What was found
INSPECTION FOUND A .25 INCH CRACK AT UPPER LEFT CORNER OF THE L-1 WINDOW FRAME. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-01, FIGURE 210, SHEETS 1-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK AT UPPER LEFT CORNER OF THE L-1 WINDOW FRAME. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-01, FIGURE 210, SHEETS 1-4.