The problem of a stationary ax symmetrical incompressible MHD boundary layer at rotational bod.es was discussed. In accordance with the purpose, the system of the starting differential equat on is derived first of all, and then the Mangler-Stepanov’s (transformations are general zed. W th this, there is the possibility of solving the problem of axisymmetrical MHD boundary layer at rotational bodies by using the solutions of corresponding plane analogies. By applying the method of Loitsyanskii, improved by Saljn'kov, one reach the universal equation of the problem observed. The equation in two--parameter once localized approximation, according to the dynam c parameter was numerically solved on a digital computer. But in th’s paper, the results obtained are presented only partially. Besides that, the procedure for calculation of the special cases of flow was given finally.