As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - DURING WALK-AROUND CHECK VISUAL INSPECTION, FOUND A 2.25 INCH CRACK AT STA 727D PLUS 2 INCHES TO 727D PLUS 4.25 INCHES JUST BELOW AND PARALLEL TO STR 23R FUSELGE SKIN. FABRICATED AND INSTALLED REPAIR FILLER AND EXTERNAL DOUBLER PER TR 53-60-03. (X)