As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXT FUSELAGE SKIN CORRODED FR 30, LEFT STR 21. CORROSION ON SKIN REMOVED IAW SRM 51-21-42 WITHIN TOLERENCE IAW 53-61-00 FIG 301 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42. MATERIAL THICKNESS: MATERIAL REMOVED: 0.001WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301.