As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FORWARD CARGO CEILING LBL 45 STA 580 MAIN CABIN FLOORBEAM "T" CAP ON THE RADIUS. DOT 88-001 REMOVED DAMAGED SECTION OF THE LT BS580 LBL45 "T" CORD. FABRICATED ANGLE AND RADIUS STRAP INSTALLED REPAIR PARTS IAW EA 5310-T0344538 P1. COMPLIED WITH FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR AT LBL 45.