As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER FLOOR PANEL SUPPORT IN CABIN AT MOST FORWARD POINT IS CRACKED. PANEL #151DTC. MX STOP DRILLED 1.25" "Z" CHANNEL CRACT AT FS 3481. FORMED DOUBLER OUT OF .032-2024 T3 OF THE SAME THICKNESS AND BEND RADIUS. IAW BEECHCRAFT 400XP SRM 51-40-00 AND 51-50-45. SEE SUPPORT ASSEMBLY-MIDDLE FUESELAGE, LOWER FIGURE 1 FOR PARTS AND SPEC. IAW SRM 53-10-53. WITH THIS REPAIR THERE IS NO RE-INSPECT CRITERIA FROM SRM MANUAL