As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, FUS EXTERIOR BULGE IN FUS SKIN AT FS 350, BETWEEN STR 26R AND STR 27R, O/B OF ACCESS PANEL. CUT OUT DAMAGED SECTION OF SKIN PER SRM 51-10-6. REMOVED CORROSION FROM LOWER SURFACE OF CHORD ANGLE PER SRM 51-10-6. INSTALLED SKIN REPAIR 16 INCHES BY 11 INCHES .080 2024-T3 AND CHORD ANGLE REPAIR 16 INCHES BY 8 INCHES .100 7075-T6 PER SRM 53-30-3 AND 51-40-4. TOTAL CYCLES 29577.