I'm guessing that due to the arena in which this incident occurred, no one really knows what the extent of repair would be before returning the aircraft to service. I'm guessing that the flap actuator jack screw was undamaged, and only the fairing requires repair, but the wing flap would require some sheet metal work. Would inspections be made of structures actuators etc. to check for damage due to the unusual loads? I'm just asking for opinions here. Of course there is always "500 mph" duct tape.