What was found
LT INTERNAL VERTICAL STABILIZER ATTACH ANGLE IS CRACKED IN RADIUS. REMOVED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW DWG 5912188.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT INTERNAL VERTICAL STABILIZER ATTACH ANGLE IS CRACKED IN RADIUS. REMOVED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW DWG 5912188.