As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(RIGHT WING) UPPER WING PANEL SUPPORT U CHANEL AT 9-INCH O/B OF FUSELAGE; ATTACH ANGLE CRACKED AT REAR SPAR ATTACH POINT<[01] REMOVED AND REPLACED ANGLE P/N 115A5582-2 AT R/WING PANEL SUPPORT U CHANEL AND REAR SPAR ATTACH POINT IAW SRM 51-40-02-0G-0.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.