As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT FIN STA 42 AT STRINGER 1R BETWEEN RIB 3A AND 4. THE CRACK WAS LOCATED BELOW AN EXISTING REPAIR. THE EXISTING REPAIR WAS REMOVED AND BOTH DAMAGE LOCATIONS INCORPORATED INTO ONE REPAIR PER B727 SRM 55-30-3, FIG 1. THE REPAIR WAS DOCUMENTED PER ER/A 366859-14.