As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CORROSION ON STRINGER 26R IN STA. FS= 280 TO FS= 295 ALSO 25RH BTW FS=280 TO FS=310 AT MAIN AVIONICS COMPARTMENT. (E/E) (TCI:53-20-304). STRINGER 26R IN STA. FS= 280 TO FS= 333 AND 25R BTW FS=280 TO FS=333 WAS REPLACED PER SRM 51-42-06-001-001-A01. P/NS SH670-31634-2 AND SH670-31212-2.