As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN AT STA 950D PLUS 10 BETWEEN STR 28R AND 27R. A 1.625 INCH BY 3.125 INCH CUT OUT IN THE 0.150 INCH BONDED 2024-T3 CLAD SKIN WAS REQUIRED. AN EXTERNAL REPAIR DOUBLER AND TRIPLER WILL BE INSTALLED PER DL ERA 301441-14.