What was found
CRACK FOUND IN FASTENER ROW LT SIDE OF VERTICAL STABILIZER FWD OF INTAKE. INSTALLED DOUBLER IAW SRM 55-01-00 FIGURE 2 SHEET 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND IN FASTENER ROW LT SIDE OF VERTICAL STABILIZER FWD OF INTAKE. INSTALLED DOUBLER IAW SRM 55-01-00 FIGURE 2 SHEET 2.