As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EVIDENCE OF CORROSION ON FRAME FLANGES, AND ON FWD AND AFT SIDE OF FRAME AT FRM 32.4, BETWEEN STRINGERS 29 - 33R. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00, REPAIR -21. REMOVED AND REPLACED THE FRAME IAW DWG:85329251, REV.C AND SRMS.