As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN FLOOR PANEL 55 HAS HOLE IN FWD END. REMOVED FLOOR PANEL IAW DC-9 SRM 51-30-1. ROUTED OUT HOLE NDT VERIFY NO DAMAGE REMAINS FAB REPAIR DOUBLER MATERIAL .025 7075T6 AND INSTALLED IAW DC-9 SRM 53-01 FIGURE 4. REINSTALL FLOOR PANEL IAW SRM DC9-A-53-20-201-925A-A. TOTAL REPAIR WEIGHT .07 OZ. INSTALLED ID TAG IAW PROCESS STANDARD 900-5-1 NO 4 P-245.