PSI - Issue 82

Valentyn Uchanin et al. / Procedia Structural Integrity 82 (2026) 281–287 Valentyn Uchanin et al. / Structural Integrity Procedia 00 (2026) 000–000

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proposed EC techniques enable the timely detection of critical damage without disassembling the AS or removing protective coatings, as part of a predictive maintenance program in the aviation industry. References Abolikhina, E.V., Molyar, A.G., 2003. Corrosion of aircraft structures made of aluminum alloys. Materials Science 39(6), 889–894. Ball, D.L., 2003. The role of nondestructive testing in aircraft damage tolerance. Materials Evaluation 61(7), 814–818. Bossi, R.H. (Ed.), 2014. ASNT Industry Handbook: Aerospace Nondestructive Testing. American Society for Nondestructive Testing, Columbus, OH, 464 pp. Campbell, G.S., Lahey, R., 1984. A survey of serious aircraft accidents involving fatigue fracture. International Journal of Fatigue 6(1), 25–30. Dalton, R.P., Cawley, P., Lowe, M.J.S., 2001. The potential of guided waves for monitoring large areas of metallic aircraft fuselage structure. Journal of Nondestructive Evaluation 20, 29–46. Dziczkowski, L., Zolkiewski, S., 2013. 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