What was found
CLT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND A 3 INCH CRACK AT NR 1 ENGINE PYLON PANEL 5724L DOUBLER. INSTALLED DOUBLER PER SRM TYPICAL REPAIR 54-50-04D. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND A 3 INCH CRACK AT NR 1 ENGINE PYLON PANEL 5724L DOUBLER. INSTALLED DOUBLER PER SRM TYPICAL REPAIR 54-50-04D. (M)