As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 26R HAS SIGNS OF CORROSION BETWEEN FS 280 AND FS 295. BLENDED AREA OF STR 26R AT FS 280 TO FS 295 MATERIAL LOSS WAS .004" OF ORIGINAL THICKNESS OF .063" NO FURTHER CORROSION NOTED AT THIS TIME IAW SRM 51-42-06, 53-21-03, 51-21-11, AND 51-21-06.