As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME HAS CORROSION AT FS 310 AND BETWEEN STR 27 AND 26L. REMOVED COATINGS AND CORROSION IAW SRM 51-21-00-001-A01. BLENDED CORRODED AREAS IAW SRM 51-21-00-001-A01. PERFORMED UT THICKNESS MEASUREMENT ON BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3 MINIMUN MATERIAL REMAINING IS .048". APPLIED A023 FINISH TO AREA BETWEEN STR 26L & 26R AT FS 310 ON FRAME FLANGE REF SRM 51-21-16-001-001-A01.