Table arrangement for an aircraft having: - a mounting element which can be fastened to a fastening structural element and defines a mounting plane (E), - 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 (S1) between a stowage position, in which the first table element and its centre longitudinal axis (L1) extend substantially parallel to the mounting plane (E) defined by the mounting element , and a use position, in which the first table element and its centre longitudinal axis (L1) extend substantially perpendicularly with respect to the mounting plane (E) 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 (D) which, in the use position, is arranged parallel to the mounting plane (E), wherein the first pivot axis (S1) 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 (D) is arranged, in the stowage position, perpendicularly with respect to the mounting plane (E), 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 (L1) of the first table element and the longitudinal axis (L2) of the second table element . - a mounting element which can be fastened to a fastening structural element and defines a mounting plane (E), - 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 (S1) between a stowage position, in which the first table element and its centre longitudinal axis (L1) extend substantially parallel to the mounting plane (E) defined by the mounting element , and a use position, in which the first table element and its centre longitudinal axis (L1) extend substantially perpendicularly with respect to the mounting plane (E) 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 (D) which, in the use position, is arranged parallel to the mounting plane (E), wherein the first pivot axis (S1) 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 (D) is arranged, in the stowage position, perpendicularly with respect to the mounting plane (E), 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 (L1) of the first table element and the longitudinal axis (L2) of the second table element . <EOS>