The invention relates to an aircraft wing suitable for shuttling back and forth aerosphere, and the aircraft wing includes a skeleton structure and skin, wherein the skeleton structure is formed by intersection of longitudinal beams and transverse ribs, the longitudinal beams comprise a front beam, a main beam and a back beam, the transverse ribs comprise a root rib, a second rib and an end rib; the end of the front beam, near the root rib, is connected with body by a first shear pin; the end of the back beam, near the root rib, is connected with the body by a second shear pin; one end of the main beam stands out of a wing contour envelope and extends into the interior of the body; an end face of one end of the main beam and a body symmetrical plane are flush, the end face of one end of the main beam is adhered to, fixed and connected to an end face of one end of a main beam of a wing at the other side, wherein the end of the main beam of the wing at the other side extends into the interior of the body; the main beam is connected, at the position of the root rib, with a ventral shield of a body internal frame by a third shear pin; a cavity of the skeleton structure is filled with honeycomb, and the skeleton structure and the skin are in co curing connection, the wing structural layout is simple, fastener use amount is less, the weight is light, and the whole wing assembly molding can be realized by overall co curing way.