As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT O/B AILERON / FRONT SPAR / LWR FLANGE / XDA 928: TOOLING DAMAGE TO LOWER SPAR FLANGE. SPAR IS M/F SOLID GRAPHITE LAMINATE, APPROX .208 THICK. LOWER FLANGE IS DELAMINATED THROUGH THICKNESS OVER APPROX 1 INCH DEPTH (CHORD-WISE) X 2 WIDTH (SPAN-WISE). REPAIR CONSISTS OF SCARFING OUT DAMAGE AND INSTALLING PRECURED GRAPHITE REPAIR DOUBLER.