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 905 TO 927 AND STRINGERS 22 AND 24 LEFT. REMOVED ALL CORROSION PER SRM 51-10-02. PERFORMED DIGITAL THICKNESS MEASUREMENT, AREA WITHIN LIMITS PER EA. INSTALLED FASTENERS FROM STATIONS 905 TO 927 AND STRINGERS 22 TO 24 LEFT PER SRM 51-40-02.