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Lycoming T53

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The engine was developed primarily for uses in helicopters. The power output gearbox is located on the front of the engine. The museums example is a training cutaway that is turned at a low RPM as an exhibit. Engine was first tested on a Kaman HOK-1 in 1956.

Technical Specifications
Rated Output 1,400 hp at 6,640 r.p.m.
Compressor 5 stage axial, 1 stage centrifugal
Turbine 1 stage
Dry Weight 54 lbs
Commonly Used On AH-1S, UH-1, UH-1H, UH-1M, HH-43F


Location: Restoration