What was found
INSPECTION FOUND A 1" CRACK IN STRINGER 16R AND 16L AT STA 500C + 5". THE CRACKED AREA OF EACH STRINGER WAS REMOVED AND REPAIRS WERE 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 1" CRACK IN STRINGER 16R AND 16L AT STA 500C + 5". THE CRACKED AREA OF EACH STRINGER WAS REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-00-03.