What was found
UPON INSPECTION, A CRACK WAS FOUND RIB 16. REPAIRED RIB PER MM 57-54-0 FIG 4, 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, A CRACK WAS FOUND RIB 16. REPAIRED RIB PER MM 57-54-0 FIG 4, FOR NR 6 L/E SLAT PANEL.