As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EVIDENCE OF CORROSION EXIST ON CIRCUMFERENTIAL JOINT INTERFACE @FS280.00-FS282.00 BETWEEN STRINGER 26R AND 26L (C-CHECK RO 11/5/2021) COMPLIED WITH ALL STEPS REO 670-53-21-2128 REV-- DATED 2021-09-09. COMPLIED WITH 51-900-1002-SKY AND DWG SH670-32420 REV. E. LEAK CHECK GOOD.