As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING WIGGLE PLATE HOLE DAMAGE ; WHILE PERFORMING OPEN HOLE INSP. FOUND 2 HOLE WITH CRACK INDICATION PER NDT PT. 6 51-00-00 PRO. 16 / REAMED FASTENER HOLES ON LT FIXED T/E LOWER PANEL PER AMM 57-50-02. / SRM 57-20-01-2R-2. REQUIRED NDT ON HOLE FASTENERS.; INSTALLED NEW WIGGLE PLATE WITH NEW FASTENERS IAW SRM 57-20-01-2R-2; INSTALLED NEW WIGGLE PLATE WITH NEW FASTENERS IAW SRM 57-20-01-2R-2