A monument for installation in an aircraft passenger cabin comprises a housing extending from the floor upwardly toward the ceiling, the housing including a first configuration configured to receive a wheelchair in a first unfolded condition, and a second configuration configured to receive a stretcher in a second unfolded condition, a first interior space formed in the housing, a staircase disposed within the interior space; a second interior space formed in the housing, a first entrance into the first interior space through a door; a second entrance into the second interior space of the housing, and a securement assembly positionable on the floor, the securement assembly configured to secure one of the wheelchair or the stretcher in place within the interior space.

An aircraft lavatory is disclosed herein. The aircraft lavatory includes a standard access door providing access to the aircraft lavatory from at least one of an aisle, a cross aisle, or a passageway of an aircraft, a first moveable wall adjacent the standard access door, the first moveable wall having a first end and a second end and configured to move between a closed position and an open position, the first end of the first moveable wall configured to rotate about a first pivot point, and a second moveable wall adjacent the first moveable wall, the second movable wall having a first end and a second end and configured to move between a closed position and an open position, the first end of the second moveable wall configured to rotate about a second pivot point.

A sleeping apparatus comprising a textile fiber shell, a plurality of adjustable straps coupled to the textile fiber shell and a plurality of anchors, wherein each anchor is coupled to one of the plurality of adjustable straps, wherein the anchors are configured to attach to one or more structures such that the textile fiber shell forms a flat sleeping surface.

A toilet module for a vehicle is provided. The toilet module comprises a housing having a front wall, a first functional wall and at least one second functional wall, which enclose a floor surface on the underside of the housing, and a toilet unit. The front wall comprises an access opening. The first functional wall is arranged opposite the front wall and accommodates the toilet unit. The at least one second functional wall extends between the first functional wall and the front wall and is perpendicular to the front wall. The toilet unit has a longitudinal extension axis which forms an angle which is greater than 0 with the at least one second functional wall. In this way, a particularly narrow and compact toilet module can be provided.

The present disclosure includes litter platform support and positioning systems described generally comprising at least one lift column mounted to an interior floor in an emergency vehicle or structure. The lift column is connected to at least one support assembly, the at least one support assembly adapted to receive and position a litter assembly. In some implementations, the support assembly is connected to the lift column and adapted to independently adjust the litter assembly vertically, laterally, longitudinally, and rotate 360. The litter platform support and positioning system further includes at least one individual motor associated with each lift column which is operatively connected to a drive screw to independently adjust and control the location of each support assembly to individually position a corresponding litter platform assembly.

A cover panel for a core panel of a structural aircraft component includes a protection cover having an outer shape corresponding to the outer shape of the core panel and including at least one cutout aperture, and at least one fabric panel mounted to the protection cover and covering the at least one cutout aperture.

An aircraft lavatory is disclosed herein. The aircraft lavatory includes a standard access door providing access to the aircraft lavatory from at least one of an aisle, a cross aisle, or a passageway of an aircraft, a first moveable wall adjacent the standard access door, the first moveable wall having a first end and a second end and configured to move between a closed position and an open position, the first end of the first moveable wall configured to rotate about a first pivot point, and a second moveable wall adjacent the first moveable wall, the second movable wall having a first end and a second end and configured to move between a closed position and an open position, the first end of the second moveable wall configured to rotate about a second pivot point.

An aircraft region comprising a main aisle extending along a longitudinal axis of an aircraft cabin, a door aisle extending along a transverse axis of the aircraft cabin substantially perpendicularly to the main aisle and an aircraft monument arranged in the door aisle and comprising at least one flight attendant seat facing a section of the main aisle adjoining the door aisle.

A portable aircraft stretcher for supporting a person on an aircraft, the stretcher configured for location in a port-starboard orientation across three or four side-by-side commercial aircraft seats. The stretcher includes a seat and a backrest. The backrest has a reclined orientation for supporting the person in a reclined position across and above the three or four aircraft seats. The stretcher further includes a support member extending downwardly from the backrest for supporting the backrest. The stretcher further includes a harness for securing the person to the stretches and one or more connection points configured to engage with at least one aircraft seatbelt of the three or four aircraft seats for securing the stretcher to the aircraft seats.

The invention provides aeromedical ambulance equipment. In some embodiments, the equipment includes a module base comprising a mount assembly having an unlocked configuration and a locked configuration. The mount assembly preferably can be adjusted between the unlocked and locked configurations by a tool-free operation. In addition, certain embodiments provide a module base having an advantageous system for releasably locking a stretcher onto the module base.