As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(RIGHT WING) UPPER T/E PANEL SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL SUPPORT ANGLE AT TRANSVERSE WEB ATTACH POINT ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02-0G-0; SOPM 20-50-01 AND AIPC 57-50-00-25.