What was found
INSPECTION FOUND A 1.125" CRACK AT UPPER R/H CORNER I/B SIDE OF CO-PILOT'S R/H WINDOW POST SKIN AND GUSSET. THE CRACKED AREA WAS ROUTED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-1, FIGURE 210.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.125" CRACK AT UPPER R/H CORNER I/B SIDE OF CO-PILOT'S R/H WINDOW POST SKIN AND GUSSET. THE CRACKED AREA WAS ROUTED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-1, FIGURE 210.