As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 161EL VERTICAL ATTACHMENT ANGLE IS CRACKED. LOCATED & DRILLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET UNDER ACCESS PANEL 161EL ON LT UPPER WING IAW SRM 51-42-06.