As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING T/E UPPER FIXED T/E PANEL JUST INBD OF DEFLECTION CONTROL RIB; PANEL SUPPORT ANGLE CRACKED @ OTBD END; MRK'D. / REMOVED CRACKED ANGLE AT RH WING T/E UPPER FIXED T/E PANEL JUST I/B OF DEFLECTION CONTROL RIB AND INSTALLED NEW ANGLE ALL IAW SRM 51-40-02-0G-0 AND DWG 115A2512 REV -. APPLIED CIC IAW AMM 51-21-91-620-802. PART NO: 115A215646 ATAG: A77920