As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CONFORMITY CHECKS A CRACK WAS FOUND AT STRINGER CUTOUT AT FS 177 AND 9R. CRACK RADIATES .2 INCH. REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW B1900D SRM 51-70 AT FS 177. REPAIR AREA APPROX 4.6 INCHES BY 2.6 INCHES. 2024 T3, .071 INCHES, MS20470 RIVETS. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1.