As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAINTENANCE FOUND THE FUSELAGE SKIN DENTED AND CRACKED BETWEEN STA 500D + 10 AND 520, S12L. THE CRACK WAS 1.4 INCHES LONG. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03361. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 12 MONTHS.