As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV-1, THE FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AT CANTED STA 1520.225 AND LONGERON L-2L. THE HORIZONTAL LEG WAS TRIMMED SIMILAR TO MD80 SRM 53-05-D, FIGURE 23. FILLER WAS ADDED TO THE TRIMMED OUT AREA AND A REPAIR ANGLE INSTALLED.