What was found
FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACKED AT LBL 45.5 AT BS 580. REMOVED DAMAGE, FABRICATED & APPLIED REPAIR IAW STANDARD REWORK DWG SR57-53-004 REV - & EA T F-5310-T0354571P1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACKED AT LBL 45.5 AT BS 580. REMOVED DAMAGE, FABRICATED & APPLIED REPAIR IAW STANDARD REWORK DWG SR57-53-004 REV - & EA T F-5310-T0354571P1.