An aircraft cabin attendant seat is disclosed. In some embodiments, the aircraft cabin attendant seat includes a support element extending from a cabin floor. The support element includes at least two coupled support element subsections configured to at least one of slide or fold onto each other. In some embodiments, a coupler is configured to attach the support element to the cabin floor. The aircraft cabin attendant seat further includes a backrest and a headrest that is coupled to the support element. The aircraft cabin attendant seat includes a seating portion coupled to the support element. The seating portion includes both seat and a hinge configured to connect the seat to the support element, where the seat is configured to retract from a seated position into a storage position.

Disclosed is a door assembly for enclosing a compartment, for instance a cabin attendant seat (CAS) compartment. The assembly generally includes spaced guides for guiding opening and closing movement of a bi-fold door including coupled upper and lower door sections. The door sections are coupled through an interface that allows vertical displacement of the lower door section relative to the upper door section when the door assembly is in the closed condition to engage or disengage latches from respective catches. In some embodiments, the assembly further includes cam latches and a biasing mechanism for driving bi-fold door movement toward the open condition, among other features.

A slim aircraft monument is installable in an aircraft cabin adjacent to an aisle and has an upper portion, a lower portion, and a middle portion between the upper and lower portions. The monument includes a storage compartment accessible from a first side and a door on an adjacent side, the door deployable into the adjacent aisle or cabin space to reveal folding interconnected panels also deployable into the cabin space. The interconnected panels unfold into a horizontal workspace and, beneath the workspace, a series of vertically stacked storage bays capable of accommodating storage drawers and a cart bay configured for temporary accommodation of a half-size galley cart.

A flight attendant seat comprising a frame that can be mounted on a carrier fixture or integrated into the carrier fixture, and at least one seat arrangement integrated into the frame. The frame comprises a lower section, an upper section and a central section taking up the at least one seat arrangement, at least partially. The lower section is formed bent at least in a region adjoining the central section. A method is provided for fitting a flight attendant seat.

A deployable cabin attendant seat system may include a primary cabin attendant seat, an auxiliary cabin attendant seat, a main support coupled to at least one of the primary cabin attendant seat or the auxiliary cabin attendant seat, and an actuation assembly coupled to at least the primary cabin attendant seat. The actuation assembly may be configured to actuate the primary cabin attendant seat relative to the auxiliary cabin attendant seat between a stowed seat position and a deployed seat position. The primary cabin attendant seat and the auxiliary cabin attendant seat may be arranged in a side-by-side configuration when the primary cabin attendant seat is in the deployed seat position. The primary cabin attendant seat may be stacked on the auxiliary cabin attendant seat when the primary cabin attendant seat is in the stowed seat position.

Disclosed is a height adjustable seat pan assembly such as for use in an aircraft cabin attendant seat. The assembly includes a seat pan supported between spaced frame members defining guide tracks including successive pivot positions each corresponding to a different seat pan height. The seat pan is movable between a deployed condition and a stowed condition in which the seat pan stows generally vertically below a backrest to provide a low profile seat in the stowed condition. Features provided on opposing sides of the seat pan interact with the successive pivot positions in the guide tracks, and the seat can be repositioned to a different pivot position to change the seat pan height. Pivoting motion of the seat pan between the stowed and deployed conditions locks or unlocks the seat pan relative to its aligned successive pivot position.

An aircraft monument for use in a cabin of an aircraft includes a monument assembly and a seat assembly. The monument assembly includes a frame having a plurality of walls defining a compartment. The plurality of walls include a first end wall having a forward section at a forward plane of the frame. The compartment is defined rearward of the forward section. The seat assembly is forward of the frame. The seat assembly has a shell configured to at least partially surround a passenger seat. The shell has a rear rearward of the forward plane of the frame.

An aircraft seat system is disclosed, in accordance with one or more embodiments of the present disclosure. In one embodiment, the aircraft seat system includes a seat casement; a headrest portion; a seat back portion; a seat pan; and one or more armrests pivotably coupled to one or more portions of the seat casement. In another embodiment, the one or more armrests include an armrest body; a rotator link system; and a pivot link system. In another embodiment, the pivot link system may be configured to pivotably extend the armrest cap and pivotably retract the armrest cap.

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.

A stowable auxiliary compartment panel system may include an auxiliary compartment panel, an actuation assembly, and a latch assembly. The auxiliary compartment panel may be configured to transition between a stowed position and a deployed position via the actuation assembly. The auxiliary compartment panel may be configured to secure to the monument via the latch assembly when the auxiliary compartment panel is in the deployed position. An auxiliary compartment defined within the monument may be accessible when the auxiliary compartment panel is in the stowed position. The stowable auxiliary compartment panel system may be installed within an aircraft cabin.