What was found
INSPECTION FOUND A .5 INCH CRACK IN VERTICAL ATTACH ANGLE AT FS 658, BL 45R. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-3, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN VERTICAL ATTACH ANGLE AT FS 658, BL 45R. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-3, AND 51-30-5.