As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION FOUND IN THE FUSELAGE SKIN ALONG THE CHEM-MILL STEP LOCATED ABOVE STR 13R AND BS 500D+12" CRACK LENGTH 1.3" APPROX. REPAIRED FUSELAGE SKIN ALONG THE CHEM-MILL STEP LOCATED ABOVE STR 13R AND BS 500D+12" CRACK LENGTH 1.3" APPROX IAW EO AEM-HC53-026/13 R0 AND EA 1-353- 21786, FOR INSPECTION SEE TLD T037051.