What was found
INSPECTION FOUND A 2 INCH CRACK IN RT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 180, STRINGER 7. THE CRACKED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-30-3, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN RT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 180, STRINGER 7. THE CRACKED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-30-3, FIGURE 1.