Maneuver
At the completion of a simulated autorotation maneuver, the main rotor severed the tailboom. The check airman reported that at approximately 20 feet above ground level he determined the sink rate was excessive and decided to perform a power recovery. The check airman stated, "I repositioned my hand, started opening the throttle while leveling the aircraft and applying a cushioning pitch pull."
Impact
The helicopter impacted off the left side of the runway with "the skids aligned with the direction of travel slightly aft skid low." The check airman reported, "The aircraft rocked up onto the toes of the skids and I increased collective pitch and applied aft cyclic, when I did the main rotor impacted the tailboom severing it."
Conclusion
The event involved a simulated autorotation, a power recovery attempt, and a subsequent impact that led to the main rotor striking and severing the tailboom. No analysis or causal factors are provided beyond the check airman's description.