As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HFEC INSPECTION FOUND ONE CRACK APPROX. 0.60 INCH IN LENGTH ON THE FUSELAGE SKIN BELOW THE 7TH STRINGER-ATTACH RIVET ALONG S13R, AFT OF FRAME BS 1654.5 IAW W/C 5330- 01229-01B STEP 4. THE CRACKED AREA OF SKIN TRIMMED OUT AND REPAIRED IAW SRM 53- 80-01-2R-7, REPAIR 7.