As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870. FRAME CLIP WAS REPAIRED PER SRM 53-00-06-2R REPAIR 2. HFEC INSPECTION WAS ACCOMPLISHED ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870 AFTER TRIM OUT. NO CRACKS WERE FOUND PER NDT SPM PART 6, 06-10-01.001.