What was found
CLT - Q-4, INNER CHORD ANGLE CRACKED .50 INCH AT STA 616 LT BELOW FLOOR LEVEL STR 17. INSTALLED FABRICATED DOUBLER AND FILLER PER TR 53-62-01. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q-4, INNER CHORD ANGLE CRACKED .50 INCH AT STA 616 LT BELOW FLOOR LEVEL STR 17. INSTALLED FABRICATED DOUBLER AND FILLER PER TR 53-62-01. (X)