What was found
INSPECTION FOUND A .5 INCH CRACK IN FRAME ATTACH ANGLE INSIDE LT SIDE OF VERTICAL STABILIZER AT STRINGER 5L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN FRAME ATTACH ANGLE INSIDE LT SIDE OF VERTICAL STABILIZER AT STRINGER 5L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.