As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
*FUSELAGE INTERNAL STRUCTURE €“ STRINGER STGR26, HAS CORROSION BETWEEN FS319 AND FS333. REMOVED CORROSION FROM STR26R BETWEEN FS319 - FS333 "OUT OF LIMITS" REF SRM (ORIGINAL: .063) - (REMAINING: .035) - (LOSS: .028). REMOVED AND REPLACED THE STRINGER IAW DRAWING, AND SRM.