Summary
On February 06, 2017, a Robinson R22 (N7685H) was involved in an incident near West Palm Beach, FL. All 2 people aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The flight instructor’s failure to maintain helicopter control while demonstrating low rotor rpm operations from a hover.
According to the flight instructor, he was conducting an instructional flight in the helicopter and demonstrating low rotor rpm operations from a hover. The helicopter was at a 3 ft hover when he initiated the maneuver, with the student pilot "on the flight controls" following the flight instructor's movements. As the throttle was reduced, the nose of the helicopter began to rotate to the left. The flight instructor pushed the right anti-torque pedal to counter the rotation but the pedal initially felt like it was "blocked." The right skid contacted the taxiway causing the helicopter to bounce and rotate to the right.
This incident is documented in NTSB report ERA17CA101. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N7685H.
Accident Details
Probable Cause and Findings
The flight instructor’s failure to maintain helicopter control while demonstrating low rotor rpm operations from a hover.
Aircraft Information
Registered Owner (Historical)
Analysis
According to the flight instructor, he was conducting an instructional flight in the helicopter and demonstrating low rotor rpm operations from a hover. The helicopter was at a 3 ft hover when he initiated the maneuver, with the student pilot "on the flight controls" following the flight instructor's movements. As the throttle was reduced, the nose of the helicopter began to rotate to the left. The flight instructor pushed the right anti-torque pedal to counter the rotation but the pedal initially felt like it was "blocked." The right skid contacted the taxiway causing the helicopter to bounce and rotate to the right. The flight instructor applied full throttle and collective to attempt to gain altitude; however, the helicopter departed the taxiway, entered an adjacent grass area, and rolled over onto its left side. The helicopter sustained substantial damage to the main rotor and the tail boom. Examination of the flight control system by a Federal Aviation Administration inspector did not reveal any anomalies. In addition, the flight instructor reported there was no preimpact mechanical failures or malfunctions with the helicopter that would have precluded normal operation.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA17CA101