As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION WAS FOUND IN THE FUSELAGE SKIN APPROXIMATELY 2 INCHES AFT OF STA 950F, AT S-28R. DAMAGE REMOVAL RESULTED IN A 4.125 INCH INBD/OUTBD BY 6.0 INCH FWD/AFT CUT-OUT. THE SKIN IS FABRICATED FROM CLAD 2024-T3 AND WAS MEASURED AT 0.150 INCH THICK. REPAIRED PER DL ERA 302750-14.