As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED TWO INCH CRACK ON COCKPIT RIGHT UPPER LONGERON AT FS 107.0 AND WL 119.0. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED FILLER PROFILE TO MATCH REMOVED SECTION OF LONGERON. FABRICATED AND INSTALLED REINFORCEMENT ANGLE IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN BEECHCRAFT FIELD REPAIR FR-CO-01729, REV 2.