As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, FOUND .375 INCH CRACK AT ANGLE ON BOTTOM OF RIGHT WING UPPER T/E PANEL AT WEB 5 INCHES FORWARD OF INBOARD AILERON L/B LEADING EDGE. FABRICATED NEW ANGLE PER SRM 51-10-1 PAGE 4. INSTALLED ANGLE PER SRM 51-30-2 PAGE 1. (M)