As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FUSELAGE SKIN BS 886-888 BETWEEN STRS 2L-2R WL 308 RBL10-LBL10. REMOVED DAMAGE AT BS 886-888 BETWEEN STRS 2L-2R WL 308.5 RBL 10-LBL 10. DAMAGE FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-01-1A-1. REPAIRED AREA PER ATS ER 20-03531 REV IR AND SWA EA 20-153-02278 REV IR.