What was found
PREVIOUS NOSE RIB O/B CRACKED 1 INCH AT NR 6 L/E SLAT PANEL. REPAIRED PER MM 57-54-0 FIG 804.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PREVIOUS NOSE RIB O/B CRACKED 1 INCH AT NR 6 L/E SLAT PANEL. REPAIRED PER MM 57-54-0 FIG 804.