What was found
CLT - FOUND VERTICAL CHORD (STIFFENER) CRACKED .25 INCH, BS 178, AFT SIDE RBL 5-7, WL 184. FOUND DOUBLER STRAP/REPAIR ANGLES PER SRM 53-10-11. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - FOUND VERTICAL CHORD (STIFFENER) CRACKED .25 INCH, BS 178, AFT SIDE RBL 5-7, WL 184. FOUND DOUBLER STRAP/REPAIR ANGLES PER SRM 53-10-11. (M)