As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE IS CRACKED AT TRANSVERSE WEB LOWER FWD ATTACH BOLT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED RH UPPER T/E PANEL SUPPORT ANGLE ON WEB ABOVE THE #2 PYLON AFT TIPPER SOPM 20-50-01; STEPS 3;4;5; SRM 51-40-02-0G-0; STEPS 4.B. AND E; AIPC 57-50-00-25.