What was found
FOUND 5 INCH CRACK ON L/E COMPOSITE PANEL, O/B OF NR 2. ENGINE ABOUT 3 FT BACK OF LEADING EDGE. STARTED PREP FOR COMPOSITE REPAIR STARTED BLENDING AREA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND 5 INCH CRACK ON L/E COMPOSITE PANEL, O/B OF NR 2. ENGINE ABOUT 3 FT BACK OF LEADING EDGE. STARTED PREP FOR COMPOSITE REPAIR STARTED BLENDING AREA.