As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 0.2" CRACK IN L/H WING UPPER SPAR AT #4 HOLE FROM THE I/B SIDE COMMOM TO THE SUPPORT FITTING. AN OVERSIZED BOLT WAS INSTALLED IAW ECRA 5743-01050. A DETAILED VISUAL INSPECTION OR HFEC INSPECTION WILL BE PERFORMED ON THE SPAR VERTICAL FLANGE BELOW AND ABOVE FOOTPRINT OF MLG FITTING IAW ECRA 5743-01050 EVERY 4500 CYCLES.