What was found
.25 PREVIOUSLY STOP DRILLED CRACK AT INBOARD LEADING EDGE OF RIGHT WING NR 6 SLAT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
.25 PREVIOUSLY STOP DRILLED CRACK AT INBOARD LEADING EDGE OF RIGHT WING NR 6 SLAT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3.