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 an aircraft seat assembly provided as one continuous row generally including at least one passenger seat and a cabin attendant seat positioned at one end of the row, wherein the at least one passenger seat and the cabin attendant seat face in opposite directions. A transverse beam of the passenger seat frame portion of the assembly extends laterally outward to support a coupling assembly attached to the cabin attendant seat. In some cabin layouts, the aircraft seat assembly is positioned adjacent to a lateral passageway extending from a longitudinal aisle to an aircraft door such that the at least one passenger seat faces away from the lateral passageway and the cabin attendant seat faces toward the lateral passageway to position a seated cabin crew member with the passengers and proximate the aircraft door.

A vertical adjustment system for an aircraft seat is disclosed. The vertical adjustment system may include an actuation assembly. The actuation assembly may include an actuator configured to provide a vertical height adjustment for the aircraft seat. The actuation assembly may include a release mechanism configured to couple to a rotatory portion of the swivel plate. The actuation assembly may include a plurality of vertical stabilizer rods coupled to a portion of the tracking plate. The actuation assembly may include a pillow block assembly. The pillow block assembly may include a plurality of pillow blocks coupled to a portion of the swivel plate. The pillow block assembly may include a plurality of rollers coupled to a portion of the plurality of pillow blocks. The plurality of rollers may be configured to provide stability along the vertical stabilizer rods when the actuator provides the vertical height adjustment.

An electronic display apparatus comprising a support frame, wherein mounted within the support frame there is an electronic display configured to display content based on image data, and a display driver circuit to receive the image data and to supply an image signal to the electronic display to cause the electronic display to display the content, the image signal based on the image data. Also mounted in the support frame is a connector cable connecting the display driver circuit and the electronic display for transmission of the image signal from the display driver circuit to the electronic display. The support frame is mountable to one or more surfaces so as to mount the electronic display to a first portion of the one or more surfaces and mount the display driver circuit to a second portion of the one or more surfaces that is away from the first portion, and the support frame maintains the electronic display in a spaced relationship from the display driver circuit.

A passenger seat assembly can include a seat frame; a seat back supported by the seat frame, comprising a rearward surface, and moveable between a stowed position and a deployed position; and a monitor shroud positioned proximate to the rearward surface of the seat back and fixedly coupled to a stationary surface, wherein the monitor shroud remains stationary as the seat back moves between the stowed position and the deployed position, and the monitor shroud defines an opening that provides access to the rearward surface of the seat back.

Described are aircraft seats having a seat bottom coupled to a seat back and a linkage mechanism for reclining the seat. The reclining mechanism includes an actuator coupled to a recline lock linkage The actuator is movable between positions and moves the recline lock linkage about a pivot point to facilitate movement of the seat between an upright position and a deployed position.

An aircraft cabin (100) is disclosed. The aircraft cabin (100) comprises a plurality of pairs of seat units (120) positioned along an aisle (101). Each aisle seat unit (122 A) comprises an aisle seat (125A) and an aisle footwell (126 A) and each non-aisle seat unit (123 A) comprises a non-aisle seat (127 A) and a non-aisle footwell (128A). The aisle seat unit (122 A) and non-aisle seat unit (123A) are positioned with respect to one another such that the aisle seat (125A) faces towards a first end of the cabin (100) and has direct access to the aisle (101), the non-aisle seat (127A) faces towards a second, opposite end of the cabin (100). The aisle seat unit (122 A) is oriented at an angle with respect to the non-aisle seat unit (123 A) to provide the non-aisle seat unit (123 A) with an aisle access path (129 A) between the non-aisle seat (127 A) and the aisle footwell (126A). The width of the non-aisle footwell (128 A) is less than the width of the non-aisle seat (127A) and the aisle seat (125A) is positioned directly adjacent the non-aisle footwell (128A).

A seating module having a recessed grip for a vehicle, in particular an aircraft, and a seating arrangement that includes a seating module that has a recessed grip. The seating module includes a shell structure that defines the recessed grip in an upper area of the shell structure.

Described are aircraft door assemblies comprising a stationary portion comprising at least one translation track and a movable portion comprising at least one channel. The movable portion is slidably coupled to the stationary portion via at least an attachment plate. The aircraft door assembly comprises a locked state and an unlocked state. In the locked state, the attachment plate and the movable portion are slidable as a unit relative to the stationary portion along the at least one translation track. In the unlocked state, the movable portion is slidable relative to the attachment plate and the stationary portion along the at least one channel.

A passenger seat includes a spreader with one or more open slot. The slot may be positioned on a lateral side of the spreader and may receive a portion of a seat base of the passenger seat within the slot. In some aspects, the slot may be elongated, and an insertion opening for the slot is provided in a top side of the spreader.