As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A "C" CHECK: RT WING LEADING EDGE COVE PANEL INBD SUPPORT ANGLE IS CRACKED AT WS 130. REMOVED R/W L/E COVE PNL SUPPORT ANGLE AND FABBED NEW FROM 2024-T3 .050 PO NR 9001417 DIM 17 1/2 INCH BY 1 1/2 INCH IAW 727 SRM 57-20-2 FIG 1. NEW ANGLE TREATED AND PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-30-2.