What was found
CLT - FOUND VERTICAL CHORD ANGLE CRACKED .25 INCH, BS 178, LBL 5.7, WL 184. INSTALLED REPAIR PER SRM 53-10-08. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - FOUND VERTICAL CHORD ANGLE CRACKED .25 INCH, BS 178, LBL 5.7, WL 184. INSTALLED REPAIR PER SRM 53-10-08. (M)