Summary
On January 23, 2014, a Robinson Helicopter R22 BETA (N72AP) 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 certificated flight instructor's failure to maintain helicopter control during a run-on landing, resulting in a rollover and ground collision.
The certificated flight instructor (CFI) stated that during a local training flight he was demonstrating how to perform a run-on landing to the student pilot. During the landing, the helicopter began to travel toward the right edge of the paved surface. The CFI stated he countered the right slide with left cyclic input. As the helicopter approached the paved surface edge, the CFI raised collective in order to attempt put the helicopter into a hover but the helicopter left the paved surface. The helicopter subsequently rolled over on to the right side, which resulted in substantial damage to the tail boom, main rotor blades, and fuselage. According to a written report, there were no mechanical malfunctions with the helicopter prior to the accident.
This incident is documented in NTSB report ERA14CA102. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N72AP.
Accident Details
Probable Cause and Findings
The certificated flight instructor's failure to maintain helicopter control during a run-on landing, resulting in a rollover and ground collision.
Aircraft Information
Registered Owner (Current)
Analysis
The certificated flight instructor (CFI) stated that during a local training flight he was demonstrating how to perform a run-on landing to the student pilot. During the landing, the helicopter began to travel toward the right edge of the paved surface. The CFI stated he countered the right slide with left cyclic input. As the helicopter approached the paved surface edge, the CFI raised collective in order to attempt put the helicopter into a hover but the helicopter left the paved surface. The helicopter subsequently rolled over on to the right side, which resulted in substantial damage to the tail boom, main rotor blades, and fuselage. According to a written report, there were no mechanical malfunctions with the helicopter prior to the accident.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA14CA102