As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1) IAW A320 AMM 71-22-11.