An aircraft with a rest arrangement, comprising: a first support element; and a first lying-down facility, a second lying-down facility, and a third lying-down facility; the first, second and third lying-down facilities (5a, b, c) comprising a first fastening region, respectively; wherein the first fastening region of the first, second and third lying-down facilities (5a, b, c) comprise a first fastening element, which is adapted as a pivot joint, and a second fastening element, respectively; and wherein the first, second and third lying-down facility (5a, b, c) are affixed to the first support element by the first and second fastening elements (8a, b), respectively; wherein the first fastening elements of the first, second and third lying-down facilities (5a, b, c) are slidably arranged on or in a linear guide (12a, b, c), respectively; wherein the linear guide of the third lying-down facility is vertically arranged to the linear guides of the first and second lying-down facilities (5a, b); wherein the first, second, and third lying-down facilities (5a, b, c) are pivotable between a first state and a second state, respectively, wherein the transition between the first and second state is a combined rotational and translational movement; wherein the first, second, and third lying-down facilities (5a, b, c) are arranged to be above each other and essentially horizontal in the first state and are arranged to be essentially vertical and parallel to each other in the second state; and wherein the first, second and third lying-down facilities (5a, b, c) comprise a second fastening region, respectively, by which the lying-down facility (5a, b, c) is affixable to a second supporting element. a first support element; and a first lying-down facility, a second lying-down facility, and a third lying-down facility; the first, second and third lying-down facilities (5a, b, c) comprising a first fastening region, respectively; wherein the first fastening region of the first, second and third lying-down facilities (5a, b, c) comprise a first fastening element, which is adapted as a pivot joint, and a second fastening element, respectively; and wherein the first, second and third lying-down facility (5a, b, c) are affixed to the first support element by the first and second fastening elements (8a, b), respectively; wherein the first fastening elements of the first, second and third lying-down facilities (5a, b, c) are slidably arranged on or in a linear guide (12a, b, c), respectively; wherein the linear guide of the third lying-down facility is vertically arranged to the linear guides of the first and second lying-down facilities (5a, b); wherein the first, second, and third lying-down facilities (5a, b, c) are pivotable between a first state and a second state, respectively, wherein the transition between the first and second state is a combined rotational and translational movement; wherein the first, second, and third lying-down facilities (5a, b, c) are arranged to be above each other and essentially horizontal in the first state and are arranged to be essentially vertical and parallel to each other in the second state; and wherein the first, second and third lying-down facilities (5a, b, c) comprise a second fastening region, respectively, by which the lying-down facility (5a, b, c) is affixable to a second supporting element.