As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF CEILING PANEL 131EC FOR AGING ACFT INSPECTION, FOUND MDCC FLOOR SUPPORT C36 BETWEEN L4 AND L5 SEAT TRACK TO BE CRACKED TOP OF VERTICAL STIFFENER LENGTH OF CRACK .400 INCH ROUTED OUT CRACK IAW A310/200 SRM 53-10-15. FABRICATED 2 REPAIR ANGLES AND INSTALLED IAW A310-200 SRM 53-10-15. REPROTECTED AREA IAW A310-200 SRM 51-75-10.