What was found
CLT - DURING RON VISUAL INSPECTION, FOUND A 0.9 INCH CRACK AT BS 727A PLUS 17.5 INCHES , 0.5 INCH ABOVE STR 18L SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-3-3 FIG 6. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING RON VISUAL INSPECTION, FOUND A 0.9 INCH CRACK AT BS 727A PLUS 17.5 INCHES , 0.5 INCH ABOVE STR 18L SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-3-3 FIG 6. (X)