As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE AFT WING TO BODY FAIRING UPPER FRAME NUTPLATE STRIP HAS INTERGRANULAR CORROSION BETWEEN STA 1220 AND STA 1240, LBL 63.0, AFT OF NUMBER 1 ELECTRIC MOTOR PUMP OF CENTER HYDRAULIC SYSTEM. EVALUATE AND RECTIFY. CORRODED LOWER CHORD REMOVED AND REPLACED IN ACCORDANCE WITH B757 SRM 51-10-02 PARAGRAPH 8, REV 95. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.