As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .5". MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 164.4 REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3. RLL INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K)