As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PREVIOUS REPAIR LOCATED ON R/SIDE FUSELAGE SKIN BETWEEN FR 66 TO 67 BETWEEN STR 35TO 38 RT HAS AN EXTERNAL REPAIR DOUBLER MEASURING 8.8 BY 11.9. REPAIR REVIEWED AND FOUND NOT TO BE IAW A310-200 SRM 53-10-12 FIG 226 SHEET 2. REWORKED REPAIR IAW A310-200 SRM 53-10-12, FIG 226 SHEET 2 REF N00503.