As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PITTING/CORROSION ON FUSELAGE SKIN FROM STATIONS 1016 TO 1040 AND STRINGERS 21 AND 22 LEFT. REMOVED ALL CORROSION PER SRM 51-10-02. PERFORMED DIGITAL THICKNESS MEASUREMENT, AREA WITHIN LIMITS PER EA B737-53-026523. INSTALLED FASTENERS FROM STATIONS 1016 TO 1040 AND STRINGERS 21 TO 22 LEFT PER SRM 51-40-02.