As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING THE HIGH CYCLE FUSELAGE INSPECTION, A SHEARED BOLT WAS FOUND INSIDE THE FUSELAGE IN THE AREA OF STA 190 RIGHT SIDE WHERE THE FORWARD SPAR PASSES THROUGH THE FUSELAGE. SUBMITTER STATED AS THIS ITEM IS IMPORTANT TO THE STRUCTURAL INTEGRITY OF THE AIRCRAFT, BEECH WAS REQUESTED TO REPLACE THE BOLT.