As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-check/EADS responsibility during DFDR system test,rudder damaged at lower t/e wedge 19" longx 4.5" wide %' up from lower edge of rudder.Corrective action/area repaired IAW A300 SRM 55-40-00 page 740 see page 2 an 3 fpr detrail instruction am NDT requirements c/w. Prepped an painted IAW A300 SRM 51-40-12