As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD SPAR ATTACH BRACKET AT STA 94.0 LEFT AND RIGHT SIDES. DURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE LOWER PORTION OF THE UPPER RADIUS FOR THE FORWARD SPAR SLOT CUT-OUT. LEFT FRAME WAS CRACKED .3750 INCH LONG, RT FRAME FOUND CRACKED .0625 INCH LONG. CAUSE: APPEARED TO BE STRESS RELEASE CRACK. ACT: 6,835.2 HOURS.