What was found
AT C-CHECK, RIGHT WING LEADING EDGE VERTICAL STIFFENER HAS A 2 INCH CRACK AT LOWER END AS VIEWED THROUGH ACCESS OPENING NR 6401 FRONT SPAR STA 120. STOP DRILL, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 7 X 1.25 X 1. N/R 2017.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, RIGHT WING LEADING EDGE VERTICAL STIFFENER HAS A 2 INCH CRACK AT LOWER END AS VIEWED THROUGH ACCESS OPENING NR 6401 FRONT SPAR STA 120. STOP DRILL, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 7 X 1.25 X 1. N/R 2017.