As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBD. TRAILING EDGE UPPER PANEL SUPPORT ANGLE CRACKED JUST INBD. OF THE DEFLECTION CONTROL RIB.<[01] LOCATED AND DRILLED FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] VERIFIED WORK SIGNED IN CA#1.......LOCATED AND DRILLED FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05;[03] ALL STEPS COMPLETE