Abstract
Introduction. The problem of POD of NDT is very important for Russian aerospace industry nowadays. Using FAAACС 33.14 data is inexpedient because of significant difference between Russian and foreign titanium disks ultrasonic testing NDT manuals. Probability of defect detection versus its size curves are necessary for the deficiency evaluation of gas-turbine engine basic parts. Evaluation of gas-turbine engine basic parts deficiency is necessary for new procedure of resource calculation introduction.
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