What was found
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 480, BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER ANGLE PER EA 65618 AND SRM 53-00-07 FIG 202. (X)
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 .50 INCH CRACK AT BS 480, BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER ANGLE PER EA 65618 AND SRM 53-00-07 FIG 202. (X)