Aircraft corrosion poses significant challenges within the aviation industry, including safety hazards, heightened maintenance expenses, and potential disruptions in operations. To mitigate these issues, electroplating techniques are commonly employed to apply corrosion-resistant coatings to aircraft components. This research project aims to investigate the electroplating process utilizing a nickel-molybdenum (Ni-Mo) alloy as a protective coating for these components. The primary goal is to create a mathematical model that optimizes electroplating parameters and accurately predicts the corrosion resistance performance of the Ni-Mo coating. By conducting a review of an existing literature, designing and executing experiments, developing a mathematical model, and validating the results, this study contributes to our knowing the electroplating process and its influence on corrosion resistance. The outcomes of this research hold significant implications for the development of advanced corrosion protection strategies in the aviation industry. Ultimately, these strategies will enhance safety, reduce maintenance costs, and improve operational reliability.