What was found
CLT - DURING Q-5 INSPECTION, FOUND CRACKED INNER CHORD ANGLE .75 INCH AT BS 616 AND STR 16. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-5 INSPECTION, FOUND CRACKED INNER CHORD ANGLE .75 INCH AT BS 616 AND STR 16. (X)