Patent ID: 8439589

Claim:
An arrangement, comprising: an aircraft interior fitting component, a bearing component, and a device for rotatably bearing the aircraft interior fitting component at the bearing component, the device comprising: a bearing bush fastened to one of the aircraft interior fitting component or the bearing component; a bearing bolt which is adapted to be rotatably accommodated in the bearing bush; and a bearing bolt guide fastened to the other of the aircraft interior fitting component or the bearing component, wherein the bearing bolt is disposed in the bearing bolt guide such that it is movable along a longitudinal axis of the bearing bolt guide between a first and a second position and retainable in at least one position in the bearing bolt guide by a retaining device, wherein the bearing bolt is disengaged from the bearing bush in the first position and is rotatably accommodated in the bearing bush in the second position, and wherein in at least one of the first and second positions, the retaining device fixes the bearing bolt against further rotational and longitudinal movement relative to the bearing bolt guide and away from the other of the first and second positions.