As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON THE MAIN CABIN FLOOR STRUCTURE REPAIR DOUBLER BS 720 BETWEEN RBL 15.5 AND RBL 45.5 UPPER SURFACE EVALUATED CORROSION ON MAIN CABIN FLOOR STRUCTURE REPAIR DOUBLER BS 720 AT RBL 15.5 TO RBL 45.5. ORIGINAL MAT THICKNESS IS .071 MATERIAL REMOVED .059 AND IS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED .3 STRAP IAW DWG NR 95-030 AND SRM 51-40-02 PAR 7.