What was found
INSPECTION FOUND A 1.5 CRACK IN VERTICAL STABILIZER LEADING EDGE INTERNAL ATTACH ANGLE, RT SIDE. THE CRACK WAS LOCATED JUST BELOW AFT SIDE OF PANEL CUTOUT NR 6301A. THE ATTACH ANGLE WAS REPLACED IAW EA 5340-01012 AND SRM 51-60-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 CRACK IN VERTICAL STABILIZER LEADING EDGE INTERNAL ATTACH ANGLE, RT SIDE. THE CRACK WAS LOCATED JUST BELOW AFT SIDE OF PANEL CUTOUT NR 6301A. THE ATTACH ANGLE WAS REPLACED IAW EA 5340-01012 AND SRM 51-60-0.