As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER ATTACH ANGLE BETWEEN LT WING INBOARD AND MIDDLE LE`S ARE CRACKED. REMOVED DAMAGED ANGLE ON LT WING LE AND DUPLICATED USING 0.040, 2024-T3 PER CRJ SRM 51-24-21 AND 51-40-11. OK TO ALODINE, PRIME, AND INSTALL. ALODINED AND PRIMED ANGLE IAW CRJ SRM 51-25-06 AND INSTALLED IAW CRJ SRM 51-42-06 AND 51-42-13.