As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING UPPER T/E FIX PANEL BETWEEN #5 AND #6 SPOILERS; SUPPORT BEAM ATTACHMENT ANGLE TO DEFLECTION CONTROL RIB CRACK.<[01] REMOVED; REPLACED; AND INSTALLED A NEW SUPPORT BEAM ATTACHMENT ANGLE TO DEFECTION CONTROL RIB AT LT WING UPPER T/E PANEL BETWEEN #5 AND #6 SPOILERS IAW SRM 51-40-02 AND IPC 57-42-51-03.;[02] JOB COMPLETE.