As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE PERFORMING AN INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION IAW TASK RJ2-57-900-320, THE AME FOUND A CRACK EMINATING FROM 1 OF THE RELIEF CUTOUTS FOR THE STR IN THE WEB OF THE SUPPORT ANGLE, PN: 601R10011-13. THE ACFT IS CURRENTLY DOWN FOR A SCHEDULED "C" CHECK. REPAIR PARTS FABRICATED AND HEAT TREATED IAW SRM 51-10-06 SECT.3D. ALUMINUM ALLOY FASTENERS INSTALLED IAW SRM 51-42-21 AND REPROTECTED IAW SRM 51-25-00 AND 51-25-16.