Abstract: An aircraft including a cabin inside which a floor is installed, and at least one arranging module which is fixed solely to the floor and which includes a front wall, a rear wall, a port-side wall and a starboard-side wall which are rigidly connected to one another. The port-side and starboard-side walls each have a door, a roof and a deck fixed to each of the front, rear, port-side and starboard-side walls, and a separating system which makes it possible to separate the internal volume of the arranging module into two volumes, each being accessible through one of the doors. Such an aircraft therefore provides an arranging module which is fixed solely to the floor of the cabin, thereby facilitating the set-up thereof.

Abstract: A retractable chair for an aircraft cabin which is connected in use to a wall of the cabin, and includes an articulated frame having a back and a seat; a support which is connected to the frame, and fitted such as to be mobile on the wall around an axis of rotation; and at least one covering stretched on the frame. The fact of pivoting the support relative to the wall makes it possible to be able to incline the back, which contributes towards improving the comfort of the chair.

Abstract: An passenger cabin of an aircraft including a floor (108) on which are mounted a front seat (104a), a rear seat (104b) and a partition wall separating the front and rear seats, wherein the front seat (104a) pivots about an axis perpendicular to the floor (108) through an angle of at least 180 degrees, and the partition wall (106) has a fixed lower portion (106a) and a removable upper portion, and wherein a securing means has a securing position which secures the upper portion to the lower portion (106a), and a release position which allows the upper portion to detach from the lower portion (106a). The pivoting front seat and partition wall with detachable upper portion provide a first configuration seating configures that provides confidentiality between two passengers seated one behind the other, and a second configuration that permits communication between the seated passengers.

Abstract: An aircraft including a cabin inside which a floor is installed, and at least one arranging module which is fixed solely to the floor and which includes a front wall, a rear wall, a port-side wall and a starboard-side wall which are rigidly connected to one another. The port-side and starboard-side walls each have a door, a roof and a deck fixed to each of the front, rear, port-side and starboard-side walls, and a separating system which makes it possible to separate the internal volume of the arranging module into two volumes, each being accessible through one of the doors. Such an aircraft therefore provides an arranging module which is fixed solely to the floor of the cabin, thereby facilitating the set-up thereof.

Abstract: An passenger cabin of an aircraft including a floor (108) on which are mounted a front seat (104a), a rear seat (104b) and a partition wall separating the front and rear seats, wherein the front seat (104a) pivots about an axis perpendicular to the floor (108) through an angle of at least 180 degrees, and the partition wall (106) has a fixed lower portion (106a) and a removable upper portion, and wherein a securing means has a securing position which secures the upper portion to the lower portion (106a), and a release position which allows the upper portion to detach from the lower portion (106a). The pivoting front seat and partition wall with detachable upper portion provide a first configuration seating configures that provides confidentiality between two passengers seated one behind the other, and a second configuration that permits communication between the seated passengers.

Abstract: A retractable chair for an aircraft cabin which is connected in use to a wall of the cabin, and includes an articulated frame having a back and a seat; a support which is connected to the frame, and fitted such as to be mobile on the wall around an axis of rotation; and at least one covering stretched on the frame. The fact of pivoting the support relative to the wall makes it possible to be able to incline the back, which contributes towards improving the comfort of the chair.

Abstract: An aircraft fuselage comprising a structural wall and a floor delimiting a cabin for passengers, said wall being covered by a plurality of adjacent trim panels arranged in succession in the longitudinal direction of the fuselage and spaced from one another with a gap between two adjacent panels. Each panel is also fixed to the wall and has a concave shape adapted to the shape of the fuselage. At least one lighting device is disposed at the level of at least one of the gaps and is arranged perpendicularly to a longitudinal axis of the fuselage. The lighting device comprises a housing fixed to the wall. The housing is provided with an opening on a face oriented toward the interior of said cabin. The housing further comprises at least one lighting element making it possible to light the cabin through the gap.

Abstract: An aircraft fuselage provided with interior fit-out equipment, including a structure and decorative panels fixed to the structure one after the other at the level of at least one fixing point by a detachable link and delimiting a cabin. The fuselage further includes interior fit-out equipment disposed between two neighboring decorative panels which includes a base fixed to the fuselage, a flap mounted movably in respect of the base between a closed position in which the fixing points are hidden and inaccessible and an open position in which the fixing points are visible and accessible, and a lock that can be moved between a locked position in which the flap is kept in the closed position and an unlocked position in which the flap is free to move from the closed position into the open position and vice versa. Access to the fixing points is easy by moving the flap.

Abstract: An aircraft fuselage comprising a structural wall and a floor delimiting a cabin for passengers, said wall being covered by a plurality of adjacent trim panels arranged in succession in the longitudinal direction of the fuselage and spaced from one another with a gap between two adjacent panels. Each panel is also fixed to the wall and has a concave shape adapted to the shape of the fuselage. At least one lighting device is disposed at the level of at least one of the gaps and is arranged perpendicularly to a longitudinal axis of the fuselage. The lighting device comprises a housing fixed to the wall. The housing is provided with an opening on a face oriented toward the interior of said cabin. The housing further comprises at least one lighting element making it possible to light the cabin through the gap.