As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING T/E SHELF PANEL AT FLAP DEFLECTION RIB HAS SUPPORT ANGLE CRACKED ON OUTBOARD END. (MARKED) / [01] REMOVED RIGHT T/E SHELF PANEL SUPPORT ANGLE IN IAW SRM 51-40-02.;[02] INSTALLED RIGHT T/E SHELF PANEL IAW SRM 51-40-02.;[03] CW