Statements (23)
Predicate | Object |
---|---|
gptkbp:instanceOf |
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
|
https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53-L-13
|
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
gptkb:Bell_UH-1H_Iroquois gptkb:Bell_UH-1H_Huey |
gptkbp:bfsLayer |
6
|