What was found
CLT - DURING A RON VISUAL INSPECTION, FOUND A 1.25 INCH CRACK LEFT SIDE OF FUSELAGE AT STRINGER 24L, 24 INCHES AFT OF AFT WING TO BODY FAIRING SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING A RON VISUAL INSPECTION, FOUND A 1.25 INCH CRACK LEFT SIDE OF FUSELAGE AT STRINGER 24L, 24 INCHES AFT OF AFT WING TO BODY FAIRING SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01. (M)