As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PREVIOUS REPAIR LOCATED ON RIGHT THS UPPER REAR SPAR CHORD BETWEEN RIBS 4 AND 5 HAS 1 EACH REPAIR ANGLE ON LOWER SURFACE OF FLANGE MEASURING 15.2 INCH LONG BY 1.65 INCH TALL REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR ANGLE IAW A310 SRM 55-11-21 FIG 211, 213 AND 218. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING, AIRCRAFT INSPECTION.