As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ESC - DURING INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-02-18, THE RIGHT TRUSS WAS FOUND CRACKED. THE .5 INCH CRACK WAS CENTERED AT THE OIL PLUG ON THE UPPER LEFT FORWARD LEG. A WELD REPAIR WAS ACCOMPLISHED IAW BEECH REPAIR KIT NR 129-9006-1 REPAIR NR 2.