As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON EXTERNAL FUSELAGE SKIN BS 360+7" STR 17L. REPAIRED EXTERNAL FUSELAGE SKIN LOCATED BETWEEN STR 16L TO STR 18L AND BETWEEN BS 360 TO BS 380 IAW EO AEM-HC53-010/13 R0 AND EA 1-353-21521 REV 0 FOR INSPECTION REQUIREMENT SEE TLD T031018