As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION ON FRAME C 39 BETWEEN CENTER LINE STRINGER 55 AND 52 RT AND ON AFT SIDE PANEL BETWEEN P 49-48 RT. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE AND CORROSION FREE CONDITION AND REPAIR OF BULKHEAD FRAME C 39 AND T-SECTION BETWEEN P 52 LT-42 RT IAW DRAWING R538-10717 ISS A, APPROVED BY RAS/70518531/048/2009 ISS A AND EA 6-5310-129112 .