As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT ELEVATOR PANEL NR 335 CT IS CORRODED. REMOVED CORROSION IAW A310 SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.080 IAW AIRBUS DWG 38; A55276950. REMOVED 0.001; REMAINING MATERIAL 0.079. FOUND TO BE WITHIN LIMITS IAW A310 SRM 55-22-00; TABLE 101. UT GAUGE NR T8225Q; CAL DATE 21/20/07. ALODINED IAW A310 SRM 51-21-10. PRIMED AND TOP COATED IAW A310 SRM 51-23-10.