As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-03 CHECK A 2.5 INCHES CRACK WAS FOUND ON LT & RT SUPPORT ANGLES OF THE VERTICAL STABILIZER TRAILING EDGE 20 INCH ABOVE TAIL CONE AT BS 1110. MAINTENANCE CUTOUT SUPPORT ANGLES, FABRICATED 2 EACH SPLICE ANGLES AND A BEAM EXTRUSION, AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5535-02267-ES4.