As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 CRACK IN ANGLE OF LT WING FORWARD SIDE AT WING ROOT, WHERE FORWARD SPAR GOES INTO FUSELAGE. THE SEAL BRACKET AND ANGLE AT WING ROOT WERE REMOVED IAW SRM 51-30-3. AN ANGLE WAS FABRICATED IAW SRM 51-10-4. THE ANGLE AND SEAL BRACKET WERE INSTALLED IAW SRM 51-30-3 AND 51-30-2.