As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE WAS FOUND TO THE FUSELAGE SKIN RIGHT BS 2655. INTERIM REPAIR WAS PERFORMED AS PER SRM 53-00-00 AND REPEAT INSPECTION EVERY 6,000 FLIGHT CYCLES PER ENGINEERING ORDER 4453A316. THIS REPAIR IS CLASSIFIED AS "MAJOR" AS DEFINED IN FAR 43 APPENDIX A.