Abstract: This fuselage comprises a wall and side doors as well as a space arranged behind the side door (10) the farthest to the rear of the aircraft. The space for work and storage is delimited by side walls (4) formed by the fuselage of the aircraft and by a transverse bulkhead (8). This space comprises housings (20) for carts arranged along the said transverse bulkhead (8). An aisle (24) serves the housings (20) arranged along the transverse bulkhead (8) and has a transverse portion (26) that is arranged entirely behind the side door (10) the farthest to the rear of the aircraft. At least one housing (22) for a cart (16) is arranged on the other side of the transverse portion (26) of the aisle (24) in relation to the housings (20) arranged along the wall, and each of the said housings (20, 22) for accommodating a cart (16) extends longitudinally in relation to a longitudinal axis (6) relative to the aircraft.

Abstract: A seat for an aircraft includes a seating surface, a backrest and two armrests. The seat also includes a mechanism for guiding at least one of the armrests in translation in an essentially-vertical direction.

Abstract: The invention relates to a seating unit for aircraft comprising at least one seat (4) and means making the said seat pivoting around a more or less vertical axis, characterized in that it comprises: an individual plate (10) for each seat, on which the said seat is assembled pivoting, a platform (6) adapted in order to be able to be fastened onto conventional rails for accommodating aircraft seats, means for translatory guidance (12, 14) of each individual plate (10) in relation to the platform (6) along a more or less horizontal direction, means for immobilization (24, 26) making it possible to immobilize on the one hand each individual plate (10) in relation to the platform (6) in its translatory movement, and on the other hand each seat (4) in relation to its individual plate (10) in its rotary movement.

Abstract: An aircraft fuselage includes an outer skin and at least one main deck separating an interior space of the aircraft fuselage longitudinally into a first space and a second space. At least one portion of the first space is divided into at least three longitudinal zones, and the at least three longitudinal zones include at least one central zone and at least two lateral zones. The at least one central zone is divided into three sectors, and the three sectors include a front sector, a central sector, and a rear sector. The at least two lateral zones include a first and second lateral zone configuration, the front sector includes a first and second front sector configuration, the central sector includes a first and second central sector configuration, and the rear sector includes a first and second rear sector configuration.

Abstract: This collapsible staircase is provided with a set of flat parts (6) each intended to function as steps. Each flat part (6) can be moved between a first position and a second position. All the flat parts (6) are substantially coplanar when they are in their first position, and are disposed one above the other and at a distance from one another when they are all in their second position. Advantageously, a retractable holding handle (44) is also provided and driven in movement together with the flat parts (6).

Abstract: This rest compartment is intended for at least one aircraft pilot. The said aircraft has a cockpit behind which there is located a first monument (4) separated from a second monument (6) by an aisle (8). A berth (12) is arranged at least partially above the aisle (8) separating the two monuments. One monument (6) is laid out so that it comprises an access to the berth (12).

Abstract: This layout shows a set or assembly of aircraft seats to outfit an aircraft cabin, comprising at least two columns of neighboring seats. The seats are arranged one behind the other in each of the columns of seats. Moreover, each seat can be converted into a sleeper so as to present a considerably stretched out sleeping surface. Each seat when converted into a sleeper, has a first sleeping portion and at least a second sleeping portion that is narrower than the first. In two neighboring columns, the seats are staggered, in such a way that the first part of a seat of a column is facing a second portion of a seat of the second column that is narrower in width.

Abstract: The invention relates to a seat which is intended for an aircraft and which comprises a seating surface (2), a backrest (4) and two armrests (8). The inventive seat also comprises means for guiding at least one of the armrests (8) in translation in an essentially-vertical direction.

Abstract: This module (8) for aircraft passenger(s) is provided with: two seats (10) disposed beside one another and oriented in the same direction, each of these seats (10) being a seat that can be converted to a berth, a side wall (14) surrounding the two seats (10), at least partly, an opening (16) provided in the side wall (14) to permit access to the module (8), and a partition (18) intended to achieve separation between the two seats (10), this partition (18) being displaceable from a first position, in which it achieves separation of the two seats (10), to a second stored position, in which it does not form a barrier between the two seats (10).

Abstract: An aircraft cabin according to the invention is provided with: a longitudinal cabin wall (2), seats (8) disposed in rows that are transversal relative to a longitudinal aisle (18), transversal accesses (20) permitting access to the seats (8) of the transversal rows closest to the cabin wall (2), and at least one storage space (24) disposed in the immediate proximity of the longitudinal cabin wall (2) and at the dead end of a transversal access (20).

Abstract: This door (2) is intended for a compartment, such as an aircraft baggage compartment, which door can be moved between a first position, in which it closes an opening of the compartment, and a second position, in which the said opening is accessible. This door (2) is provided on both sides of the opening of the compartment with guide means (20, 22), so as to guide the door (2) in a substantially vertical translational movement.

Abstract: In an arrangement according to the invention, an aircraft cabin segment is provided with: at least one longitudinally extending aisle (8), seats disposed in rows that are transversal relative to the longitudinal aisles (8), at least one assembly of baggage compartments (12) that are aligned and positioned overhead, the baggage compartments (12) being aligned in transversal direction and positioned above seats.

Abstract: This aircraft fuselage comprises an outer skin and at least one main deck defining an occupancy space. At least one portion of the occupancy space is divided into at least three longitudinal zones, at least one central zone and at least two lateral zones. The lateral zones are adapted to hold either seats for accommodating passengers, or freight. At least one central zone is adapted to hold freight over at least a portion of its length. At least one lateral zone comprises an aisle for the passage, in a transverse direction, of the freight placed in a central zone.

Abstract: This layout shows a set or assembly of aircraft seats to outfit an aircraft cabin, comprising at least two columns of neighboring seats. The seats are arranged one behind the other in each of the columns of seats. Moreover, each seat can be converted into a sleeper so as to present a considerably stretched out sleeping surface. Each seat when converted into a sleeper, has a first sleeping portion and at least a second sleeping portion that is narrower than the first. In two neighboring columns, the seats are staggered, in such a way that the first part of a seat of a column is facing a second portion of a seat of the second column that is narrower in width.