Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
helicopters
|
| gptkbp:configuration |
axial-centrifugal flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.53 m
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:length |
1.52 m
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:numberOfStages |
5 axial, 1 centrifugal
|
| gptkbp:partOf |
Lycoming T53 family
|
| gptkbp:powerOutput |
1,400 shp
|
| gptkbp:status |
in service
|
| gptkbp:usedIn |
gptkb:Bell_205
gptkb:Bell_204 gptkb:Bell_212 gptkb:Bell_UH-1_Iroquois |
| gptkbp:weight |
385 kg
|
| gptkbp:bfsParent |
gptkb:UH-1H_helicopter
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53-L-13
|