Landing is a critical flight phase that requires precise energy dissipation. This paper utilizes the 4th-order Runge-Kutta method and MATLAB software to evaluate the touchdown performance profiles of the C-212 platform under standard, headwind, and tailwind conditions. The computational results indicate a nominal ground roll distance of exactly 598.97 meters. Under the influence of a headwind at -6m/s, the distance decreases significantly to 454.65 meters. Conversely, a tailwind at +6 m/s substantially extends the necessary stopping distance to 770.99 meters. Ultimately, these specific quantitative results serve as a crucial theoretical foundation for future pilot training.

Van Viet Vo, Duc Dung Nguyen, Le Thanh Nguyen, "Investigation Into Wind Influence on the Landing Performance of the C-212 Platform" International Journal of Advanced Multidisciplinary Research and Educational Development, V2(4): Page(22-24) July - August 2026. ISSN: 3107-6513. www.ijamred.com. Published by Scientific and Academic Research Publishing.