Incident Overview
During a training flight, the pilot initiated an autorotation at approximately 500 feet and 60 knots. Both the pilot and the FAA check airman reported that the main rotor RPM was in the 'low green' range during the maneuver.
Loss of Control and Landing
As the helicopter flared, a partial loss of control occurred. The right skid sank several inches into the wet, grassy terrain. The helicopter then skidded approximately 15 feet before coming to rest in a nose-low, left bank attitude.
Rotor Strike and Damage
The main rotors struck the tailboom, severing it. The pilot stated that he had informed the check airman that the grass was wet prior to the maneuver.
Maneuver Status
According to the report, the autorotation to touchdown was not a required maneuver, nor was it prohibited. The check airman did not intervene during the conduct of the autorotation.
Key Facts
- Autorotation initiated at 500 feet and 60 knots
- Main rotor RPM in low green range
- Partial loss of control during flare
- Right skid sank into wet grass
- Helicopter skidded 15 feet
- Main rotors severed tailboom
- Pilot informed check airman of wet grass
- Maneuver was not required, but not prohibited
- Check airman did not intervene