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. @ FR. 80 between STR. 4R to 11RCorrective action/Removed corr. IAW A300 SRM 51-40-11. UT thickness checked per NTM 51-20-00, minimum remaining1.75 mm before 1.85 mm within limits per SRM A300 53-10-00. Treated an protected area IAW A300 SRM 51-40-12.