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 LOCATED Y=1022 BETWEEN L-9L AND L-8L. SUMMARY OF NRC 00496: CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L WAS REPAIRED PER PRI 616777-14 REV 1 AND ERA 616777-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR.