What was found
VERTICAL STAB UPPER RIGHT LEADING EDGE SPAR CRACKED (.25) AROUND RIVET AT STIFFENER PLATE JUST BELOW TENSION TIE FORWARD ATTACH BOLT. REMOVED FASTENERS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 55-30-6 AND 51-1-20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB UPPER RIGHT LEADING EDGE SPAR CRACKED (.25) AROUND RIVET AT STIFFENER PLATE JUST BELOW TENSION TIE FORWARD ATTACH BOLT. REMOVED FASTENERS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 55-30-6 AND 51-1-20.