As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - FUSELAGE FRAME CRACKED APPROX .400 INCH IN LENGTH AT THE STRINGER 10R CUTOUT AT FS 164. MX REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT F.S. 164 AND STRINGER 10R. REPAIR APPROX 5.5 INCHES BY 2.5 INCHES OUT OF 2024 T3 ALUMINAUM, .071 INCH, MS20470AD RIVETS. RII INSP COMPLIED IAW TASKCARD 8.2.1.