As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - DURING C-4 CHECK, FOUND .125 INCH CRACK IN FUSELAGE SIN 727D PLUS 3 INCHES AND .5 INCH BELOW STRINGER 23R. CUT OUT DAMAGE APPROX 8 INCH BY 6 INCH AREA. INSTALLED DOUBLER AND FILLER PER TYPICAL REPAIR 53-60-03. DOUBLER MEASURES 17 INCHES BY 17 INCHES. ADDED WEIGHT FOR REPAIR IS 2 LBS. REPAIRED PER TYPICAL REPAIR 53-60-03. (M)