As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN FLOOR PANEL NR 85 HAS CRACK INBD AFT END. CUTOUT DAMAGE 2 INCHES BY 1.25 INCHES NO DEFECTS PER NDT SPM 06-10-01. FABRICATED AND INSTALLED FILLER AND DOUBLER FROM .020 7075-T6 PO NR 1120495 IAW DC-9 SRM 53-01 FIG 4, P225. REQUIRED INSPECTION COMPLETED PEMCO Q919.