As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-check/R/H aft upper fuselage ext. skin has areas of corr. @ fr80 between STR. 12R to 17R.Corrective action/removed corrosion IAW A300 SRM 51-40-11. UT thickness checked per NTM 51-20-00 before 2.04 mm minimum after 1.97 mm. Treated an protected area IAW A300 SRM 51-40-12.