Aircraft-seat assembly

An aircraft seat arrangement with a first aircraft seat device and with a second aircraft seat device, the second aircraft seat device is arranged directly behind the first aircraft seat device and is realized at least substantially identically to the first aircraft seat device,

• wherein the second aircraft seat device has an aircraft seat device longitudinal axis which extends along fastening points of the second aircraft seat device, the fastening points of the second aircraft seat device are arranged one behind the other, and the second aircraft seat device has an aircraft seat device transversal axis which is oriented orthogonally to an aircraft cabin longitudinal axis of an aircraft cabin,
• wherein the first aircraft seat device has an enclosure and the second aircraft seat device has an enclosure which forms a backrest wall at least in a subregion of the enclosure of the second aircraft seat device,
• wherein the first aircraft seat device and the second aircraft seat device together form an aircraft seat region for a passenger, which is arranged at least substantially between the enclosure of the first aircraft seat device and the enclosure of the second aircraft seat device,
• wherein the second aircraft seat device comprises in the aircraft seat region a seat bottom which has a seat bottom front edge, a main extension axis of the seat bottom front edge being oriented at an angle of at least 5 degrees with respect to the aircraft seat device transversal axis of the second aircraft seat device,
• wherein the first aircraft seat device comprises in the aircraft seat region an ottoman, which in a lying-down position of the aircraft seat region together with the seat bottom of the second aircraft seat device forms at least a portion of a lying-down surface of the aircraft seat region, and
• wherein a lying-down direction of the aircraft seat region, which is directed from a head region of the lying-down surface to a foot region of the lying-down surface, is oriented at an angle of at least 30 degrees with respect to the aircraft seat device longitudinal axis of the second aircraft seat device, the lying-down direction being directed away from an access region of the aircraft seat region.