A wing for an aircraft, comprising a main wing, a slat, and a connection assembly movably connecting the slat to the main wing, such that the slat can be moved between a retracted position and at least one extended position, wherein the connection assembly comprises a first connection station and a second connection station spaced apart from the first connection station in a wing span direction, wherein the first connection station comprises: a first linkage pivotally mounted to the main wing via a first joint and pivotally mounted to the slat via a second joint, a first slat track that is guided at the main wing for movement along a predefined path, and that is pivotally mounted to the slat via a third joint, and a first drive station including a first input section coupled to a drive shaft, a first gear unit, and a first output section drivingly coupled to the first slat track, wherein the second connection station comprises: a second linkage pivotally mounted to the main wing via a fourth joint and pivotally mounted to the slat via a fifth joint, a second slat track that is guided at the main wing for movement along a predefined path, and that is pivotally mounted to the slat via a sixth joint, and a second drive station including a second input section coupled to the drive shaft, a second gear unit, and a second output section drivingly coupled to the second slat track, characterized in that the connection assembly comprises a sync shaft coupling the first connection station to the second connection station for sync movement of the first and second connection stations (13, 15). a main wing, a slat, and a connection assembly movably connecting the slat to the main wing, such that the slat can be moved between a retracted position and at least one extended position, wherein the connection assembly comprises a first connection station and a second connection station spaced apart from the first connection station in a wing span direction, wherein the first connection station comprises: a first linkage pivotally mounted to the main wing via a first joint and pivotally mounted to the slat via a second joint, a first slat track that is guided at the main wing for movement along a predefined path, and that is pivotally mounted to the slat via a third joint, and a first drive station including a first input section coupled to a drive shaft, a first gear unit, and a first output section drivingly coupled to the first slat track, a first linkage pivotally mounted to the main wing via a first joint and pivotally mounted to the slat via a second joint, a first slat track that is guided at the main wing for movement along a predefined path, and that is pivotally mounted to the slat via a third joint, and a first drive station including a first input section coupled to a drive shaft, a first gear unit, and a first output section drivingly coupled to the first slat track, wherein the second connection station comprises: a second linkage pivotally mounted to the main wing via a fourth joint and pivotally mounted to the slat via a fifth joint, a second slat track that is guided at the main wing for movement along a predefined path, and that is pivotally mounted to the slat via a sixth joint, and a second drive station including a second input section coupled to the drive shaft, a second gear unit, and a second output section drivingly coupled to the second slat track, a second linkage pivotally mounted to the main wing via a fourth joint and pivotally mounted to the slat via a fifth joint, a second slat track that is guided at the main wing for movement along a predefined path, and that is pivotally mounted to the slat via a sixth joint, and a second drive station including a second input section coupled to the drive shaft, a second gear unit, and a second output section drivingly coupled to the second slat track, characterized in that the connection assembly comprises a sync shaft coupling the first connection station to the second connection station for sync movement of the first and second connection stations (13, 15).