Assembly of individual seats intended to be installed in an aircraft cabin having a longitudinal axis, said assembly comprising: - a first seat (11.1) and a second seat (11.2) facing each other, each seat (11.1, 11.2) having an axis, - a central console arranged between the first seat (11.1) and the second seat (11.2), said central console comprising a first foot zone (20.1) and a second foot zone (20.2), - the first foot zone (20.1) being associated with the first seat (11.1) in front of which there is an opening of the first foot zone (20.1), - the second foot zone (20.2) being associated with the second seat (11.2) in front of which there is an opening of the second foot zone (20.2), the first seat (11.1) facing inwards in the direction of the axis of the aircraft cabin and the second seat (11.2) facing outwards in the opposite direction of the axis of the aircraft cabin, so that an axis of the first seat (11.1) forms a first non-zero angle with respect to a reference straight line (Dref) parallel to the axis of the aircraft cabin, an axis of the second seat (11.2) forming a second non-zero angle with respect to the reference straight line (Dref), characterized in that at least a part of the first seat (11.1) and the corresponding first foot zone (20.1) are adapted to define at least a part of a first bed surface (25.1) facing outwards in the opposite direction of the axis of the aircraft cabin, such that an axis of the first bed surface (25.1) forms a non-zero third angle with respect to the reference straight line (Dref), and in that at least a part of the second seat (11.2) and the corresponding second foot zone (20.2) are able to define at least a part of a second bed surface (25.2) facing inwards in the direction of the axis of the aircraft cabin, so that an axis of the second bed surface (25.2) forms a fourth non-zero angle with respect to to the reference line (Dref). - a first seat (11.1) and a second seat (11.2) facing each other, each seat (11.1, 11.2) having an axis, - a central console arranged between the first seat (11.1) and the second seat (11.2), said central console comprising a first foot zone (20.1) and a second foot zone (20.2), - the first foot zone (20.1) being associated with the first seat (11.1) in front of which there is an opening of the first foot zone (20.1), - the second foot zone (20.2) being associated with the second seat (11.2) in front of which there is an opening of the second foot zone (20.2), the first seat (11.1) facing inwards in the direction of the axis of the aircraft cabin and the second seat (11.2) facing outwards in the opposite direction of the axis of the aircraft cabin, so that an axis of the first seat (11.1) forms a first non-zero angle with respect to a reference straight line (Dref) parallel to the axis of the aircraft cabin, an axis of the second seat (11.2) forming a second non-zero angle with respect to the reference straight line (Dref), characterized in that at least a part of the first seat (11.1) and the corresponding first foot zone (20.1) are adapted to define at least a part of a first bed surface (25.1) facing outwards in the opposite direction of the axis of the aircraft cabin, such that an axis of the first bed surface (25.1) forms a non-zero third angle with respect to the reference straight line (Dref), and in that at least a part of the second seat (11.2) and the corresponding second foot zone (20.2) are able to define at least a part of a second bed surface (25.2) facing inwards in the direction of the axis of the aircraft cabin, so that an axis of the second bed surface (25.2) forms a fourth non-zero angle with respect to to the reference line (Dref). the first seat (11.1) facing inwards in the direction of the axis of the aircraft cabin and the second seat (11.2) facing outwards in the opposite direction of the axis of the aircraft cabin, so that an axis of the first seat (11.1) forms a first non-zero angle with respect to a reference straight line (Dref) parallel to the axis of the aircraft cabin, an axis of the second seat (11.2) forming a second non-zero angle with respect to the reference straight line (Dref), characterized in that at least a part of the first seat (11.1) and the corresponding first foot zone (20.1) are adapted to define at least a part of a first bed surface (25.1) facing outwards in the opposite direction of the axis of the aircraft cabin, such that an axis of the first bed surface (25.1) forms a non-zero third angle with respect to the reference straight line (Dref), and in that at least a part of the second seat (11.2) and the corresponding second foot zone (20.2) are able to define at least a part of a second bed surface (25.2) facing inwards in the direction of the axis of the aircraft cabin, so that an axis of the second bed surface (25.2) forms a fourth non-zero angle with respect to to the reference line (Dref).