An arrangement for installing a component in an aircraft comprises a guide device which is connectable to an aircraft structure or is formed integrally with the aircraft structure, as well as an elastically deformable damping element which is adapted to enable the component to be mounted in the guide device in a self-supporting manner. The RCC configures a feature on a first MWCD of a first supplier and a second MWCD of a second supplier. The divider circuit includes a first capacitor, a second capacitor, and a switch to alternately divide a remaining charge Q by 2N between the first and second capacitors until the remaining charge Qin at the amplifier is below a threshold value.