What was found
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L AT BS 827 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND TR 53-10-14. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L AT BS 827 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND TR 53-10-14. (M)