What was found
INSPECTION FOUND A 2 INCH CRACK IN NR 4 SLAT CLOSURE PANEL. THE PANEL WAS REPAIRED IAW SRM 51-70-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN NR 4 SLAT CLOSURE PANEL. THE PANEL WAS REPAIRED IAW SRM 51-70-05.