Table arrangement for an aircraft having: - a mounting element which can be fastened to a fastening structural element and defines a mounting plane, - a first table element connected to the mounting element, wherein the first table element can be pivoted relative to the mounting element about a first pivot axis between a stowage position, in which the first table element and its centre longitudinal axis extend substantially parallel to the mounting plane defined by the mounting element, and a use position, in which the first table element and its centre longitudinal axis extend substantially perpendicularly with respect to the mounting plane defined by the mounting element, and - a second table element connected to the first table element, wherein the second table element is arranged substantially parallel to the first table element and can be rotated relative to the first table element about a rotational axis which, in the use position, is arranged parallel to the mounting plane, wherein the first pivot axis can be moved between a rest position and an operating position in the case of a transfer of the first table element between its stowage position and its use position relative to the mounting element, characterized in that - the rotational axis is arranged, in the stowage position, perpendicularly with respect to the mounting plane, and - the second table element, at least when the first table element is arranged in its stowage position, can be displaced relative to the first table element in a direction parallel to the centre longitudinal axis of the first table element and the longitudinal axis of the second table element. - a mounting element which can be fastened to a fastening structural element and defines a mounting plane, - a first table element connected to the mounting element, wherein the first table element can be pivoted relative to the mounting element about a first pivot axis between a stowage position, in which the first table element and its centre longitudinal axis extend substantially parallel to the mounting plane defined by the mounting element, and a use position, in which the first table element and its centre longitudinal axis extend substantially perpendicularly with respect to the mounting plane defined by the mounting element, and - a second table element connected to the first table element, wherein the second table element is arranged substantially parallel to the first table element and can be rotated relative to the first table element about a rotational axis which, in the use position, is arranged parallel to the mounting plane, wherein the first pivot axis can be moved between a rest position and an operating position in the case of a transfer of the first table element between its stowage position and its use position relative to the mounting element, - the rotational axis is arranged, in the stowage position, perpendicularly with respect to the mounting plane, and - the second table element, at least when the first table element is arranged in its stowage position, can be displaced relative to the first table element in a direction parallel to the centre longitudinal axis of the first table element and the longitudinal axis of the second table element.