What was found
IAH - INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE, LT SIDE. A REPAIR WAS PERFORMED IAW SRM 53-05, FIGURE 23A. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IAH - INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE, LT SIDE. A REPAIR WAS PERFORMED IAW SRM 53-05, FIGURE 23A. (X)