|Turbine:||2x gas generator turbine stages + 1x free power turbine stage|
|Compressor:||10 stage axial-flow|
|Displacement:||176 cu. in|
|Power Output:||1,250 hp|
Courtesy of the National Museum of Naval Aviation
Born from a proposal to the U.S. Navy in 1953 for an advanced helicopter engine, the T58 first flew in February, 1957 and quickly gained popularity with helicopter manufacturers.
Variants of the the T58 were used in aircraft included:
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