As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE/OVERWING LONGITUDINAL FLOORBEAMS, CRACK REPAIR DURING ACCOMPLISHMENT OF INSPECTIONS OF THE LT/RT BL 24.8 OVERWING LONGITUDINAL FLOORBEAMS PER SI 3-056673-12AD, FATIGUE CRACKS WERE DETECTED IN THE WEB DOUBLERS AND BS 678 VERTICAL STIFFENER. CRACKED DOUBLERS AND STIFFENERS REPLACED AND INSTALLS 3-056673-3AD MODIFICATION PER ER/A 450791-14AD.