As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT AFT FUSELAGE PASSENGER/CREW ENTRANCE LOWER CENTER CORNER UNDER SCUFF PLATE FWD FITTING CORRODED. REMOVED EXFOLIATED CORROSION CENTER SHAPE SILL. LOCATED AND DRILLED NEW SHAPE SILL. TREATED AND PRIMED FASTENERS HOLE ON NEW SHAPE SILL. INSTALLED NEW SHAPE SILL. PAINTED FASTENERS.