As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION WAS FOUND IN THE FUSELAGE SKIN LOCATED AT THE BS 827+3.5" ABOVE STR 16L CRACK LENGHT=1.00". REPAIRED FUSELAGE EXTERNAL SKIN LOCATED BETWEEN BS 818 TO BS 850 STR 14L TO STR 17L IAW EA 1-353-21451 REV 0 AND EO NO AEM-HC53-592