As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RH WING UPPER FIXED TE PANEL 651ET LATERAL STIFFNER CRACKED 12.<[01] UPPER RIGHT WING PANEL (651CT) CRACK IS LOCATED IN THE RADIUS OF THE PANEL STIFFENER JUST FORWARD OF THE VISIBLE NUT PLATES AND IS APPROXIMATELY 12? IN LENGTH. REMOVED AND REPLACED WING PANEL ASSY. 651DT IAW SRM 51-40-02-0G-0