As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURAL INSPECTION AT THE ENGINE NR 2 PYLON AREA, WAS FOUND THE NR 2 PYLON AFT ENGINE MOUNT FITTING WITH CORROSION. THE DAMAGED AREA WAS REPAIRED PER AIRBUS INSTRUCTIONS UNDER REF 80356610 AND EOD 32S-54-0180-R00 AND APPROVED UNDER RDAS 80356610/003/2017.