What was found
INSPECTION FOUND A .625 INCH CRACK IN LT VERTICAL STABILIZER ANGLE 37.5 INCHES AFT OF STA 1089.5. REPAIRED IAW SRM 55-02, FIGURE 26.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .625 INCH CRACK IN LT VERTICAL STABILIZER ANGLE 37.5 INCHES AFT OF STA 1089.5. REPAIRED IAW SRM 55-02, FIGURE 26.