As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, RT FWD VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. MAINTENANCE R & R RT FWD VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. MAINTENANCE R & R NEW DRAG ANGLE ON RT FWD VERTICAL TO FUSELAGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.