A cabin arrangement for a cabin of an aircraft having a cabin floor, a door region, and a galley module arranged on the cabin floor, the galley module comprising: - a base galley section and - a top galley section, wherein the base galley section comprises a top end adapted for carrying the top galley section, wherein the base galley section comprises a first functional arrangement (10, 12) with a first access direction in a horizontal plane, wherein a main part of the top galley section comprises at least one second functional arrangement having a second access direction in the horizontal plane and wherein the first access direction and the second access direction enclose an angle of 90° in the horizontal plane, wherein the first access direction of the base galley section faces to the door region of the aircraft, wherein the galley module comprises a first lateral surface and a second lateral surface, wherein the second lateral surface is positioned opposite to the first lateral surface, wherein the second lateral surface is curved, such that the second lateral surface rests flush on an interior surface of a cabin lining, which follows the contour of a fuselage of the aircraft, wherein the base galley section comprises a working surface, which extends from the first lateral surface of the base galley section to an access side of the top galley section, and wherein a depth of the top galley section is smaller than the width of the base galley section, such that a fraction of a surface on the top end of the base galley section provides the working surface; wherein the galley module rests flush against an inner wall of the cabin, wherein an access side of the top galley section faces away from said inner wall. - a base galley section and - a top galley section, wherein the base galley section comprises a top end adapted for carrying the top galley section, wherein the base galley section comprises a first functional arrangement (10, 12) with a first access direction in a horizontal plane, wherein a main part of the top galley section comprises at least one second functional arrangement having a second access direction in the horizontal plane and wherein the first access direction and the second access direction enclose an angle of 90° in the horizontal plane, wherein the first access direction of the base galley section faces to the door region of the aircraft, wherein the galley module comprises a first lateral surface and a second lateral surface, wherein the second lateral surface is positioned opposite to the first lateral surface, wherein the second lateral surface is curved, such that the second lateral surface rests flush on an interior surface of a cabin lining, which follows the contour of a fuselage of the aircraft, wherein the base galley section comprises a working surface, which extends from the first lateral surface of the base galley section to an access side of the top galley section, and wherein a depth of the top galley section is smaller than the width of the base galley section, such that a fraction of a surface on the top end of the base galley section provides the working surface; wherein the galley module rests flush against an inner wall of the cabin, wherein an access side of the top galley section faces away from said inner wall. wherein the base galley section comprises a top end adapted for carrying the top galley section, wherein the base galley section comprises a first functional arrangement (10, 12) with a first access direction in a horizontal plane, wherein a main part of the top galley section comprises at least one second functional arrangement having a second access direction in the horizontal plane and wherein the first access direction and the second access direction enclose an angle of 90° in the horizontal plane, wherein the first access direction of the base galley section faces to the door region of the aircraft, wherein the galley module comprises a first lateral surface and a second lateral surface, wherein the second lateral surface is positioned opposite to the first lateral surface, wherein the second lateral surface is curved, such that the second lateral surface rests flush on an interior surface of a cabin lining, which follows the contour of a fuselage of the aircraft, wherein the base galley section comprises a working surface, which extends from the first lateral surface of the base galley section to an access side of the top galley section, and wherein a depth of the top galley section is smaller than the width of the base galley section, such that a fraction of a surface on the top end of the base galley section provides the working surface; wherein the galley module rests flush against an inner wall of the cabin, wherein an access side of the top galley section faces away from said inner wall.