What was found
CLT - Q-4, FRAME HAD .25 INCH CRACK AT STA 400 BETWEEN S9L AND S8L. DOUBLER INSTALLED PER TR NR 53-10-14. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q-4, FRAME HAD .25 INCH CRACK AT STA 400 BETWEEN S9L AND S8L. DOUBLER INSTALLED PER TR NR 53-10-14. (X)