What was found
CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .75 INCH CRACK AND 5 INCH CRACK IN SKIN AROUND PANEL 5724L. INSTALLED DOUBLER PER TR 54-40-040. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .75 INCH CRACK AND 5 INCH CRACK IN SKIN AROUND PANEL 5724L. INSTALLED DOUBLER PER TR 54-40-040. (X)