What was found
UPON INSPECTION, FOUND A CRACK IN RIB 17. REPAIRED SRM 57-50-3, FOR NR 6 L/E SLAT PANEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON INSPECTION, FOUND A CRACK IN RIB 17. REPAIRED SRM 57-50-3, FOR NR 6 L/E SLAT PANEL.