As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LWR AFT FUSELAGE SKIN APPROX 3 INCH BY 1.5 INCH AREA OF CORROSION 12 INCH AFT OF FR 69, 3 INCH ABOVE STR 34R LAV VENT EXHAUST. REMOVED CORROSION IAW SRM 53-41-11 OUT OF LIMITS IAW SRM 53-41-11. CUT OUT DAMAGE AREA IAW SRM 53-41-11. FABRICATED DOUBLER AND FILLER IAW SRM 53-41-11. LOCATED AND DRILLED REPAIR PARTS IAW SRM 53-44-11. INSTALLED DOUBLER PER SRM 53-41-11.