Reliability analysis of the PZL-130 Orlik TC-II aircraft structural component under real operating conditions

The theme of the paper is to present development of new methods for assessing the reliability of the aircraft structure. Based on the described mathematical models , the author developed the “Aircraft Structural Reliability Assessment” (AStRAss) computer software, which implements the realized mathematical model. The aim of the software is calculation of aircraft structure reliability. In this contribution the failure rate of the selected location within the structure of the PZL-130 Orlik TC-II under real operating conditions were calculated. For the chosen control point within the structure the sensitivity of failure rate to the input data was investigated.

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