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 ABOVE #2 PYLON AFT T IP LWR SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LWR ATTACH BOLT / REMOVED AND REPLACED (RIGHT WING) UPPER T/E PANEL ABOVE #2 PYLON AFT TIP LWR SUPPORT ANGLE THAT WAS CRACKED AT TRANSVERSE WEB LWR ATTACH BOLT. IAW AMM 20-50-11-901-801 89813U 09-15-17