Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:Lycoming_T53-L-703
gptkb:Lycoming_T53-L-91 |
| gptkbp:application |
helicopter propulsion
|
| gptkbp:compression_ratio |
8:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
approximately 14 in
|
| gptkbp:engine |
gptkb:engine
|
| gptkbp:first_introduced |
1960s
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53-L-740
|
| gptkbp:length |
approximately 40 in
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:notable_users |
gptkb:Bell_UH-1_Iroquois
|
| gptkbp:power_output |
1,500 shp
|
| gptkbp:type |
turbo shaft engine
|
| gptkbp:used_in |
gptkb:helicopter
|
| gptkbp:variant |
T53-L-703
|
| gptkbp:weight |
approximately 400 lb
|