As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING FLIGHT, FUSELAGE SKIN PANEL SECTION BROKEN OFF (APPROXIMATELY 10 INCH BY 20 INCH BETWEEN STA 2690.85 AND 2701.5 AT WL 310). VEERED AFTER LANDING DURING MAINTENANCE INSPECTION ACTIVITY. REPAIR IN PROGRESS, TO BE PERFORMED IN ACCORDANCE WITH BOEING STRUCTURAL REPAIR MANUAL.