As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER CRACKED VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 180.6 STA 9L. CRACK RUNS FROM HOLE TO EDGE OF PART. NO STOP DRILL REQUIRED. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. IK INSTALL. BEGAN INSTALL OF REPAIR PER M/M 55-30-0 FIG 803. FINISHED INSTALL OF REPAIR PER M/M 55-30-0 FIG 803.