As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK CRACK AROUND RIVETS FRAME 75 STRINGER 1R (EXTERNAL FUSELAGE). MX REPAIRED 2 REAMED RIVET HOLES IAW EC5330-01938 AND INSTALLED RIVETS AT FRAME 75 STRINGER 1R IAW SRM 51-40-02 AND PREPPED, PRIMED AND RESTORED ORIGINAL FINISH IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.