What was found
CLT - DURING RON VISUAL INSPECTION, FOUND A 1.2 INCH CRACK AT BS 727B PLUS 18 INCHES, 0.4 INCH ABOVE STR 18L FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3 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 1.2 INCH CRACK AT BS 727B PLUS 18 INCHES, 0.4 INCH ABOVE STR 18L FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3 FIG 6. (X)