As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 3.5 INCH CRACK IN LT WING LEADING EDGE RIB AT HI-LOK IN UNDERSIDE OF LEADING EDGE AT XOS 516. THE RIB WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED ON RIB IAW SRM 57-02, FIGURE 6 AND 51-10-3. THE RIB WAS REINSTALLED IAW SRM 51-30-2.