As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TOOLING MARKS WERE FOUND AT FRAME 12A BETWEEN STRG 26-27 RT. REPAIR PERFORMED BY REMOVING FASTENERS, SMOOTH BLEND OUTS, FOR ELIMINATE THE DEEPEST MARK A 13MM SKIN HOLE DIA WAS PERFORMED, ROTO TEST AND HFEC INSPECTION WITH NIL FINDINGS AND ONE 13MM DIAMETER SHOULDERED BUSH WAS INSTALLED AS PER SRM 53-10-12/FIG 221 WITH A ASNA2019-40 FASTENER. REPAIR IAW EA 6-5312-101254 AND RAS 044514/014/2006 ISSUE A.