Abstract: An aircraft lavatory comprising an enclosure having a door, a first side wall, a rear wall, a ceiling, and a second side wall, wherein the second side wall includes a sink, the second side wall defining a plane and wherein the sink is inwardly disposed from said plane. To create space for a stowage compartment, an additional side wall parallel to, and adjacent to, said second side wall is formed. This space houses a stowage compartment accessible from outside said lavatory, the stowage compartment formed between said second side wall and said additional wall.

Abstract: An aircraft lavatory comprising an enclosure having a door, a first side wall, a rear wall, a ceiling, and a second side wall, wherein the second side wall includes a sink, the second side wall defining a plane and wherein the sink is inwardly disposed from said plane. To create space for a stowage compartment, an additional side wall parallel to, and adjacent to, said second side wall is formed. This space houses a stowage compartment accessible from outside said lavatory, the stowage compartment formed between said second side wall and said additional wall.

Abstract: An aircraft lavatory comprising an enclosure having a door, a first side wall, a rear wall, a ceiling, and a second side wall, wherein the second side wall includes a sink, the second side wall defining a plane and wherein the sink is inwardly disposed from said plane. To create space for a stowage compartment, an additional side wall parallel to, and adjacent to, said second side wall is formed. This space houses a stowage compartment accessible from outside said lavatory, the stowage compartment formed between said second side wall and said additional wall.

Abstract: An aircraft lavatory comprising an enclosure having a door, a first side wall, a rear wall, a ceiling, and a second side wall, wherein the second side wall includes a sink, the second side wall defining a plane and wherein the sink is inwardly disposed from said plane. To create space for a stowage compartment, an additional side wall parallel to, and adjacent to, said second side wall is formed. This space houses a stowage compartment accessible from outside said lavatory, the stowage compartment formed between said second side wall and said additional wall.

Abstract: An aircraft lavatory comprising an enclosure having a door, a first side wall, a rear wall, a ceiling, and a second side wall, wherein the second side wall includes a sink, the second side wall defining a plane and wherein the sink is inwardly disposed from said plane. To create space for a stowage compartment, an additional side wall parallel to, and adjacent to, said second side wall is formed. This space houses a stowage compartment accessible from outside said lavatory, the stowage compartment formed between said second side wall and said additional wall.

Abstract: An aircraft lavatory comprising an enclosure having a door, a first side wall, a rear wall, a ceiling, and a second side wall, wherein the second side wall includes a sink, the second side wall defining a plane and wherein the sink is inwardly disposed from said plane. To create space for a stowage compartment, an additional side wall parallel to, and adjacent to, said second side wall is formed. This space houses a stowage compartment accessible from outside said lavatory, the stowage compartment formed between said second side wall and said additional wall.

Abstract: An aircraft interior panel for supporting high-weight loads including a core panel sandwiched between structural plies, a panel insert embedded in the panel and passing through and interrupting the core panel, the insert having an elongate stem capped on each end with an enlarged flange, the elongate stem being arranged axially perpendicular to the core panel and the enlarged flanges being arranged parallel to the core panel, and facing sheets bonded outward of the panel insert for concealing the panel insert within the aircraft interior panel.

Abstract: A method and apparatus for assembling an aircraft. A wing spar fitting is connected to a spar in a wing for the aircraft. A body frame fitting is connected to a frame in a body for the aircraft. The locations and orientations of the body frame fitting and the wing spar fitting allow for the body frame fitting to be attached to the wing spar fitting when the wing is positioned for attachment to the body of the aircraft. The wing is positioned with respect to the body of the aircraft for attachment to the body. The body frame fitting and the wing spar fitting are attached to each other with a set of fasteners after the body frame fitting is aligned to the wing spar fitting without penetrating any sealed areas in the wing, wherein the wing is attached to the body by a mechanical joint that is formed by the body frame fitting and the wing spar fitting.

Abstract: A method and apparatus for assembling an aircraft. A wing spar fitting is connected to a spar in a wing for the aircraft. A body frame fitting is connected to a frame in a body for the aircraft. The locations and orientations of the body frame fitting and the wing spar fitting allow for the body frame fitting to be attached to the wing spar fitting when the wing is positioned for attachment to the body of the aircraft. The wing is positioned with respect to the body of the aircraft for attachment to the body. The body frame fitting and the wing spar fitting are attached to each other with a set of fasteners after the body frame fitting is aligned to the wing spar fitting without penetrating any sealed areas in the wing, wherein the wing is attached to the body by a mechanical joint that is formed by the body frame fitting and the wing spar fitting.