As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, FOUND CRACK ON STRINGER CLIP ON RIGHT WING AT, XRS 22.730 AND BETWEEN STRINGERS 1R AND 2R. NEITHER REPLACEMENT PART NOR BLANK FORGING AVAILABLE FROM ACFT MFR. FABRICATED AND INSTALLED NEW CLIP IAW TIMCO REO-02751 DTD 2/11/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).