What was found
INSPECTION FOUND A 1.5 INCH CRACK IN THE RADIUS OF THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT FS 1474. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05. (M)
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 THE RADIUS OF THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT FS 1474. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05. (M)