Abstract
The reliability and maintainability problems associated with gas turbine engines currently operational with the U.S. military services were examined in the report. A broad spectrum of turboshaft and turboprop engines in U.S. Army, Navy and Marine helicopters and fixed-wing aircraft was examined. The study concentrated on the detailed R and M experience of the T53, T55, T58, T64, T73 and T74, although quantitative R+M data is provided on other gas turbine engines in military and commercial service.

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