What was found
INSPECTION FOUND A .25 INCH CRACK IN TOP RIB AND A .25 INCH CRACK IN 7TH RIB FROM BOTTOM OF VERTICAL STABILIZER LEADING EDGE. BOTH CRACKS WERE STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 55-01, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN TOP RIB AND A .25 INCH CRACK IN 7TH RIB FROM BOTTOM OF VERTICAL STABILIZER LEADING EDGE. BOTH CRACKS WERE STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 55-01, FIGURE 2.