What was found
INSPECTION FOUND VERTICAL STABILIZER RT ACCESS PANEL NR 5216 AND STIFFENER CORRODED. A NEW PANEL AND NUT PLATES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-30-2, 51-10-2, AND MM 51-20-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND VERTICAL STABILIZER RT ACCESS PANEL NR 5216 AND STIFFENER CORRODED. A NEW PANEL AND NUT PLATES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-30-2, 51-10-2, AND MM 51-20-0.