As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE LOWER SKIN INTERGRANULAR CORROSION NOTED AT STA. 1042 AND 2' BELOW STR 20L AT FWD UPPER CORNER OF 311AL ACCESS DOOR CUTOUT. ALL WORK FOR THIS REPAIR ACCOMPLISHED ON TTG8Q00712D9 REF EA 21-153-3210 INSPECTION VERIFIED. AUDIT CW