What was found
INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1486, L3R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1486, L3R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23.