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 SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE #2 PYLON AFT TIP<[01] REMOVED UPPER T/E SUPPORT ANGLE AT TRANSVERSE WEB ABOVE #2 PYLON AFT TIP AND INSTALLED NEW SUPPORT ANGLE P/N 115A2982-10; PO # 934058/1; IAW SRM 51-40-02-0G.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE