What was found
INSPECTION FOUND A 1.2 INCH CRACK IN RT LOWER VERTICAL STABILIZER DRAG ANGLE AT FORWARD CENTER SPAR POSITION. THE ANGLE WAS REPAIRED IAW SRM 53-20-00, FIGURE 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.2 INCH CRACK IN RT LOWER VERTICAL STABILIZER DRAG ANGLE AT FORWARD CENTER SPAR POSITION. THE ANGLE WAS REPAIRED IAW SRM 53-20-00, FIGURE 3.