As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INTERNAL FUSELAGE SKIN CORROSION AT FR 11-12 BETWEEN STGR 20R-21R ON PREVIOUS BLEND.-C/A-ACCOMPLISHED PERMANENT REPAIR ON INTERNAL FUSELAGE SKIN CORROSION BETWEEN FR 11-12 AND STGR 20R-21R IAW ERS-EM-53MR-4083. REPAIR MATERIALS: DOUBLER: AL CLAD 2024-T3, 0.050? THICK. FILLER: AL CLAD 2024-T3, 0.032? THICK. REPAIR FASTENERS: MS14218-AD5. ORIGINAL FASTENERS: SAME TYPE AS ORIGINAL.