As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CABIN BS 500 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE, REMOVED MAXIMUM OF .036" FROM ORIGINAL FRAME THICKNESS OF .056" WITH .020" REMAINING. OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED.