Abstract: A cabin attendant seat including a carrier element which comprises a backrest section and a base section that carries the backrest section and a seat element fastened to a front side of the carrier element. At least one first stowage compartment is integrated into the carrier element. An inclined section of a rear wall of the carrier element is inclined, at least along a section of the first stowage compartment integrated into the carrier element, in such a way that a cross-sectional area of the carrier element increases in the direction of the base section of the carrier element.

Abstract: A cabin attendant seat (14) comprises a backrest element (20) and a seat element (22) which is secured to the backrest element (20). The backrest element (20) is rotatable about a rotation axis (24a, 24b) in order to move the cabin attendant seat (14) between a rest position and an operating position. A fastening device (18) for fastening the cabin attendant seat (14) to a side wall (16) of an aircraft monument (12) is constructed and sized in such a manner that it is capable of directing away a predetermined maximum force which can be introduced into the cabin attendant seat (14) during operation of the cabin attendant seat (14) via the side wall (16) of the aircraft monument (12).

Abstract: A cabin attendant seat comprising a carrier element which comprises a backrest section and a base section that carries said backrest section. A seat element is fastened to the carrier element. At least one first stowage compartment is integrated into said carrier element. A section of a rear wall of the carrier element is inclined, at least along a section of the stowage compartment integrated into said carrier element, in such a way that a cross-sectional area of said carrier element increases in the direction of the base section of said carrier element.