What was found
INSPECTION FOUND A 2.75 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1474. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.75 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1474. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23B.