What was found
CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .875 INCH CRACK AFT OF 620 STRINGER 16. INSTALLED REPAIR PART PER SRM 53-00-03 FIG 201. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .875 INCH CRACK AFT OF 620 STRINGER 16. INSTALLED REPAIR PART PER SRM 53-00-03 FIG 201. (M)