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Lycoming LTC1, T-53

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The engine was developed under a joint Air Force & Army contract. One of the designers worked on the WW-II German Juno 004. Engine went through improvements during it's production life.

Technical Specifications
Rated Output 1,400 hp plus 126 lbs thrust at 20,150 r.p.m.
Compressor 4 stage axial
Turbine Free-Turbine
Dry Weight 549 lbs
Commonly Used On UH-1D/H, AH-1G, CUH-1H


Location: Hangar 4