A flame-holder device for the afterburning of a bypass turbojet, said turbojet comprising first and second internal annular casings, defining a passageway for a main flow, and an external annular casing defining with said first internal annular casing a passageway for a bypass flow, comprising:
at least one metal arm support designed to be attached to said external casing by means of a top plate,
at least one flame-holder arm, having a trough shape making a cavity, designed to be attached to the arm support, and
at least one screen for the heat protection of the arm cavity, the arm support and the heat-protection screen being in one piece.