What was found
CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH INNER SKIN CRACK AT NR 2 PYLON/OUTBOARD SKIN AT PANEL NR 5824R OPENING. INSTALLED DOUBLER, OVERSIZE DRILL HOLE PER REPAIR DOCUMENT SRM 54-50-04C TYPICAL REPAIR. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH INNER SKIN CRACK AT NR 2 PYLON/OUTBOARD SKIN AT PANEL NR 5824R OPENING. INSTALLED DOUBLER, OVERSIZE DRILL HOLE PER REPAIR DOCUMENT SRM 54-50-04C TYPICAL REPAIR. (X)