As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME AT FS 177.3 CRACKED AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .6 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME AT FS 177.3 AT STRINGER 9R RELIEF HOL IAW. SRM 51-70. REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3 .071. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1.