Abstract: A repair laminate for the quick repair of lightweight panels used particularly in aircraft construction comprised of a lightweight core 2, e.g., in the form of a possibly pressed honeycomb structure, and two outer laminates 3,4, which repair laminate is comprised of a solid cured or thermoplastic layer of synthetic material 13 bonded on one side to a hot-melt adhesive 15 and optionally on the other side to a decorative liner-layer. The synthetic material layer 13 may advantageously be a glass-fabric reinforced phenol aldehyde resin and the liner-laminate may be a dyed polyvinyl fluoride film.