As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
COCKPIT FLOOR PANEL 211AF AFT ATTACH FLANGE HAS A CRACK BS 270 LBL 8.5. TRIMMED OUT DAMAGE AREA AT LATERAL INTERCOSTAL BS 270 LBL 8.5. FABRICATED-1 REPAIR ANGLE MAT USED BAC 1490-2738 7075 T6. FABRICATED-2 TAPERED FILLERS MAT USED 7075 T6 .063' AND INSTALLED REPAIR PARTS, PER REF RES NR 2016182-2 AND EA NO: 20-153-01600 REV IR.