As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RH WING TE: DEFLECTION CONTROL RIB ORRS 261+11;18 INCH AFT OF REAR SPAR; REAR SUPPORT ATTACH POINT HAS CRACK.<[01] REMOVED AND REPLACED SUPPORT AT R/WING TE; ORRS 261 + 11.18 AFT OF REAR SPAR IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION