Stability analysis of conceptual design ultralight aircraft “Kiras” is presented in this master’s thesis. Longitudinal stability is evaluated by manual counting and Athena vortex – lattice based AVL program. Lateral derivatives, such as eigenvalues of spiral mode, “dutch roll“, Phugoid and short period oscillations were estimated by AVL . Thesis involves analysis of damping ratio, period T 1/2, time t 1/2, ocsillation circular frequency wn, number of cycles N 1/2 of distinct aircraft motions. The range of eigenvalues for specified run cases were automatically generated by AVL eigenmode meniu. At early phase of ultralight aircraft design, spiral instability was found. This problem fixed by approach method by correction of tail geometry and wing dihedral. According to the counting results and computerized motion analysis of an airplane, the corrected geometry of vertical tail is offered. Finally, the conclusions were made. Thesis consist of: 54 p. text without appendixes (67 p. with), 9 pictures, 10 tables, 12 bibliographical notes. Appendixes included.