Summary
On January 17, 2016, a Tucker Mitchel C H 13 (N9669) was involved in an incident near Zephyrhills, FL. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's failure to maintain aircraft control while on ground standing with the engine running during high crosswind conditions which resulted in a static rollover and collision with the ground.
The pilot of the experimental helicopter was returning from a local flight and landed near his hanger to drop off his passenger. After his passenger disembarked, the pilot was preparing to take off and reposition the helicopter to another spot, but before he added power for liftoff, a strong gust of wind struck the left side of the helicopter, thrusting the cyclic control out of his hand and hard over to the right. This caused the helicopter to lift up and roll onto its right side, causing substantial damage to the blades, engine mount, fuselage and tail boom. The pilot stated, it happened very quickly and there was no chance to recover. Post-accident examination of the helicopter did not reveal any preimpact mechanical malfunctions which would have precluded normal operation.
This incident is documented in NTSB report ERA16CA102. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N9669.
Accident Details
Probable Cause and Findings
The pilot's failure to maintain aircraft control while on ground standing with the engine running during high crosswind conditions which resulted in a static rollover and collision with the ground.
Aircraft Information
Registered Owner (Current)
Analysis
The pilot of the experimental helicopter was returning from a local flight and landed near his hanger to drop off his passenger. After his passenger disembarked, the pilot was preparing to take off and reposition the helicopter to another spot, but before he added power for liftoff, a strong gust of wind struck the left side of the helicopter, thrusting the cyclic control out of his hand and hard over to the right. This caused the helicopter to lift up and roll onto its right side, causing substantial damage to the blades, engine mount, fuselage and tail boom. The pilot stated, it happened very quickly and there was no chance to recover. Post-accident examination of the helicopter did not reveal any preimpact mechanical malfunctions which would have precluded normal operation. The wind at the time of the accident were from 240 degrees at 13 knots gusting to 17.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16CA102