What was found
INSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STRINGER 22L STA 360. THE CRACKED SECTION WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STRINGER 22L STA 360. THE CRACKED SECTION WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.