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 , wherein the second end of the flaperon linkage is pivotally attached to a first lever arm of the at least two lever arms and the second end of the droop panel linkage is pivotally attached to a second lever arm of the at least two lever arms , wherein the lever arms 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 , wherein the second end of the flaperon linkage is pivotally attached to a first lever arm of the at least two lever arms and the second end of the droop panel linkage is pivotally attached to a second lever arm of the at least two lever arms , wherein the lever arms form an L-shape, wherein the first lever arm points to the droop panel and the second lever arm points to the flaperon , <EOS>