What was found
CLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, BS 178, LBL 7, WL 183. INSTALLED REPAIR ANGLES AND STRAPS PER SRM 53-10-08 FIG 205. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, BS 178, LBL 7, WL 183. INSTALLED REPAIR ANGLES AND STRAPS PER SRM 53-10-08 FIG 205. (M)