As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING NDT INSPECTION FOUND 1EACH FASTENER HOLE WITH CRACK ON RT VERTICAL STAB FRONT SPAR CAP FORWARD FLANGE. STA ZFS-52.267. REMOVED UPPER L/E SURFACE AND REMOVED DAMAGE. HFEC TRIMOUT. NO DEFECTS NOTED. FABRICATED REPAIR ANGLE, STRAP AND FILLERS IAW DWG 09550005. 3 RIBS BELOW REPAIR, DERIVETED FOM AND RIVETS REINSTALLED. OPEN HOLES DURING REPAIR HFEC INSPECTED. NO DEFECTS NOTED.