The exploitation process of gas turbines features various damage to their elements with
various effects on their usability. The overheating of the blade material, especially of
uncooled blades constitutes damage that is very difficult to identify and a failure hazard that
is very difficult to classify. The article presents the results of testing of selected factors on the
condition and degradation of heat-resistant coatings (insulation and protective layers) of gas
turbine blades from jet motors for manoeuvring aircraft drive units. The deliberations were …