Abstract: An aircraft with a potable water system enabling the connection of monuments to preinstalled aircraft potable water interfaces by customized piping, which is routed within raceways for example directly along seat rails, and an installation method.

Abstract: An aircraft with a potable water system to feed potable water from a potable water tank to a consumer equipment of a monument in the aircraft cabin, including potable water interfaces, and at least one monument, with at least one opening in the monument to establish a fluid connection to the consumer equipment, wherein at least one potable water interface is accessible through the at least one opening, and an assembly method for installing a potable water system wherein standard parts of the potable water system are preinstalled and customized parts are installed later on.

Abstract: An aircraft window arrangement comprising a sidewall lining panel which is provided with a window opening, an inner window attached to the sidewall lining panel and extending across the window opening formed in the sidewall lining panel and an outer window arranged at a distance from the inner window and extending across a window opening formed in an aircraft outer skin. The aircraft window arrangement further comprises a window funnel including an inner rim facing the inner window and extending along a circumference of the window opening formed in the sidewall lining panel, and an outer rim facing the outer window and extending along a circumference of the window opening formed in the aircraft outer skin. The window funnel is formed separate from the sidewall lining panel. The window funnel may be attached to a retainer for retaining the outer window.

Abstract: An aircraft monument comprising a first compartment and a cabin attendant seat having a backrest and a seat element. The seat element is movable relative to the backrest between a folded position, wherein a seat surface of the seat element extends substantially parallel to a backrest surface of the backrest, and an unfolded position, wherein the seat surface of the seat element extends substantially perpendicular to the backrest surface of the backrest. The cabin attendant seat is movable relative to the aircraft monument between a stowed position, wherein the cabin attendant seat, with the seat element being in its folded position, is received in the first compartment of the aircraft monument, and an operating position, wherein the cabin attendant seat is disposed outside of the first compartment of the aircraft monument in a position which allows the seat element to be moved into its unfolded position.

Abstract: A cabin attendant seat comprises a seat element and a backrest. The backrest is movable relative to the seat element between an upright position, wherein a backrest surface of the backrest extends at an angle of approximately 80 to 100° relative to a seat surface of the seat element, and a folded-back position, wherein the backrest surface of the backrest extends substantially co-planar with the seat surface of the seat element.

Abstract: An aircraft monument comprising a first compartment and a cabin attendant seat having a backrest and a seat element. The seat element is movable relative to the backrest between a folded position, wherein a seat surface of the seat element extends substantially parallel to a backrest surface of the backrest, and an unfolded position, wherein the seat surface of the seat element extends substantially perpendicular to the backrest surface of the backrest. The cabin attendant seat is movable relative to the aircraft monument between a stowed position, wherein the cabin attendant seat, with the seat element being in its folded position, is received in the first compartment of the aircraft monument, and an operating position, wherein the cabin attendant seat is disposed outside of the first compartment of the aircraft monument in a position which allows the seat element to be moved into its unfolded position.

Abstract: A cabin attendant seat comprises a seat element and a backrest. The backrest is movable relative to the seat element between an upright position, wherein a backrest surface of the backrest extends at an angle of approximately 80 to 100° relative to a seat surface of the seat element, and a folded-back position, wherein the backrest surface of the backrest extends substantially co-planar with the seat surface of the seat element.

Abstract: An aircraft window arrangement comprising a sidewall lining panel which is provided with a window opening, an inner window attached to the sidewall lining panel and extending across the window opening formed in the sidewall lining panel and an outer window arranged at a distance from the inner window and extending across a window opening formed in an aircraft outer skin. The aircraft window arrangement further comprises a window funnel including an inner rim facing the inner window and extending along a circumference of the window opening formed in the sidewall lining panel, and an outer rim facing the outer window and extending along a circumference of the window opening formed in the aircraft outer skin. The window funnel is formed separate from the sidewall lining panel. The window funnel may be attached to a retainer for retaining the outer window.