What was found
INSPECTION FOUND A .5 INCH CRACK AT RIVET HOLES OF NR 3 SLAT PANEL ON I/B SIDE OF PANEL. FILLER AND DOUBLER WERE INSTALLED IAW BOEING DRAWING 65C30133.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT RIVET HOLES OF NR 3 SLAT PANEL ON I/B SIDE OF PANEL. FILLER AND DOUBLER WERE INSTALLED IAW BOEING DRAWING 65C30133.