What was found
INSPECTION FOUND A 4 INCH CRACK IN RT LOWER VERTICAL STABILIZER SLIDING PANEL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01 FIGURE 2, 51-10-2A, 51-10-4, 51-10-3 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4 INCH CRACK IN RT LOWER VERTICAL STABILIZER SLIDING PANEL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01 FIGURE 2, 51-10-2A, 51-10-4, 51-10-3 AND 51-30-2.