What was found
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 601, WL 203 LEFT SIDE CHORD ANGLE. REPAIRED STIFFENER ANGLE PER EA 65335 ADN TR 53-10-23. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 601, WL 203 LEFT SIDE CHORD ANGLE. REPAIRED STIFFENER ANGLE PER EA 65335 ADN TR 53-10-23. (M)