What was found
INSPECTION FOUND TWO 1 CRACKS ON PLATE AT FASTENERS TOP OF WEB STRINGER 18R, FS 575. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-20-01, AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO 1 CRACKS ON PLATE AT FASTENERS TOP OF WEB STRINGER 18R, FS 575. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-20-01, AND 51-10-2.