As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C2 - INTERNAL FUSELAGE AT STA X116.000 FRAME TIES AT STRINGERS 30R TO 30L HAVE CORROSION. REMOVED RIVETS FROM AFFECTED AREA IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 53-00-00-02-09. REMAINING THICKNESS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. APPLIED TOPCOAT AND CORROSION INHIBITING COMPOUND IAW SRM 53-00-00-02-09.