As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV, FOUND VERTICAL STABILIZER EXTERIOR SKIN HAS A STOP DRILL ON RT SIDE 20 INCHES FWD OF REAR SPAR AT FUSELAGE, REPAIRED PER FABRICATING DOUBLER PER MM 55-30-0 PG 801 CRACK PREVIOUSLY STOP DRILLED, DYE CHECKED CRACK AND NO FURTHER DAMAGE. INSTALLED DOUBLER PER MM 55-30-0 PG 801.