What was found
INSPECTION FOUND A .5 INCH CRACK IN PILOT'S FORWARD WINDOW POST SKIN AT NR 1 WINDSHIELD UPPER O/B CORNER, STA 196.5, S6L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-10-01, FIGURE 210.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN PILOT'S FORWARD WINDOW POST SKIN AT NR 1 WINDSHIELD UPPER O/B CORNER, STA 196.5, S6L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-10-01, FIGURE 210.