As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON INNER FUSELAGE SKIN PREVIOUS REPAIR DOUBLER BETWEEN STA Y=610 TO Y=628 LONG, 28RY AND 29 LT REF (T0 277241). REPAIR FILLER WAS REMOVED IAW SRM MD-88 51-30-5. FABRICATED AND INSTALLED, AND PROTECTED AGAINST CORROSION IAW SRM 51-10-3 PAR 14-21 AND 41. CORROSION LEVEL 2. ASSOCIATED ER/A 45-768714 ADDED FOR AC 0946.