As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT SCHEDULED INSPECTION DISCOVERED LT FUSELAGE SKIN DAMAGE DUE TO CORROSION. LOCATED AT F.S.363.250 STRINGER 13L CUT OUT SECTION OF CORRODED SKIN 2.0 IN X 5.0 IN FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER IAW STRUCTURAL REPAIR MANUAL 51-70-06.