What was found
INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER FORWARD LEFT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. REPAIRED ANGLE 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 .5 INCH CRACK IN VERTICAL STABILIZER FORWARD LEFT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. REPAIRED ANGLE IAW SRM 55-02, FIGURE 26.