A wing with a main wing, a high-lift flap, which is movably arranged on the main wing by means of at least two adjustment mechanisms (1, 2) which are arranged next to each other in the span-wise direction of the wing and are adjustable by means of a drive device, each of the adjustment mechanisms comprising: - a first adjustment lever (11, 21), which is articulated on the main wing via a first rotary joint (13, 23) to form a first axis of rotation (A11, A21), - a second adjustment lever (12, 22), which is articulated on the high-lift flap via a second rotary joint to form a second axis of rotation (A21, A22), - a third joint (15, 25) which connects the first (11, 21) and the second (12, 22) adjustment lever to each other in an articulated manner to form a third axis of rotation (A31, A32), wherein the first, second and third axis of rotation (A11, A12, A13; A21, A22, A23) extent through a common pole which is fixed with respect to the position of the main wing when adjusting the high-lift flap, characterised in that on at last one of the adjustment mechanisms (1, 2) an intermediate articulated part, which comprises a base body with at least one first axle shaft mounting and with a second axle shaft mounting spaced apart in the transverse direction of the base body, is arranged and designed such that two axle shaft elements extending along the longitudinal direction (Z-L1) of the base body are received rotatably and spaced apart from one another in the transverse direction (Z-L2) of the base body, wherein the intermediate articulated part - with the first axle shaft mounting rotatably supports a first axle shaft element to form the first axis of rotation (A11, A21) and with the second axle shaft mounting rotatably supports a fourth axle shaft element to form a fourth axis of rotation (A4-1) for purposes of coupling the first adjustment lever (11, 21) and the main wing to the intermediate articulated part, with an axes distance D between the first axis of rotation (A11, A21) and the fourth axis of rotation (A4-2), or - with the first shaft mounting rotatably supports a second axle shaft element to form the second axis of rotation (A12, A22) and with the second shaft mounting rotatably supports a fourth axle shaft element to form a fourth axis of rotation (A4-2) for purposes of coupling the second adjustment lever (12, 22) and the high-lift flap to the intermediate articulated part, with an axes distance D between the second axis of rotation (A12, A22) and the fourth axis of rotation (A4-2), wherein the base body - is integrally formed in one piece, or - is formed in two pieces from two intermediate levers (121, 122) each extending in the transverse direction (Z-L2) of the base body, wherein the first intermediate lever is coupled via two spherical rotary joints (123, 124) and the second intermediate lever is coupled via a spherical bearing and is coupled via a non-spherical bearing or in rotationally fixed manner. - a first adjustment lever (11, 21), which is articulated on the main wing via a first rotary joint (13, 23) to form a first axis of rotation (A11, A21), - a second adjustment lever (12, 22), which is articulated on the high-lift flap via a second rotary joint to form a second axis of rotation (A21, A22), - a third joint (15, 25) which connects the first (11, 21) and the second (12, 22) adjustment lever to each other in an articulated manner to form a third axis of rotation (A31, A32), wherein the first, second and third axis of rotation (A11, A12, A13; A21, A22, A23) extent through a common pole which is fixed with respect to the position of the main wing when adjusting the high-lift flap, characterised in that on at last one of the adjustment mechanisms (1, 2) an intermediate articulated part, which comprises a base body with at least one first axle shaft mounting and with a second axle shaft mounting spaced apart in the transverse direction of the base body, is arranged and designed such that two axle shaft elements extending along the longitudinal direction (Z-L1) of the base body are received rotatably and spaced apart from one another in the transverse direction (Z-L2) of the base body, wherein the intermediate articulated part - with the first axle shaft mounting rotatably supports a first axle shaft element to form the first axis of rotation (A11, A21) and with the second axle shaft mounting rotatably supports a fourth axle shaft element to form a fourth axis of rotation (A4-1) for purposes of coupling the first adjustment lever (11, 21) and the main wing to the intermediate articulated part, with an axes distance D between the first axis of rotation (A11, A21) and the fourth axis of rotation (A4-2), or - with the first shaft mounting rotatably supports a second axle shaft element to form the second axis of rotation (A12, A22) and with the second shaft mounting rotatably supports a fourth axle shaft element to form a fourth axis of rotation (A4-2) for purposes of coupling the second adjustment lever (12, 22) and the high-lift flap to the intermediate articulated part, with an axes distance D between the second axis of rotation (A12, A22) and the fourth axis of rotation (A4-2), wherein the base body - is integrally formed in one piece, or - is formed in two pieces from two intermediate levers (121, 122) each extending in the transverse direction (Z-L2) of the base body, wherein the first intermediate lever is coupled via two spherical rotary joints (123, 124) and the second intermediate lever is coupled via a spherical bearing and is coupled via a non-spherical bearing or in rotationally fixed manner.