A full flight simulator, comprising: - a simulator cabin, wherein a seat for an operator, an image display device for displaying the simulated surroundings and at least one operating element for generating simulation control data and in particular for controlling the simulated flight vehicle and for allowing the operator to influence the simulation are provided in the simulator cabin, - a parallel kinematic arrangement, comprising a basis, a support element and multiple linear motion devices, wherein the support element is connected to the basis via at least three, preferably six, linear motion devices, and wherein the basis is connected or coupled to the ground and the support element is connected or coupled to the simulator cabin so that the simulator cabin is arranged on the parallel kinematic arrangement, wherein the simulator cabin has an initial position, which substantially corresponds to a stationary straight flight of the simulated flight vehicle and in which the roll axis of the simulated flight vehicle or of the operator extends substantially horizontally, wherein the simulator cabin has a maximum positive pitch position, in which the roll axis, based on the horizontal extension, is inclined upwards by a first pitch angle as far a possible within the scope of the kinematic possibilities of the parallel kinematic arrangement in compliance with potentially provided control reserves, whereby the operator is inclined backwards, wherein the simulator cabin has a maximum negative pitch position, in which the roll axis, based on the horizontal extension, is inclined downwards by a second pitch angle within the scope of the kinematic possibilities of the parallel kinematic arrangement in compliance with potentially provided control reserves, whereby the operator is inclined forwards, characterized - in that the first pitch angle is greater than 25°, - in that the parallel kinematic arrangement has a parallel kinematic initial position, in which the basis and the support element extend substantially parallel and in which the roll axis is inclined upwards by a positive differential angle and in which the simulator cabin is arranged in a position deviating from its initial position, - and in that the parallel kinematic arrangement is arranged in a position deviating from the parallel kinematic initial position when the simulator cabin is arranged in its initial position. - a simulator cabin, wherein a seat for an operator, an image display device for displaying the simulated surroundings and at least one operating element for generating simulation control data and in particular for controlling the simulated flight vehicle and for allowing the operator to influence the simulation are provided in the simulator cabin, - a parallel kinematic arrangement, comprising a basis, a support element and multiple linear motion devices, wherein the support element is connected to the basis via at least three, preferably six, linear motion devices, and wherein the basis is connected or coupled to the ground and the support element is connected or coupled to the simulator cabin so that the simulator cabin is arranged on the parallel kinematic arrangement, wherein the simulator cabin has an initial position, which substantially corresponds to a stationary straight flight of the simulated flight vehicle and in which the roll axis of the simulated flight vehicle or of the operator extends substantially horizontally, wherein the simulator cabin has a maximum positive pitch position, in which the roll axis, based on the horizontal extension, is inclined upwards by a first pitch angle as far a possible within the scope of the kinematic possibilities of the parallel kinematic arrangement in compliance with potentially provided control reserves, whereby the operator is inclined backwards, wherein the simulator cabin has a maximum negative pitch position, in which the roll axis, based on the horizontal extension, is inclined downwards by a second pitch angle within the scope of the kinematic possibilities of the parallel kinematic arrangement in compliance with potentially provided control reserves, whereby the operator is inclined forwards, characterized - in that the first pitch angle is greater than 25°, - in that the parallel kinematic arrangement has a parallel kinematic initial position, in which the basis and the support element extend substantially parallel and in which the roll axis is inclined upwards by a positive differential angle and in which the simulator cabin is arranged in a position deviating from its initial position, - and in that the parallel kinematic arrangement is arranged in a position deviating from the parallel kinematic initial position when the simulator cabin is arranged in its initial position.