As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT FR 36 STR 14 CORROSION. RT FRAME 36 STRINGER 14 CORROSION REMOVED AS PER SRM 51-21-42. MATERIAL THICKNESS 0.080 MATERIAL REMOVED .005 WITHIN LIMITS AS PER SRM 53-61-00 FIG 301. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 51-21-42 (CLOSED)