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 157.2 STR 8L. CRACK RAN FROM CTR OF HOLE TO EDGE OF STRINGER. FABRICATED REPAIR ANGLE PER MM 55-30-0 FIG 803 OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 FIG 803.