What was found
INSPECTION FOUND A .5 INCH CRACK IN LT VERTICAL STABILIZER SLIDER PANEL AND A .75 INCH CRACK IN RT VERTICAL STABILIZER SLIDER PANEL. BOTH PANELS WERE REPLACED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN LT VERTICAL STABILIZER SLIDER PANEL AND A .75 INCH CRACK IN RT VERTICAL STABILIZER SLIDER PANEL. BOTH PANELS WERE REPLACED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-2.