As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
2 GOUGES IN UPPER EXTERIOR FUSELAGE SKIN AT FR61 BETWEEN RT STRINGERS 3-4. CUT OUT DAMAGED AREA OF SKIN IAW A310-200 SRM 53-27-00. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED DOUBLER REPAIR IAW A310-200 SRM 53-10-12 FIG. 228.