What was found
INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER ATTACH ANGLE AT STA 142 CENTER SPAR LEADING EDGE. THE CRACK WAS STOP DRILLED IAW SRM 55-10-4. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 55-10-4 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER ATTACH ANGLE AT STA 142 CENTER SPAR LEADING EDGE. THE CRACK WAS STOP DRILLED IAW SRM 55-10-4. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 55-10-4 AND 51-30-2.