The Procaer Cobra was a two-seat turbojet powered light aircraft designed and built in Italy and flown in the early 1960s.
The Cobra was a cantilever low wing monoplane with a wooden structure covered in plywood, which had an outer thin aluminium skin bonded to it.
The single spar wings had a maximum thickness to chord ratio of 16.5%; in plan they were unswept and straight tapered.
The horizontal tail was unswept and straight tapered, with squared tips, the starboard elevator carrying an electrically operated trim tab.
The Cobra had a retractable tricycle undercarriage, the wing mounted main members swinging inwards close to the air inlet ducts.