Ranking of the technical condition of aircraft according to the diagnostic data of the glider design

Analysis of the data obtained through non-destructive testing of the power elements of the airframe structure enables the division of the studied aircraft into separate groups based on operational methods and, accordingly, predicts the probability of trouble-free operation of the airframe structure. Based on a bionic logical analysis of data on the technical condition of the aircraft’s airframe design, the article considers methodological approaches to building the author’s mathematical model of ranking the aircraft fleet. The ranking of the technical condition of aircraft serves as the basis for solving the problem of preparation, making a decision on extending the service life and taking into account the aging of the airframe design in operating conditions. The application of the proposed set of methods will create and establish a practical and effective system of intelligent support for decision-making on aircraft operations.