As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND IN COE MAJOR REPAIR. DENTS AND GOUGES ON RT WING LWR SKIN IN AREA OF SINGLE POINT FUELING DOOR. BLEND OUT OF CORROSION BEYOND SRM (STRUCTURAL REPAIR MANUAL) ALLOWABLE LIMIT. MULTIPLE DENTS BETWEEN RIBS 19 - 21 STRINGERS 2 - 5 FROM FUEL CAP. SRAS DO/TS-189/09. 5016 ISSUED FOR REPAIR OF THIS DISCREPANCY. DAMAGE TO BE 'LEFT AS IS'. A PERIODIC VISUAL INSPECTION TO BE PERFORMED AT 12,000 FC INTERVALS FROM DATE OF DAMAGE DISCOVERY.