As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CABIN FLOOR PNL 37 FWD END TOP SKIN IS CRACKED, DENTED, AND CORRODED. RII: Y. REMOVED EXISTING REPAIR WITH CRACK AT CENTER PORTION OF PANEL 37. FURTHER EVALUATION FOUND CRACK IN PNL. STOP DRILL CRACK IN PANEL. FABRICATED AND INSTALLED REPAIR IAW SRM 51-30-2 PG 2. REMOVED CORROSION IAW WITHIN LIMITS IAW SRM 53-01 PG 8. TREATED AND PRIMED.