What was found
DURING OP-16, FOUND A 23 INCH CRACK AT RIGHT WING TOP, IN LEADING EDGE PANEL, AFT OF CENTER OF NR 18 LEADING EDGE FLAP. REPAIRED PER SRM 51-40-12 AND TWA STANDARD PRACTICES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP-16, FOUND A 23 INCH CRACK AT RIGHT WING TOP, IN LEADING EDGE PANEL, AFT OF CENTER OF NR 18 LEADING EDGE FLAP. REPAIRED PER SRM 51-40-12 AND TWA STANDARD PRACTICES.