A safety seat for an occupant includes a front shell secured to a bulkhead. The front shell has an outer edge and an inner edge. The inner edge defines an opening. The safety seat includes a seat base having a first side and a second side opposite the first side. The seat base has a first position and a second position. In the first position, the first side is flush with the inner edge and in the second position; the second side supports the occupant.

A support structure for a flight attendant seat, the support structure having supporting elements arranged at an upper and a lower end of the support structure. The supporting elements connect the support structure to an aircraft structure via fastening points, the support structure having receiving elements for receiving the flight attendant seat. The support structure has at least two substantially vertical elements and at least one substantially horizontal element. The vertical elements have at least one upper and one lower end, the supporting elements being attached to respective ends of the vertical elements and forming lattice struts. The support elements are designed to be connected to the aircraft structure at at least two attachment positions, at least two upper and two lower fastening points being selectable in their respective attachment position to the aircraft structure, at least one cabin element being adaptively attached to the support structure.

An aircraft assembly with first and second seat rails for interlocking with an aircraft seat, and a systems component mounting member interlocked with those seat rails. The mounting member has a first anchor member interlocked with the first seat rail and a second anchor member interlocked with the second seat rail. The assembly includes an aircraft systems component mounted on the mounting member. Existing seat rails or tracks of the aircraft can be used for attachment of support brackets for aircraft systems components. A novel way of using existing seat rails to provide anchorage points for systems brackets for systems components is disclosed.

The present disclosure provides a detachable cabin attendant seat (CAS). In various embodiments, the detachable CAS may comprise a first section, comprising, a first rod and a second rod, and a first post and a second post extending from the first section, wherein the first post and the second post are configured to be coupled to a mount assembly when the detachable CAS is in a stowed position and the first rod and the second rod are configured to be coupled to the mount assembly when the detachable CAS is in a deployed position.

A seat with self-stowage capability is provided. The seat includes a seat pan lever which is rotatable between stowed and open positions, a fixed seat structure and an elastic assembly. The fixed seat structure includes an annulus. The elastic assembly includes a damper and an arc-spring disposable within the annulus to permit first rotations of the seat pan lever from the stowed position to the open positions and to urge second rotations of the seat pan lever from the open positions to the stowed position.

An apparatus for use with a wall and by a person leaning against the wall and including: a receiver mounted in use to the wall; a support having an operative position whereat the support generally follows the curvature of the buttocks of the person; and a mechanism adapted to suspend the support from the receiver at the operative position.

An example seat pan for an aircraft includes a first portion having a first end and a second portion that is adjacent to the first portion and is adjustable to be in a first position in which the second portion forms a seating surface together with the first portion, the seating surface having a width that is wider than a width of the first end of the first portion. The second portion is adjustable to alternatively be in a second position in which the first end of the first portion extends beyond the second portion to be insertable into a footwell.

A vehicle seat structure including: a seat cushion on which a vehicle occupant sits; a seat back that supports a back portion of the vehicle occupant while sitting on the seat cushion in a seat deployed state, the seat deployed state being a state in which the vehicle occupant is able to sit on the seat cushion; and a seat deploying/retracting mechanism that enables the seat cushion and the seat back to slide in a vehicle up-down direction, and that, in a seat retracted state in which the seat cushion and the seat back are retracted, enables the seat cushion and the seat back to be placed in the vehicle up-down direction such that the seat cushion stands upright, and the seat back is placed at an upper side of the seat cushion.

An aircraft comprises a fuselage and an aft wall of a lavatory monument within the fuselage and extending radially inwardly relative to the fuselage. The aft wall is removably connected to an outboard wall, a ceiling, and a floor of the lavatory monument.

A safety seat for an occupant includes a front shell secured to a bulkhead. The front shell has an outer edge and an inner edge. The inner edge defines an opening. The safety seat includes a seat base having a first side and a second side opposite the first side. The seat base has a first position and a second position. In the first position, the first side is flush with the inner edge and in the second position; the second side supports the occupant.