As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME AT FS 265 BETWEEN STR 26-27 R IS CORRODED. BLENDED CORROSION IAW SRM 51-42-06-001-001 & SRM 51-21-06-001-001. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURES UT-3. MINIMUM MATERIAL REMAINING .049" ORIGINAL .050" MATERIAL REMOVED .001". REPAIRED IAW REO 670-53-11-688, STEP 1.