What was found
AFTER PLATE REMOVAL, CRACK ON PLATE ANGLE WAS FOUND AT FWD WASTE INTERNAL STRUCTURE, PLATE ANGLE AT FWD WASTE INTERNAL STRUCTURE WAS REPLACED IAW SRM 51-42-06-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER PLATE REMOVAL, CRACK ON PLATE ANGLE WAS FOUND AT FWD WASTE INTERNAL STRUCTURE, PLATE ANGLE AT FWD WASTE INTERNAL STRUCTURE WAS REPLACED IAW SRM 51-42-06-001-001-A01.