As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 BETWEEN 11 LBL/RBL AT COCKPIT. (CPIL) TCI 53-10-219. SUMMARY: CRACK IN FLOORBEAM [ UPPER/AFT FLANGE ] IN STA. FS= 280 AND 27LBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) WAS REPLACED PER SRM 51-42-13-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.