As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/E VERTICAL STABILIZER FWD ANGLE HAS CRACKED INSIDE LT SIDE OF VERTICAL STABILIZER AT VERTICAL FUSE BOXED STRUCTURE INSIDE OF LOWEST PANEL OPENING. R & R FWD ANGLE INSIDE LEFT VERTICAL STABILIZER AT VERTICAL FUSE BOX IAW DWG 173T1215 AND SRM 51-40-02. ACFT WAS GROUNDED.