbp:configuration |
axial-centrifugal flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:Lycoming_T53
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
Jet fuel
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53-L-11 turboshaft
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
1100 shp
|
| gptkbp:usedIn |
gptkb:Bell_205
gptkb:Bell_204 gptkb:Bell_UH-1_Iroquois |
| gptkbp:bfsParent |
gptkb:Bell_UH-1D
gptkb:Bell_204B |
| gptkbp:bfsLayer |
7
|