Method for manufacturing a panel for an aircraft structure, said panel being provided with a doubler (310, 311), wherein the method comprises: - supplying the doubler in the form of a laminate of layers of metal and at least one fibre-reinforced adhesive layer in each case between two layers of metal, and by means of said at least one fibre-reinforced adhesive layer the at least two layers of metal are fastened together, - supplying a jig, - supplying, in the jig, a stack of layers of metal and layers of fibres embedded in a precursor of an adhesive included in each case between two layers of metal to form a skin, - placing a further layer of fibres embedded in a precursor of an adhesive on the stack, - placing the doubler on the further layer of fibres embedded in a precursor of an adhesive, so that the further layer of fibres embedded in a precursor of an adhesive forms an intermediate layer between the stack and the doubler, - placing an air-tight covering layer over the stack, the intermediate layer and the doubler, thereby forming a space between the jig and the covering layer, - air-tight closure of the covering layer around the perimeter of the stack, the intermediate layer and the doubler with respect to the jig, - putting the jig with the stack, the intermediate layer and the doubler as well as the sealed covering layer in an autoclave, - lowering the pressure in the space between the jig and the covering layer, - under the effect of heat and pressure in the autoclave, gluing the layers of metal together by activating the precursor of the adhesive of each embedded layer of fibres with formation of a laminated skin, as well as simultaneously, under the effect of the heat and pressure in the autoclave, activating the precursor of the adhesive of the further layer of fibres in the intermediate layer with formation of a supplementary adhesive layer, by means of which the doubler is bonded to the laminated skin, thereby forming the panel, - removing the panel from the autoclave, the method further comprising the steps of: - causing the perimeter of the further layer of fibres to recede relative to the perimeter of the doubler, - filling the space delimited by the doubler, the stack and the perimeter of the further layer of fibres with glue, forming a glued edge, - activating the glued edge under the effect of heat in the autoclave. - supplying the doubler in the form of a laminate of layers of metal and at least one fibre-reinforced adhesive layer in each case between two layers of metal, and by means of said at least one fibre-reinforced adhesive layer the at least two layers of metal are fastened together, - supplying a jig, - supplying, in the jig, a stack of layers of metal and layers of fibres embedded in a precursor of an adhesive included in each case between two layers of metal to form a skin, - placing a further layer of fibres embedded in a precursor of an adhesive on the stack, - placing the doubler on the further layer of fibres embedded in a precursor of an adhesive, so that the further layer of fibres embedded in a precursor of an adhesive forms an intermediate layer between the stack and the doubler, - placing an air-tight covering layer over the stack, the intermediate layer and the doubler, thereby forming a space between the jig and the covering layer, - air-tight closure of the covering layer around the perimeter of the stack, the intermediate layer and the doubler with respect to the jig, - putting the jig with the stack, the intermediate layer and the doubler as well as the sealed covering layer in an autoclave, - lowering the pressure in the space between the jig and the covering layer, - under the effect of heat and pressure in the autoclave, gluing the layers of metal together by activating the precursor of the adhesive of each embedded layer of fibres with formation of a laminated skin, as well as simultaneously, under the effect of the heat and pressure in the autoclave, activating the precursor of the adhesive of the further layer of fibres in the intermediate layer with formation of a supplementary adhesive layer, by means of which the doubler is bonded to the laminated skin, thereby forming the panel, - removing the panel from the autoclave, - causing the perimeter of the further layer of fibres to recede relative to the perimeter of the doubler, - filling the space delimited by the doubler, the stack and the perimeter of the further layer of fibres with glue, forming a glued edge, - activating the glued edge under the effect of heat in the autoclave.