As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FUSELAGE FRAME AT FS 639 HAD A PREVIOUS REPAIR ON THE AFT SIDE AT LONGERON 18L THAT HAD CRACKED THROUGH THE PREVIOUS STOP DRILL. REPAIRED LEFT FUSELAGE FRAME AT FS 639 IAW ABX REA D953-13924-MR.