What was found
INSPECTION FOUND A .75 INCH CRACK IN STRINGER 16R AT BS 500C. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK IN STRINGER 16R AT BS 500C. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.