Frame component for a frame of a fuselage structure of an aircraft , comprising: a central web extending along a longitudinal direction (L1), which has an inner edge region with respect to a radial direction (R1) extending transversely to the longitudinal direction (L1) and an outer edge region with respect to the radial direction (R1); 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 (M) 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 (L1), the central web having, at an end region adjoining the connecting region with respect to the longitudinal direction (L1), 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 (R1); 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 (T1) extending transversely to the radial direction and to the longitudinal direction. a central web extending along a longitudinal direction (L1), which has an inner edge region with respect to a radial direction (R1) extending transversely to the longitudinal direction (L1) and an outer edge region with respect to the radial direction (R1); 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 (M) 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 (L1), the central web having, at an end region adjoining the connecting region with respect to the longitudinal direction (L1), 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 (R1); 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 (T1) extending transversely to the radial direction and to the longitudinal direction. <EOS>