As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
*AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED AT L/H SIDE (MARKED) (C-CHECK RO 1/30/2024) REMOVED AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE REF CRJ 700 SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01 AND INSTALLED NEW AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE REF CRJ 700 SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01 AND DWG IFBA670-35002 REV-C. COMPLIED WITH 51-900-1002-SKY