As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME CRACK AT FS 163.97 AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .5 INCH IN LENGTH. MAINT REPAIRED FUSELAGE FRAME AT FS 163.97 AT STRINGER 9R RELIEF HOLE IAW. SRM 51-70. REPAIR APPROXIMATELY 5.5 INCH BY 2.5 INCH. 2024-T3 .071. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.