As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** FUSELAGE SKIN (148A3321) HAS CORROSION AT BS1016 BUTT JOINT; S-24L TO S-24R / REMOVED CORROSION; INSPECTED AND RESTORED AREA OF FUSELAGE SKIN AT BS 1016 BUTT JOINT S-24L-24R (148A3321) IAW EA 1-753-32725 REV IR AND ER 18-02660 REV IR