What was found
DURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING LEADING EDGE PLATING WAS FOUND CRACKED AT THE INBOARD STUB WING, INBOARD END. THE CRACK WAS REPAIRED IAW THE DOUGLAS SRM 57-2-1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING LEADING EDGE PLATING WAS FOUND CRACKED AT THE INBOARD STUB WING, INBOARD END. THE CRACK WAS REPAIRED IAW THE DOUGLAS SRM 57-2-1. (M)