Frame component for a frame of a fuselage structure of an aircraft, comprising: a central web extending along a longitudinal direction, which has an inner edge region with respect to a radial direction extending transversely to the longitudinal direction and an outer edge region with respect to the radial direction; an inner web bent from the inner edge region of the central web towards a first side; an outer web bent from the outer edge region of the central web towards the first side, wherein the central web, the outer web and the inner web are made in one piece from a metal sheet and together define a C-shaped cross-section of the frame component; and at least one stringer recess formed in the outer web and in the outer edge region of the central web; wherein the central web has, in the region of the stringer recess, a first reinforcing formation which forms a projection on the first side of the central web; characterised in that the frame component (1; 1A) has a connecting region for connection to a further frame component (1; 1B), which connecting region forms one end of the frame component (1; 1A) in the longitudinal direction, the central web having, at an end region adjoining the connecting region with respect to the longitudinal direction, a second reinforcing formation in the form of a bead introduced from a second side of the central web, which bead forms a projection on the first side of the central web and extends at least partly along the radial direction; and wherein the connecting portion of the frame component is arranged relative to the end region of the frame component with an offset with respect to a thickness direction extending transversely to the radial direction and to the longitudinal direction. a central web extending along a longitudinal direction, which has an inner edge region with respect to a radial direction extending transversely to the longitudinal direction and an outer edge region with respect to the radial direction; an inner web bent from the inner edge region of the central web towards a first side; an outer web bent from the outer edge region of the central web towards the first side, wherein the central web, the outer web and the inner web are made in one piece from a metal sheet and together define a C-shaped cross-section of the frame component; and at least one stringer recess formed in the outer web and in the outer edge region of the central web; wherein the central web has, in the region of the stringer recess, a first reinforcing formation which forms a projection on the first side of the central web; characterised in that the frame component (1; 1A) has a connecting region for connection to a further frame component (1; 1B), which connecting region forms one end of the frame component (1; 1A) in the longitudinal direction, the central web having, at an end region adjoining the connecting region with respect to the longitudinal direction, a second reinforcing formation in the form of a bead introduced from a second side of the central web, which bead forms a projection on the first side of the central web and extends at least partly along the radial direction; and wherein the connecting portion of the frame component is arranged relative to the end region of the frame component with an offset with respect to a thickness direction extending transversely to the radial direction and to the longitudinal direction.