As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME CRACKED APPROXIMATELY .8 INCH IN LENGTH AT FS 177 AT STRINGER 9AR. CRACKED AT STRINGER CUTOUT ON FRAME. REPAIRED FUSELAGE FRAME CRACK AT STRINGER RELIEF HOL AT F.S. 177 STRINGER 9AR. REPAIR APPROXIMATELY 4.4 INCH BY 2.5 INCH .080 2024 T-3.