Machining system for aircraft structural components

A processing installation for aircraft structural components having a processing station comprising a clamping frame for receiving the aircraft structural component which is intended to be processed in each case, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction and a processing unit for processing the aircraft structural component which has an upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis extend parallel with a vertical direction which is angled relative to the longitudinal direction, in particular orthogonal, wherein the processing installation has a processing region for processing the aircraft structural component which is formed by a laterally delimited, first spatial portion in which the clamping frame and the processing unit are arranged during processing, wherein the processing installation has a service region for carrying out service operations, which is formed by a laterally delimited, second spatial portion, wherein the first spatial portion is separated from the second spatial portion in a transverse direction which is orthogonal to the longitudinal direction and vertical direction, wherein a service platform is arranged in the service region and is or can be positioned in a service plane which is orthogonal to the vertical direction,

• wherein
• the upper tool and the lower tool are displaceable into at least one service position, wherein both tools are accessible from the common service platform which is positioned in the service plane in the service positions.