What was found
AT C-CHECK, VERTICAL STAB INTERIOR, FIN STA 157.2 STR 8 TO FRAME IS CRACKED. CUT OUT DAMAGED AREA AT FLANGE OF STRINGER 8, CUT NEW ANGLE AND INSTALLED REPAIR PER SRM 55-30-4. REPAIR 1 BY 12, STRAP 12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, VERTICAL STAB INTERIOR, FIN STA 157.2 STR 8 TO FRAME IS CRACKED. CUT OUT DAMAGED AREA AT FLANGE OF STRINGER 8, CUT NEW ANGLE AND INSTALLED REPAIR PER SRM 55-30-4. REPAIR 1 BY 12, STRAP 12.