What was found
INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LEFT INTERNAL ATTACH ANGLE CRACKED IN HALF JUST BELOW AFT SIDE OF PANEL CUTOUT NR 6301A. A NEW ATTACH ANGLE WAS INSTALLED IAW SRM 51-30.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LEFT INTERNAL ATTACH ANGLE CRACKED IN HALF JUST BELOW AFT SIDE OF PANEL CUTOUT NR 6301A. A NEW ATTACH ANGLE WAS INSTALLED IAW SRM 51-30.