As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND WEAR MARK ON INNER FLANGE OF FRAME 38.1 BETWEEN STRG 14-15 RT. REPAIR PERFORMED BY INSTALLING INTERNAL ANGLE AND ADDITIONAL SHIM AS PER PRINCIPLES GIVEN IN SRM 53-10-13/FIG 202, APPROVED EA 6-5314-95855 AND RAS/DABRE/7005992/2005.