As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE LT FORWARD SPAR CAP ANGLE AT VSS 84.10 AND 20 PERCENT CHORD FROM THE TOP OF THE ANGLE DOWN AND STARTING ABOVE THE SECOND FASTENER DOWN AND EXTENDING PAST THE FASTENER HOLE, 1.125" IN LENGTH. REPAIRED IAW FR-CO-02602R1.