As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CABIN BS 620 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE ON FRAME INNER CHORD, STA 620 STR 11R, FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .056" .008" BLEND, .048" REMAINING. FABRICATED NEW DOUBLER REF SRM 51-40-3 AND INSTALLED DOUBLER REF 51-30-2.