As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ONE INCH SUB-SURFACE CHEM-MILL CRACK FOUND DURING NDT INSPECTION, ABOVE STR-26L AT BS 383 TO BS 384. REPAIRED CHEM-MILL CRACK OF FUSELAGE SKIN AT BS 383 TO 384 STR 26L IAW ER 13-01261 & EA 1-353-21605 FACT AS A RESULT OF POST REPAIR INSPECTION.