Rotatable cabin attendant seat and aircraft monument arrangement with a rotatable cabin attendant seat

1. A cabin attendant seat comprising:

a backrest element,

a seat element which is fastened to the backrest element, the backrest element being rotatable about a rotation axis in order to move the cabin attendant seat between a rest position and an operating position, and

a fastening device for fastening the cabin attendant seat to a side wall of an aircraft monument, the fastening device being 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 during operation of the cabin attendant seat via the side wall of the aircraft monument, wherein:

the fastening device comprises a frame having a first, a second, a third and a fourth frame element,

when the cabin attendant seat is in the operating position, the first frame element is mounted substantially perpendicular to and above an upper portion of the fourth frame element and orientated substantially parallel with and located above an upper side of a headrest of the cabin attendant seat, the second frame element is orientated substantially parallel with a rear side of the backrest element of the cabin attendant seat, the third frame element is orientated substantially parallel with a lower side of the seat element of the cabin attendant seat and the fourth frame element is orientated substantially parallel with a first side face of the backrest element of the cabin attendant seat, and

when the cabin attendant seat is in the rest position, the second frame element is oriented substantially parallel to a second side face of the backrest element of the cabin attendant seat, and the fourth frame element is oriented substantially parallel to the rear side of the backrest element of the cabin attendant seat.

2. The cabin attendant seat according to claim 1 , wherein the third frame element is formed by a portion of an upper boundary wall of a storage compartment which is arranged below the cabin attendant seat when the cabin attendant seat is mounted in an aircraft cabin.

3. The cabin attendant seat according to claim 1 , wherein a first portion of the fourth frame element is constructed integrally with the first frame element and in that a second portion of the fourth frame element that is not constructed integrally with the first frame element is received in a groove which is delimited by a surface of the first frame element facing the fourth frame element and a part-region of the first portion of the fourth frame element that is constructed integrally with the first frame element.

4. The cabin attendant seat according to claim 1 , wherein at least one bore for receiving a fastening element for fastening the frame to the side wall of the aircraft monument is constructed in the fourth frame element.

5. The cabin attendant seat according to claim 1 , wherein the backrest element comprises a receiving device which is provided with an inner thread, and in that a portion of the rotation axis that is provided with an outer thread is screwed in the receiving device in order to connect the rotation axis to the backrest element.

6. The cabin attendant seat according to claim 1 , wherein the fastening device comprises a first connection device for rotatably connecting the rotation axis to the frame, in particular the first frame element and/or a second connection device for rotatably connecting the rotation axis to the frame, in particular the third frame element.

7. The cabin attendant seat according to claim 6 , wherein the first and/or the second connection device comprise(s) a bore which is provided with a radially inwardly protruding flange for receiving the rotation axis.

8. The cabin attendant seat according to claim 7 , wherein a first surface of the flange forms an abutment face for a head of a rotation axis that is constructed in the form of a pin and/or in that a second surface of the flange opposite the first surface forms an abutment face for a bearing which is at least partially received in the bore.

9. The cabin attendant seat according to claim 8 , wherein the bearing is retained in its position in the bore by means of a resilient ring, the resilient ring being supported in particular in a groove which is formed in a wall of the bore.

10. The cabin attendant seat according to claim 1 , wherein the rotation axis is connected to the backrest element with spacing from the first side face ( 32 ) of the backrest element ( 20 ) in the region of a front side of the backrest element ( 20 ).

11. The cabin attendant seat according to claim 1 , wherein an edge formed by the first side face and a rear side of the backrest element is constructed in a rounded manner.

12. The cabin attendant seat according to claim 11 , further comprising a lining which is configured to cover the rounded edge of the backrest element when the cabin attendant seat is located in its rest position.

13. An aircraft monument arrangement comprising:

an aircraft monument and

a cabin attendant seat which is fastened to a side wall of the aircraft monument according to claim 1 .

14. The aircraft monument arrangement according to claim 13 , characterised by a storage compartment which adjoins the cabin attendant seat adjacent to the second frame element.