Abstract: A gear box, in particular a planetary gear box of a gas turbine engine, is proposed, having at least one planet carrier which comprises two webs which are spaced apart in an axial direction. By means of the webs, at least one planet gear which is configured to be rotatable relative to the planet carrier is operatively connected to the planet carrier. An axis of rotation of the planet gear, below or in the case of a defined load-dependent deformation of the planet carrier, deviates from a parallel course of an axis of symmetry of the planet carrier. Furthermore, the axis of rotation of the planet gear, in the case of a further defined load-dependent deformation of the planet carrier greater than the defined load-dependent deformation of the planet carrier, runs at least approximately parallel to the axis of symmetry of the planet carrier.