The invention provides an anti-bird-impact wing fixed front edge, which comprises composite material skins (1), a metal anti-collision skin (2), butt joint separation plates (3) and common separationplates (4), wherein the metal anti-collision skin (2) and the two composite material skins (1) are adhered to form a front edge skin with a U-shaped cross section, the composite material skin (1) hasa honeycomb sandwich structure, the metal anti-collision skin (2) is positioned at the bending position of the U-shaped front edge skin, and is specifically adhered at the part within the 5% chord length of the shape surface of the front edge, both ends of the U-shaped front edge skin are respectively provided with the butt joint separation plate (3) forming butt joint with the remaining anti-bird-impact wing fixed front edge, the two common separation plates (4) are attached to the concave surface sides of the U-shaped front edge skin, and the two butt joint separation plates (3) and the twocommon separation plates (4) are arranged at equal intervals. According to the present invention, the front edge is combined by adhering the composite material and the metal material so as to complement the advantages and the disadvantages and reduce the structural weight.