As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME AT FS 451 CRACKED ON THE TOP SIDEOF STRINGER 10R. CRACK APPROXIMATELY 1.1 INCH LENGTH. MAINT REPAIRED FUSELAGE FRAME FLANGE AT FS 451 STRINGER 10R IAW SRM 51-70. REPAIR APPROXIMATELY 6 INCH BY 2 INCH. 2024-T3 .071. RII INSPECTIONS COMPLIED WITH IAW TASKCARD 8.2.1.