As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE AIRCRAFT STRUCTURAL INSPECTION, WAS FOUND AT SECTION 43 FUSELAGE SKIN BETWEEN BS 360 AND BS 420 AND BETWEEN STRINGER 27R-27L SKIN WITH NICKS. IT WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST 4-4703561547 AND EO NUMBER COO-EO-2020-10845.