What was found
DURING INSPECTION, STRINGER 8R OF THE VERTICAL STAB. HAS A CRACK ON THE FIN STA. 157.2 RIB ATTACHMENT TAB. THE SUBJECT CRACK RUNS FROM FASTENER HOLE TO EDGE OF TAB. A REPAIR ANGLE WAS INSTALLED IN ACCORDANCE WITH B727 S/B 55-0075.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, STRINGER 8R OF THE VERTICAL STAB. HAS A CRACK ON THE FIN STA. 157.2 RIB ATTACHMENT TAB. THE SUBJECT CRACK RUNS FROM FASTENER HOLE TO EDGE OF TAB. A REPAIR ANGLE WAS INSTALLED IN ACCORDANCE WITH B727 S/B 55-0075.