As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHAFING ON THE LT X-FRAMES AFT UPPER AND LOWER LEGS. THE AFT UPPER LEG DAMAGE IS .24” BY .22” AND IS .024” AT ITS DEEPEST POINT LOCATED AT STA 3650, WL 1979, AND BL 430L. THE AFT LOWER LEG DAMAGE IS .74” BY .19” AND MEASURES .002” LOCATED AT STA 3650, WL 2305, AND BL 430L.