What was found
INSPECTION FOUND A .5 INCH CRACK IN STRINGER 28R AT STA 440. THE CRACKED SECTION OF STRINGER WAS CUT OUT AND A J-ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN STRINGER 28R AT STA 440. THE CRACKED SECTION OF STRINGER WAS CUT OUT AND A J-ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03.