Wing for an aircraft

A high lift assembly for a wing of an aircraft, the high lift assembly comprising:

• a high lift body, and
• a connection assembly for movably connecting the high lift body to the wing, such that the high lift body is configured to move between a retracted position and at least one extended position,
• wherein the connection assembly comprises a first connection element and a second connection element,
• wherein the first connection element is configured to be movably mounted to the wing and is mounted to the high lift body, and
• wherein the second connection element is configured to be movably mounted to the wing and is mounted to the high lift body in a position spaced apart from the first connection element in a wing span direction,
• wherein the connection assembly comprises a drive system configured to be mounted to the wing and that is connected to the high lift body for driving the high lift body between the retracted position and the at least one extended position,
• wherein the connection assembly comprises a sync arrangement coupled between the first connection element and the second connection element,
• wherein the sync arrangement comprises a first engagement track having an uneven surface and coupled to the first connection element, a second engagement track having an uneven surface and coupled to the second connection element, and a locking mechanism engaging the first engagement track and the second engagement track when the high lift body is moved between the retracted position and the at least one extended position, and
• wherein the locking mechanism is configured such that the locking mechanism permits synchronous movement of the first connection element and the second connection element and restricts asynchronous movement of the first connection element and the second connection element by interlocking with the first engagement track and the second engagement track.