As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TYS, DURING A SCHEDULED INSPECTION THE LOWER SKIN SUPPORT BRACKET BETWEEN STR 21L AND 21R ON FR21 HAS ELONGATED HOLES. MAINTENANCE PERFORMED REPAIR WITH TWO INTERNAL L ANGLE DOUBLERS ON FR 21 BETWEEN STR 21L AND 21R. ALODINED, PRIMED AND INSTALLED IAW EC5310-01328 AND EMB 135/145 CPM 51-21-04/05.