As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 265 FRAME WAS CORRODED BEWEEN STR 27 - 26L. FOUND CORROSION TO BE CENTRALIZED TO THE BS 265 LOWER STIFFENING ANGLE BTWN STR 26-27L. REMOVED AND INSTALLED A NEW SERVICEABLE TIFFENING ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & 51-42-22-001-001-A01.