As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ANGLE ON THE VERTICAL FRONT SPAR TO FUSELAGE SPLICE STRAP IS CHAFFED (MARKED) (C-CHECK RO 3/14/2022) REPLACED ANGLE ON THE VERTICAL FRONT SPAR TO FUSELAGE SPLICE STRAP REF DWG 600-21108 REV. C, CRJ200 SRM 51-42-21, CRJ200 SRM 51-41-02. COMPLIED WITH 51-900-1003-SKY.