Wing for an aircraft, comprising a droop panel pivotally attached at a connection point to the wing, a flaperon pivotally attached at a connection point to the wing, a support structure rigidly attached to the wing and a linkage mechanism for linking the flaperon to the droop panel, the linkage mechanism comprising a support structure linkage, a droop panel linkage, and a flaperon linkage, wherein the support structure linkage is pivotally attached at a pivot end to the support structure of the wing, wherein the droop panel linkage is pivotally attached at a first end to the droop panel, the first end of the droop panel linkage being spaced apart from the connection point of the droop panel, wherein the flaperon linkage is pivotally attached at a first end to the flaperon, the first end of the flaperon linkage being spaced apart from the connection point of the flaperon, wherein a second end of the droop panel linkage and a second end of the flaperon linkage are pivotally attached to a connecting section of the support structure linkage, wherein the connecting section is spaced apart from the pivot end of the support structure linkage, such that the linkage mechanism is configured to transfer a pivoting motion from the flaperon into a pivoting motion of the droop panel, and wherein the connecting section comprises at least two lever arms (65, 67), wherein the second end of the flaperon linkage is pivotally attached to a first lever arm of the at least two lever arms (65, 67) and the second end of the droop panel linkage is pivotally attached to a second lever arm of the at least two lever arms (65, 67), wherein the lever arms (65, 67) form an L-shape, wherein the first lever arm points to the droop panel and the second lever arm points to the flaperon, wherein the flaperon linkage and the droop panel linkage are pivotally linked and provide a direct linkage connection between the flaperon and the droop panel. a support structure linkage, a droop panel linkage, and a flaperon linkage, wherein the support structure linkage is pivotally attached at a pivot end to the support structure of the wing, wherein the droop panel linkage is pivotally attached at a first end to the droop panel, the first end of the droop panel linkage being spaced apart from the connection point of the droop panel, wherein the flaperon linkage is pivotally attached at a first end to the flaperon, the first end of the flaperon linkage being spaced apart from the connection point of the flaperon, wherein a second end of the droop panel linkage and a second end of the flaperon linkage are pivotally attached to a connecting section of the support structure linkage, wherein the connecting section is spaced apart from the pivot end of the support structure linkage, such that the linkage mechanism is configured to transfer a pivoting motion from the flaperon into a pivoting motion of the droop panel, and wherein the connecting section comprises at least two lever arms (65, 67), wherein the second end of the flaperon linkage is pivotally attached to a first lever arm of the at least two lever arms (65, 67) and the second end of the droop panel linkage is pivotally attached to a second lever arm of the at least two lever arms (65, 67), wherein the lever arms (65, 67) form an L-shape, wherein the first lever arm points to the droop panel and the second lever arm points to the flaperon,