As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE/OVERWING FLOORBEAM,BL 0 FS 660-664, REPAIR FOR CRACKS. THE OVERWING LONGITUDINAL FLOORBEAM UPPER CAP AT BL 0 WAS SEVERED AT FS 660 AND HAD AN ADDITIONAL CRACK FS 664. THE BEAM WEB WAS NOT DAMAGED. THE FLOORBEAM CAP WAS REPAIRED PER THE PROCEDURES OUTLINED IN BAC S/B 737-57-1210 AND DOCUMENTED PER ER/A 366299-14.