As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 25R HAS SIGNS OF CORROSION BETWEEN FS 280 AND FS 295. BLENDED AREA STR 25R BETWEEN FS 280 AND FS 295 MATERIAL LOSS WAS .005" OF ORIGINAL MATERIAL 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.